observer/jump seat option ica supplement - cessna support

TEXTRON AVIATION INC.AIRCRAFT DIVISION

WICHITA, KANSAS 67277

Observer/Jump Seat Option

ICA Supplement

MODEL NO: 700

SUPPLEMENT NO: ICA-700-25-00001SUPPLEMENT DATE: 9/26/2019

© TEXTRON AVIATION INC.Form 2261 Rev 1



REVISIONS

ICA-700-25-00001 Rev: - Date: 09/26/2019

ICA Summary Pages 1-7

Manuals Affected Description Title5-10-01 pages1-29

MSG-3 Inspection Time Limits

5-10-02 pages1-28

Systems, APU, and Powerplant Inspection Tasks

5-12-00 pages1-9

MSG-3 Inspection Documents and Other Required Tasks

5-12-02 pages1-4

Inspection Document 2

5-12-11 pages1-6

Inspection Document 11

5-18-00 pages1-5

Supplier Information

Maintenance Manual

25-10-00 pages601-604

Flight Compartment - Inspection/Check

• Adds the observer/jump seat inspection and the observer/jump seat oxygen mask inspection.

Maintenance Manual 35-10-00 pages1-5

Crew Oxygen System - Description and Operation

• Adds the observer/jump seat oxygen mask.

Maintenance Manual 35-10-00 pages601-

Crew Oxygen System - Inspection/Check

• Adds instructions for the inspection of the observer/jump seat oxygen mask.

Maintenance Manual 35-10-10 pages401-404

Crew Oxygen Mask - Removal/Installation

• Adds instructions for the removal and operation of the observer/jump seat oxygen mask.

Appendix A: Illustrated PartsCatalog

NOT USED

Appendix B: Wiring DiagramManual

NOT USED

Appendix C: Model 700-0011Interior Maintenance Manualand Illustrated Parts Catalog

25-20-35 pages1-3

Left-Hand Forward Closet with Jumpseat - Maintenance

• Contains Operation and Maintenance Instructions for the Left-Hand Forward Closet with Jump Seat.

Page 1 of 7Sep 26/2019

© TEXTRON AVIATION INC.ICA-700-25-00001 Form 2261 Rev 1



25-20-36-01pages 1-4

25-20-36-02pages 1-2

25-20-36-03pages 1-2

25-20-36-04pages 1-2

25-20-36-05pages 1-3

25-20-36-06pages 1-3

25-20-36-07pages 1-2

25-20-36-08pages 1-2

25-20-36-09pages 1-5

25-20-36-10pages 1-2

25-20-36-11pages 1-2

25-20-36-12pages 1-2

25-20-36-13pages 1-2

25-20-36-14pages 1-4

Model 700-0011 InteriorMaintenance Manual andIllustrated Parts Catalog

25-20-36-15pages 1-3

• Contains necessary Illustrated Parts for the Left-Hand Forward Closet with Jump Seat.

1. Export ComplianceA. This publication contains technical data and is subject to U.S. export regulations. This information has

been exported from the United States in accordance with export administration regulations. Diversioncontrary to U.S. law is prohibited.

ECCN: 9E991

2. Revision BarsA. Revision bars in this ICA supplement identify new ICAs and/or changes to the current ICAs in the

released maintenance manual.• New ICAs that are not in the current maintenance manual will have a revision bar from top to

bottom along the left margin.• ICAs that are in the current maintenance manual and have information added, deleted or revised

will have a revision bar(s) in the left margin adjacent to the added, deleted or revised information.





• New or changed illustrations will have a change bar for the entire length of the page.

3. Page NumberingA. The page number system for ICA included in this supplement have three-element numbers that are

separated by dashes. The three-element number is found at the bottom right corner of the page, leftof the page number. The date is found below the page number.

B. When the chapter/system element number is followed with zeros in the section/subsystem andsubject/unit element number (28-00-00), the information is applicable to the entire system.

C. When the section/subsystem element number is followed with zeros in the subject/unit elementnumber (28-21-00), the information is applicable to the subsystems in the system.

D. The subject/unit element number is used to identify information applicable to units in the subsystems.The subject/unit element number continues in sequence from the number -01- with the number ofsubsystem units in which maintenance information is necessary.

E. All system/subsystem/unit (chapter/section/subject) maintenance data is separated into specifiedtypes of information: Description and Operation, Troubleshooting, Maintenance Practices, etc.Blocks of page numbers that are in sequence are used to identify the type of information:(1) Description and Operation or Troubleshooting information may not be included if the procedure

is easy. When subtopics are short, they may be put together into the Maintenance Practicessection. Maintenance Practices can have a mix of subtopics that includes information to service,remove, install, adjust, test, clean, paint or do approved repairs.

(2) Longer procedures that are not as easy to do may be included in a specified section.Page 1 through 99 - Description and OperationPage 101 through 199 - TroubleshootingPage 201 through 299 - Maintenance PracticesPage 301 through 399 - Servicing01 through 499 - Removal/InstallationPage 501 through 599 - Adjustment/TestPage 601 through 699 - Inspection/CheckPage 701 through 799 - Cleaning/PaintingPage 801 through 899 - Approved Repairs

F. A typical page number:





G. Illustrations use the same figure numbers as the page block in which they appear. For example, Figure202 would be the second figure in a Maintenance Practices section.

4. Supplement RevisionsA. Revisions to this supplement may be accomplished if changes to this supplement are required after

release of the original issue and prior to incorporation into the manuals listed in the REVISIONS table.

B. All revisions to this supplement will have changes identified in detail in the revision block(s) above.

C. All pages in this ICA supplement will have the same date and are valid as of the date shown.

5. ICA Incorporation into Applicable Manuals

NOTE: Most ICA supplements will be incorporated in the next available revision to the manualslisted above and should be used in conjunction with those manuals until the next availablerevision is released.

A. The ICA Supplement List located in the Introduction section of each manual listed in the REVISIONStable will indicate the incorporation status as of the release date of the published revision.

B. The manual revision level of the supplement incorporation will be listed in the "Manual IncorporationStatus" column in the ICA Supplement List, when those ICAs associated with that manual have beenincorporated. After ICAs are incorporated, the manual that they are incorporated in must now be usedfor those ICAs instead of the supplement.• Based on revision cycle times for the affected manuals, MM ICAs, WDM ICAs, etc. in this

supplement may be incorporated in the manuals at different times.• There will not be a revision to this supplement to indicate incorporation in the manuals. Users are

required to check the ICA Supplement List for each manual affected to determine incorporationstatus.

C. This supplement will be completely superseded by the manuals listed in the REVISIONS table whenit has been incorporated in all of the manuals.





INTRODUCTION

1. PurposeA. The purpose of this Supplement is to provide the maintenance technician with the information

necessary to ensure the correct functionality and performance of the Observer/Jump Seat Option onthe Cessna Model 700 until this information gets incorporated into the next revision to the manualslisted in the "REVISIONS" section of this supplement.

B. This ICA supplement is designed to satisfy the requirements of 14 CFR 23.1529 "Instructions forContinued Airworthiness" associated with this installation. This document is a supplement to theModel 700 Maintenance Manual and will be incorporated in the next revision to the manual.

C. When this information is incorporated in the next revision to the manuals listed in the "REVISIONS"section, those manuals shall take precedence over this supplemental document. Refer to the "ICASupplement List" in the "Introduction" section of the respective manual for the status of all applicableICA Supplements.

D. Revisions to this supplement may occur if there is a change to any of the ICAs in this supplementprior to incorporation into all of the affected manuals.

NOTE: This document must be placed with the aircraft operator's Technical Library CD-ROMor Model 700 Maintenance Manual and incorporated into the operator's scheduledmaintenance program.

2. EffectivityA. These Instructions for Continued Airworthiness (ICA) are effective for the following aircraft model and

serialization.

Model Beginning Effectivity Ending Effectivity

700 -0011 And On

3. Complete ICA DocumentsA. The following document(s), in conjunction with this supplement, constitute the Instructions for

Continued Airworthiness for the Observer/Jump Seat Option on the Cessna Model 700. All itemsmust be available to the operator at initial delivery.(1) Model 700 Maintenance Manual(2) Model 700 Interior Maintenance Manual and Illustrated Parts Catalog

4. System ComponentsA. Refer to Appendix C: Model 700-0011 Interior Maintenance Manual and Illustrated Parts Catalog.





LIST OF INSTRUCTIONS FOR CONTINUED AIRWORTHINESS

1. Model 700 Maintenance ManualA. Chapter 5, Time Limits/Maintenance Checks

(1) Refer to 5-10-01, MSG-3 Inspection Time Limits(2) Refer to 5-10-02, Systems, APU, and Powerplant Tasks(3) Refer to 5-12-00, MSG-3 Inspection Documents and Other Required Tasks(4) Refer to 5-12-02, Inspection Document 2(5) Refer to 5-12-11, Inspection Document 11(6) Refer to 5-18-00, Supplier Information

B. Chapter 25, Equipment/Furnishings(1) Refer to 25-10-00, Flight Compartment - Inspection/Check

C. Chapter 35, Oxygen(1) Refer to 35-10-00, Crew Oxygen System - Description and Operation(2) Refer to 35-10-00. Crew Oxygen System - Inspection/Check(3) Refer to 35-10-10, Crew Oxygen Mask - Removal/Installation

2. Appendix C: Model 700-0011 Interior Maintenance Manual and Illustrated Parts CatalogA. Chapter 25, Equipment/Furnishings

(1) Refer to 25-20-35, Left-Hand Forward Closet with Jumpseat - Maintenance(2) Refer to 25-20-36-01(3) Refer to 25-20-36-02(4) Refer to 25-20-36-03(5) Refer to 25-20-36-04(6) Refer to 25-20-36-05(7) Refer to 25-20-36-06(8) Refer to 25-20-36-07(9) Refer to 25-20-36-08(10) Refer to 25-20-36-09(11) Refer to 25-20-36-10(12) Refer to 25-20-36-11(13) Refer to 25-20-36-12(14) Refer to 25-20-36-13(15) Refer to 25-20-36-14(16) Refer to 25-20-36-15





INSPECTION PROGRAM AND AIRWORTHINESS LIMITATIONS

1. Continuous Inspection ProgramA. This ICA Supplement revises the inspection program to include the inspection of the observer seat at

the existing interval of 54 months.

2. Airworthiness LimitationsA. Cessna Aircraft Company Model 700 Airworthiness Limitations Manual contains the system and

airframe limitations for the Model 700.

NOTE: The Airworthiness Limitations section is FAA-approved and specifies maintenancerequired under Section 43.16 and 91.403 of Title 14 Code of Federal Regulations, unlessan alternative program has been FAA approved.

(1) There are no new (or additional) airworthiness limitations associated with this equipment and/orinstallation.



CESSNA®MODEL 700

MAINTENANCE MANUAL

MSG-3 INSPECTION TIME LIMITS

1. Purpose and UseA. MSG-3 Inspection Tasks in Table 1 provide a list of MSG-3 derived inspection and servicing tasks that

must be completed for the Model 700 MSG-3 Inspection Program.

NOTE: In addition to the tasks listed in Table 1 below, there are other scheduled inspectionrequirements detailed in Chapter 5-12-00, MSG-3 Inspection Documents and OtherRequired Tasks that must be accomplished to be in compliance with the Chapter 5-10-00,Maintenance Planning Document, Standard Manufacturer’s Recommended ContinuousAirworthiness Inspection Program.

B. This section also includes:(1) Component Time Limit Tasks - Refer to Table 2 for Component Time Limits Tasks that have been

duplicated from Table 1 to assist operators in maintenance planning.(2) Baseline Corrosion Prevention and Control Program (CPCP) Tasks - Refer to Table 3 for

Corrosion Prevention and Control Program (CPCP) Tasks that have been duplicated from Table1 to assist operators with proper implementation of a CPCP.

(3) For details on how to properly implement a CPCP, refer to the Citation Standard PracticesManual, Chapter 51, Corrosion Prevention and Control Program - Description and Operation.

NOTE: Airplane washing is a key component of any CPCP. Washing removes corrosiveagents from the surface of the airplane.

NOTE: The wash schedule found in Chapter 5, MSG-3 Inspection Documents andOther Required Tasks, Table 4 Discretionary Maintenance is for airplanes thatoperate in mild to moderate corrosion areas. If an airplane flies into any SevereCorrosion Areas during its operation route, a more frequent wash schedule maybe required. Refer to the Citation Standard Practices Manual, Chapter 20, Exterior- Cleaning/Washing/Rinse - Servicing and Chapter 51, Corrosion Prevention andControl Program - Description and Operation for more information.

NOTE: Textron Aviation strongly recommends washing or rinsing the airplane as soon aspossible, no later than three days, after any operation that exposes the airplaneto Runway De-Icing (RDI) fluids. Any delay can result in the greater likelihoodof corrosion.

NOTE: Operators can refer to the exterior cleaning procedures in the Citation StandardPractices Manual, Chapter 20, Exterior - Cleaning/Washing/Rinse - Servicing.Operators can refer to the Citation Standard Practices Manual, Chapter 51,Corrosion - Description and Operation and the Corrosion Severity Maps can befound in the Citation Standard Practices Manual, Chapter 51, Corrosion SeverityMaps - Description and Operation.

C. Table 1 MSG-3 Inspection Tasks gives a list of all the inspection and servicing requirements that mustbe completed for the Model 700 MSG-3 Inspection Program. Table 1 has columns for MaintenanceManual Task, Task Title, Interval/Note(s), Inspection Document, Zone, and Effectivity.(1) The Maintenance Manual Task column gives the task number in chapter order.(2) The Task Title column gives the title of the related task.(3) The Interval/Note(s) column gives the minimum frequency at which the scheduled Task must

be completed. As each operator establishes their inspection program, these intervals must beobeyed.

(4) The Inspection Document column gives the inspection document for where the relatedMaintenance Manual Task is contained.

(5) The Zone column gives a reference to the physical location(s) on the airplane that is related tothe scheduled Task. Some operational and functional checks do not list a zone, but list a codethat is related to special conditions required to perform the task. These codes are: ENG, AUX,BAT, LAB, and FLT.• ENG - One or both airplane engines necessary to be running.

5-10-01 Page 1© TEXTRON AVIATION INC. Sep 26/2019

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• AUX - External source of electrical, hydraulic, pneumatic power, or a combination of these.Airplane engine power sources should not be used for these tests. It is possible to performmany of the tests in the AUX code with the airplane's battery power. However, it is notrecommended due to the power drain on the batteries.

• BAT - These tests must be performed with the component operated by the airplane’sbatteries or the batteries built into the individual component in the case of the ELT or othercomponents with internal battery power.

• LAB - Used when special equipment requires that the component be removed from theairplane and taken to a place equipped to perform the check or calibration.

• FLT - Test is to be performed during a flight.

D. The MM task numbers are hyperlinked to task details in this manual. The Zone number(s) are alsohyperlinked to Chapter 6, Airplane Zoning - Description and Operation to assist in planning andcompleting the tasks.

E. For operators developing a Custom Continuous Airworthiness Inspection Program, it may be helpfulto refer to the following sections for a correlation between the MRBR Task Numbers and MM TaskNumbers.

NOTE: The tasks referenced in the following sections are duplicates of tasks listed in Chapter5-10-01, MSG-3 Inspection Time Limits. However, the following sections organize thetask data in a format similar to the MRBR along with the corresponding MaintenanceManual Task - to - MRBR Task(s) and other useful information to assist operators indeveloping and/or optimizing a Custom Continuous Airworthiness Inspection Program.

(1) Chapter 5-10-01, MSG-3 Inspection Time Limits(a) Chapter 5-10-02, Systems, APU, and Powerplant Inspection Tasks(b) Chapter 5-10-03, Structures Inspection Tasks(c) Chapter 5-10-04, Zonal Inspection Tasks(d) Chapter 5-10-05, Enhanced Zonal Analysis Procedure (EZAP) Inspection Tasks(e) Chapter 5-10-06, Lightning/High Intensity Radiated Fields (L/HIRF) Inspection Tasks

(2) Chapter 5-12-00, MSG-3 Inspection Documents and Other Required Tasks(3) Chapter 5-13-00, Regulatory Inspections/Time Limits(4) Chapter 5-14-00, Airworthiness Directives(5) Chapter 5-15-00, Instructions for Continued Airworthiness (ICA) Supplements(6) Chapter 5-16-00, Supplemental Type Certificates (STC)(7) Chapter 5-17-00, Service Letters and Service Bulletins(8) Chapter 5-18-00, Supplier Information(9) Chapter 5-19-00, Discretionary Maintenance(10) Chapter 5-50-00, Unscheduled Maintenance Checks

2. MSG-3 Inspection Tasks

NOTE: All initial intervals are repeat intervals unless otherwise noted.

Table 1. MSG-3 Inspection Tasks

MSG-3 Inspection TasksMaintenanceManual Task Task Title Interval/

Note(s)InspectionDocument Zone Effectiv-

ityChapter 12 - Servicing

12-20-10-610 Main Landing Gear Oleo AssemblyServicing

2400FlightHours

5-12-08 721, 722 -0001 andOn

12-20-10-611 Nose Landing Shock Strut Servicing2400FlightHours

5-12-08 711 -0001 andOn


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Table 1. MSG-3 Inspection Tasks (continued)MSG-3 Inspection Tasks

MaintenanceManual Task Task Title Interval/


ity

12-20-10-612 Landing Gear Lubrication 18 Months 5-12-01 711, 712,723, 724

-0001 andOn

12-20-25-640 Key Lock Lubrication 18 Months 5-12-01

152, 313,314, 541,641, 811,831, 861,

862

-0001 andOn

12-20-30-640 Flap Actuation System Lubrication 36 Months 5-12-05513, 532,613, 632,723, 724

-0001 andOn

12-20-30-641 Horizontal Stabilizer Trim SystemLubrication 18 Months 5-12-01 348 -0001 and

On

12-20-30-642 Outboard Aileron ControlComponents Lubrication 36 Months 5-12-05 542,642 -0001 and

On

Chapter 21 - Air Conditioning

21-20-00-290Conditioned Air Pressure VesselCheck Valves (Borescope) SpecialDetailed Inspection

36 Months 5-12-05 365, 367 -0001 andOn

21-30-00-710

Manual Pressurization OperationalCheck

NOTE:An Equivalent CertificationMaintenance Requirement existsthat may require a different interval.

800 FlightHoursNOTE

5-12-02 233, 234 -0001 andOn

21-30-00-720

Pressurization Control SystemFunctional Check


1600FlightHoursNOTE

5-12-04 188, 282 -0001 andOn

21-30-00-721

Recirculation Shutoff FunctionalCheck


1600FlightHoursNOTE

5-12-04 282, 283 -0001 andOn

21-70-00-160 Ozone Converter (Cleaning)Restoration

6600FlightHours

5-12-17 365, 367 -0001 andOn


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ity

21-70-00-960 HEPA Filter Discard2400FlightHours

5-12-08 282 -0001 andOn

Chapter 23 - Communications

23-60-00-720 Static Discharge System FunctionalCheck 72 Months 5-12-13

343, 351,352, 542,551, 642,

651

-0001 andOn

23-70-00-710

Cockpit Voice Recorder UnderwaterLocator Beacon (Ping Test)Operational Check

NOTE:Per Supplier Recommendation.Reference Dukane Seacom03-TM-0037 Technical ManualUnderwater Acoustic Beacon.

24 MonthsNOTE 5-12-03 366 -0001 and

On

23-70-00-960 Cockpit Voice Recorder UnderwaterLocator Beacon Battery Discard

Compo-nent Ex-pirationDate

Refer toChapter5-12-00,Table 2

366 -0001 andOn

Chapter 24 - Electrical Power

24-30-00-210

Lithium-Ion Battery General VisualInspection

NOTE:Per supplier recommendation. TrueBlue Power Installation Manualand Operating Instructions ManualNumber 9018041

18 Months 5-12-01 311, 312 -0001 andOn

24-30-00-720

Marathon Nickel-Cadmium Battery(Capacity) Functional Check (IfInstalled)

NOTE:Per supplier recommendation.MarathonNorco AerospaceComponent Maintenance ManualDCR59577

800 FlightHoursor 18Months,WhicheverOccursFirst

5-12-20 311, 312 -0001 andOn

24-30-00-721

Standby Battery (Capacity)Functional Check

NOTE:Per supplier recommendation.Securaplane ComponentMaintenance Manual MM-0070-01

54 MonthsThen

Every 18Months

ThereafterUntil

Battery isReplaced

5-12-22 215 -0001 andOn


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ity

24-30-00-722

Lithium-Ion Battery (Capacity)Functional Check

NOTE:Per supplier recommendation. TrueBlue Power Installation Manualand Operating Instructions ManualNumber 9018041

36 Months 5-12-21 311, 312 -0001 andOn

24-30-00-910

Engine Direct-Current Generator(Bearing Replacement) Restoration

NOTE:You may contact Textron AviationParts Department (TAPD) at316-517-6002 for assistance withobtaining a properly restored EngineDirect-Current Generator and/orreference Component MaintenanceManual with Illustrated Parts List DCGenerator (Main)

3,200FlightHoursor 60Months,WhicheverOccursFirstNOTE


415, 416 -0001 andOn

24-30-00-911

Auxiliary Power Unit Direct-CurrentGenerator (Bearing Replacement)Restoration

NOTE:You may contact Textron AviationParts Department (TAPD) at316-517-6002 for assistance withobtaining a properly restored APUDirect-Current Generator and/orreference Component MaintenanceManual with Illustrated Parts List DCGenerator (APU)

3,200FlightHoursor 60Months,WhicheverOccursFirstNOTE


332 -0001 andOn

Chapter 25 - Equipment/Furnishings

25-10-00-220 Crew Seat, Seat Rail, and SeatRestraint Detailed Inspection

2400FlightHours

5-12-08 233, 234 -0001 andOn

25-10-00-221Observer/Jump Seat, CarriagePlate, Seat Rail, and Seat RestraintDetailed Inspection (If Installed)

54 Months 5-12-11 241 -0001 andOn

25-20-00-210

Inflatable Occupant ProtectionSystem Component General VisualInspection

NOTE:Per Supplier Recommendation.Reference Aviation OccupantSafety 01.01.00.03 ComponentMaintenance Manual.

18 MonthsNOTE 5-12-01 242, 267,

275-0001 and

On


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ity

25-20-00-220Passenger Seat, Seat AttachmentFitting and Seat Restraint DetailedInspection

54 Months 5-12-11251, 252,267, 268,275, 276

-0001 andOn

25-20-00-221Side Facing Couch Frame Assembly,Couch Attachment Fitting and CouchRestraint Detailed Inspection (IfInstalled)

54 Months 5-12-11 242, 267,275

-0001 andOn

25-20-00-710

Inflatable Occupant ProtectionSystem Operational Check


18 MonthsNOTE 5-12-01 AUX, 242,

267, 275-0001 and

On

25-20-00-960

Inflatable Occupant ProtectionSystem Component Discard


120MonthsTrackedby Com-ponentManufac-ture DateNOTE


242, 267,275

-0001 andOn

25-60-00-221

Emergency Locator TransmitterAntenna Detailed Inspection

NOTE:National Requirements may existwith a different interval. Per SupplierRecommendation. ReferenceARTEX Y1-03-0333 ComponentMaintenance Manual.

72 MonthsNOTE 5-12-13 362 -0001 and

On

25-60-00-720

Artex ELT-4000 Transmitter DetailedInspection and Functional Check

NOTE:National Requirements may existwith a different interval. Per SupplierRecommendation. ReferenceARTEX Y1-03-0333 ComponentMaintenance Manual.

12 MonthsNOTE 5-13-00 226, 362,

366-0001 and

On

25-60-00-960 Emergency Locator TransmitterBattery Discard



366 -0001 andOn


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ity

25-61-00-210

Model FA-AV(SA) Life Raft VisualCheck (If Installed)

NOTE:Per Supplier Recommendation.Life Raft Visual Check is to beaccomplished by an authorizedWinslow Life Raft Service Station.Reference Winslow Doc NoMFG-526/RS-457

36 MonthsTrackedby Com-ponentManufac-ture DateNOTE


200 -0001 andOn

25-61-00-211

Model FA-AV(SA) Life Raft GeneralVisual Inspection (If Installed)

NOTE:Per Supplier Recommendation.Reference Winslow Doc NoMFG-526/RS-457



200 -0001 andOn

25-61-00-220 Emergency Equipment DetailedInspection 18 Months 5-12-01 200, 233,

234-0001 and

On

25-61-00-221 Personal Flotation Device StoragePouch Detailed Inspection 54 Months 5-12-11

233, 234,242, 251,252, 267,268, 275,276, 282

-0001 andOn

25-61-00-222 Water Barrier Detailed Inspection 36 Months 5-12-05 241 -0001 andOn

25-61-00-720

Model FA-AV(SA) Life Raft(Hydrostatic) Functional Check (IfInstalled)

NOTE:Per Supplier Recommendation.Life Raft (Hydrostatic) FunctionalCheck is to be accomplished by anauthorized Winslow Life Raft ServiceStation. Reference Winslow Doc NoMFG-526/RS-457



200 -0001 andOn

25-61-00-910

P07074-207 Personal FlotationDevice (Accomplish Supplier 120Month Maintenance Inspection)Restoration

NOTE:You may contact Textron AviationParts Department (TAPD) at316-517-6002 for assistance withobtaining a properly restoredPersonal Flotation Device

120MonthsTrackedby Man-ufac-

ture DateNOTE


233, 234,242, 251,252, 267,268, 275,276, 282

-0001 andOn


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ityChapter 26 - Fire Protection

26-10-00-210 Engine Nacelle Fire DetectorsGeneral Visual Inspection 36 Months 5-12-05 415, 416 -0001 and

On

26-11-00-210 Auxiliary Power Unit Fire DetectorLoop General Visual Inspection 72 Months 5-12-13 332 -0001 and

On

26-20-00-220 Engine Fire Deployment Check TeeSpecial Detailed Inspection

AnytimeBottle 1and/or 2EngineFire Ex-tinguisheris Dis-charged

Chapter5-50-00 365, 366 -0001 and

On

26-20-00-710 Engine Fire Extinguishing SystemOperational Check

800 FlightHoursNOTE

5-12-02173, 174,233, 234,317, 318,365, 366

-0001 andOn

26-20-00-720

Engine Fire Extinguishing Bottle LowPressure Switch Functional Check

NOTE:This Task is Accomplished Duringthe Hydrostatic Check. Per SupplierRecommendation MASS Systems26-22-02 Component MaintenanceManual and Supplement 26-22-02FX04900-1 Fire Extinguisher, DualOutlet.

Coincidewith Hy-drostaticTest (if ap-plicable)not to Ex-ceed 60MonthsNOTE


365, 366 -0001 andOn

26-20-00-960

CT03200-1 and CT03300-1 EngineFire Bottle Cartridge (Squib) Discard

NOTE:Per Supplier Recommendation. Themaximum service life of the cartridgeinstalled is 144 Months. The totallife of the cartridge including shelflife is 180 Months. Reference MASSSystems 26-22-02 ComponentMaintenance Manual.

144MonthsTrackedby Com-ponent In-stallationDate


365, 366 -0001 andOn

26-21-00-710Auxiliary Power Unit FireExtinguishing System OperationalCheck

800 FlightHours 5-12-02 174, 225,

365, 366-0001 and

On


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ity

26-21-00-720

Auxiliary Power Unit FireExtinguishing Bottle Low PressureSwitch Functional Check

NOTE:This Task is Accomplished Duringthe Hydrostatic Check. Per SupplierRecommendation MASS Systems26-22-02 Component MaintenanceManual and Supplement 26-22-02FX05000-1 Fire Extinguisher, DualOutlet.

Coincidewith Hy-drostaticTest (if ap-plicable)not to Ex-ceed 60MonthsNOTE


365 -0001 andOn

26-21-00-960

CT03400-1 Auxiliary Power Unit FireBottle Cartridge (Squib) Discard


144MonthsTrackedby Com-ponent In-stallationDate


365 -0001 andOn

26-22-00-720 Portable Fire Extinguisher (WeightCheck) Functional Check 12 Months 5-13-00 234, 275 -0001 and

On

Chapter 27 - Flight Controls

27-10-00-220 Aileron Control System DetailedInspection

2400FlightHours

5-12-08

131, 132,175, 176,515, 534,544, 615,634, 644

-0001 andOn

27-10-00-720 Aileron Control System (Tension)Functional Check

2400FlightHours

5-12-08 131, 132,515, 615

-0001 andOn

27-10-00-721 Aileron Servo Tab (Free Play)Functional Check

2400FlightHours

5-12-08 544, 644 -0001 andOn

27-12-00-710 Pitch/Roll Disconnect SystemOperational Check

2400FlightHours

5-12-08 131, 132,225, 234

-0001 andOn

27-20-00-210Rudder Control System Structure(Cockpit Section Above Floor)General Visual Inspection

96 Months 5-12-16 233, 234 -0001 andOn

27-20-00-220 Cockpit Rudder Control SystemDetailed Inspection

2400FlightHours

5-12-08 233, 234 -0001 andOn


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27-20-00-221 Rudder Assembly DetailedInspection

2400FlightHours

5-12-08 343 -0001 andOn

27-30-00-220

Horizontal Stabilizer Rear Sparand Cove Section Structureand Corrosion Special DetailedInspection

NOTE:This is a CPCP Task

18 Months 5-12-01 351, 352 -0001 andOn

27-30-00-221 Elevator Servo Tab ActuatorStructure Detailed Inspection 72 Months 5-12-13 351, 352,

353, 354-0001 and

On

27-30-00-222 Elevator System Detailed Inspection2400FlightHours

5-12-08

131, 132,141, 142,153, 154,163, 164,175, 176,185, 186,346, 348,351, 352,365, 366,367, 368

-0001 andOn

27-30-00-720 Elevator System (Tension)Functional Check

2400FlightHours

5-12-08

131, 132,141, 142,153, 154,163, 164,175, 176,185, 186,346, 365,

367

-0001 andOn

27-50-00-220 Flap Actuation System DetailedInspection 36 Months 5-12-05 513, 532,

613, 632-0001 and

On

Chapter 28 - Fuel

28-10-00-220 Fuel Panel and Fuel Panel SealDetailed Inspection 54 Months 5-12-11

161, 162,171, 172,512, 521,531, 541,612, 621,631, 641

-0001 andOn

28-40-00-710 Low Fuel Level Sensor OperationalCheck 54 Months 5-12-11 225 -0001 and

On

Chapter 29 - Hydraulic Power

29-10-00-210 Hydraulic System Ecology BottleGeneral Visual Inspection

2400FlightHours

5-12-08 318 -0001 andOn


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29-10-00-960 Hydraulic System Filters Discard2400FlightHours

5-12-08 317, 318 -0001 andOn

29-20-00-710 Rudder Standby System OperationalCheck 36 Months 5-12-05 332 -0001 and

On

Chapter 30 - Ice and Rain Protection

30-40-00-720Cockpit Windshield and SideWindowSurface Seal (Mist Spray) FunctionalCheck


5-12-15 231, 232 -0001 andOn

30-70-00-710 Heated Drains Operational Check 36 Months 5-12-05 162, 166,315, 317

-0001 andOn

Chapter 31 - Indicating/Recording System

31-30-00-710

Flight Data Recorder UnderwaterLocator Beacon (Ping Test)Operational Check (If Installed)


24 MonthsNOTE 5-12-03 365 -0001 and

On

31-30-00-960Flight Data Recorder UnderwaterLocator Beacon Battery Discard (IfInstalled)



365 -0001 andOn

Chapter 32 - Landing Gear

32-00-00-220Landing Gear and Doors BondingJumpers Standalone L/HIRFDetailed Inspection

36 Months 5-12-05 712, 723,724

-0001 andOn

32-10-00-210Main Landing Gear Wheel Well andLanding Gear Zonal General VisualInspection

72 Months 5-12-13 721, 722,723, 724

-0001 andOn

32-10-00-220

Main Landing Gear Assembly andWheel Well Structural and CorrosionDetailed Inspection


18 Months 5-12-01 721, 722,723, 724

-0001 andOn

32-10-00-221 Main Landing Gear DetailedInspection

6600FlightHours

5-12-17 721, 722,723, 724

-0001 andOn


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32-20-00-210Nose Wheel Well and NoseLanding Gear Zonal General VisualInspection

72 Months 5-12-13 711, 712 -0001 andOn

32-20-00-220

Nose Landing Gear Assembly andWheel Well Structural and CorrosionDetailed Inspection


18 Months 5-12-01 711, 712 -0001 andOn

32-20-00-221 Nose Landing Gear TrunnionAssembly Detailed Inspection

6600FlightHours

5-12-17 712 -0001 andOn

32-30-00-720Nose and Main Landing GearActuator (Lash Check) FunctionalCheck

6600FlightHours

5-12-17 712, 723,724

-0001 andOn

32-32-00-220Main Landing Gear EmergencyExtension Component DetailedInspection

36 Months 5-12-05 723, 724 -0001 andOn

32-32-00-710 Landing Gear Emergency ExtensionOperational Check 36 Months 5-12-05 229 -0001 and

On

32-40-00-220 Main Landing Gear Wheel and TireDetailed Inspection

Every TireChangeNot to

Exceed 36Months


721, 722 -0001 andOn

32-40-00-221 Nose Landing Gear Wheel and TireDetailed Inspection

Every TireChangeNot to

Exceed 36Months


711 -0001 andOn

32-40-00-280

Nose Landing Gear Wheel AssemblySpecial Detailed Inspection

NOTE:Per Supplier Recommendation.Reference BF Goodrich 32-47-43Component Maintenance Manual

Basedon TireChanges,Calendar

andLandingsNOTE


711 -0001 andOn

32-40-00-281

Main Landing Gear Wheel AssemblySpecial Detailed Inspection


Basedon TireChanges,Calendar

andLandingsNOTE


721, 722 -0001 andOn


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32-41-00-220 Main Landing Gear Brake AssemblyDetailed Inspection

EveryWheelRemoval


721, 722 -0001 andOn

32-41-00-720 Main Landing Gear Brake AssemblyWear Pin Functional Check

EveryWheelRemoval


AUX, 721,722

-0001 andOn

32-43-00-710 PARK BRAKE EICAS MessageOperational Check 36 Months 5-12-05 233 -0001 and

On

32-50-00-220 Nose Wheel Steering CableAssembly Detailed Inspection

3200FlightHours

5-12-12131, 132,233, 234,

712-0001 and

On

Chapter 33 - Lights

33-50-00-710LED Rechargeable FlashlightSystem Operational Check (IfInstalled)

18 Months 5-12-01 233, 234 -0001 andOn

33-50-00-720 Emergency Lighting SystemFunctional Check 36 Months 5-12-05 233, 234,

281, 282-0001 and

On

33-50-00-960 Crew Flashlight Batteries Discard (2D-cell Type)(If Installed) 18 Months 5-12-01 233, 234 -0001 and

On

Chapter 35 - Oxygen

35-10-00-220 Crew Oxygen Mask and StorageBox Detailed Inspection

800 FlightHours 5-12-02 235, 236 -0001 and

On

35-10-00-221 Oxygen Bottle Detailed Inspection 800 FlightHours 5-12-02 215, 216 -0001 and

On

35-10-00-222 Observer/Jump Seat Oxygen MaskDetailed Inspection (If Installed)

800 FlightHours 5-12-02 241 -0001 and

On

35-10-00-910

MC10-16-150 Crew Oxygen Mask(Accomplish Supplier Testing andFault Isolation Task) Restoration (IfInstalled)

NOTE:You may contact Textron AviationParts Department (TAPD) at316-517-6002 for assistance WithObtaining a Properly Restored CrewOxygen Mask and/or Reference35-13-63 Intertechnique AircraftSystems CMM with IPL CrewOxygen Mask Regulator

72 MonthsTrackedby Com-ponent

Time Lim-its NOTE


235, 236 -0001 andOn


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35-10-00-911

MLD20-505 Full Face Crew OxygenMask (Accomplish Supplier Testingand Fault Isolation Task) Restoration(If Installed)

NOTE:You may contact Textron AviationParts Department (TAPD) at316-517-6002 for assistance WithObtaining a Properly Restored FullFace Crew Oxygen Mask and/orReference EROS (Intertechnique)35-13-64 Component MaintenanceManual


Time Lim-its NOTE


235, 236 -0001 andOn

35-10-00-912

MC10-15-109 or MC10-16-101Observer/Jump Seat Oxygen Mask(Accomplish Supplier Testing andFault Isolation Task) Restoration (IfInstalled)



Time Lim-its NOTE


241, -0001 andOn

35-20-00-220 Passenger Oxygen Canister andMask Detailed Inspection

800 FlightHours 5-12-02

241, 242,251, 252,267, 268,275, 276

-0001 andOn

35-20-00-720 Passenger Oxygen SystemFunctional Check

800 FlightHours 5-12-02 227 -0001 and

On

35-30-00-210

Protective Breathing EquipmentGeneral Visual Inspection

NOTE:User Reference and ProceduresManual for the Essex CrewmemberPBE

18 MonthsNOTE 5-12-01 275 -0001 and

On

35-30-00-960

Protective Breathing EquipmentDiscard

NOTE:Per Supplier Recommendations.User Reference and ProceduresManual for the Essex CrewmemberPBE

Com-ponentExpira-tion DateNOTE


275 -0001 andOn


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ityChapter 38 - Water/Waste

38-10-00-160 Potable Water Storage Tank(Cleaning) Restoration 18 Months 5-12-01 273 -0001 and

On

38-10-00-961 Potable Water Cartridge FilterElement Discard

1600FlightHours

5-12-04 273 -0001 andOn

38-30-00-210Toilet Catch Pan and Waste Tubes(Borescope) Special DetailedInspection

24 Months 5-12-03175, 176,185, 186,276, 278,311, 312

-0001 andOn

Chapter 49 - Auxiliary Power Unit (APU)

49-10-00-220

Auxiliary Power Unit Igniter PlugsDetailed Inspection

NOTE:Reference Honeywell 49-24-09,36-150 [EMB] APU Inspection/RepairManual

1500 APUHoursNOTE


332 -0001 andOn

49-10-00-221

Auxiliary Power Unit Starter MotorBrushes Detailed Inspection

NOTE:Reference Honeywell ServiceInformation Letter D201608000071

1500 APUHoursNOTE


332 -0001 andOn

49-10-00-222

Auxiliary Power Unit Magnetic ChipCollector Detailed Inspection

NOTE:Reference Honeywell 49-24-86,36-150 [EMB] APU LightMaintenance Manual

750 APUHoursNOTE


332 -0001 andOn

49-10-00-960

Auxiliary Power Unit CompressorRotor Discard

NOTE:Reference Honeywell 49- 24-87,36-150 [EMB] APU ComponentMaintenance Manual

20,000APUCyclesNOTE


332 -0001 andOn

49-10-00-961

Auxiliary Power Unit Turbine RotorDiscard


10,000APUCyclesNOTE


332 -0001 andOn


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49-10-00-962

Auxiliary Power Unit Fuel FilterDiscard


1500 APUHoursNOTE


332 -0001 andOn

49-10-00-963

Auxiliary Power Unit Oil Filter Discard


750 APUHoursNOTE


332 -0001 andOn

49-10-00-964

Auxiliary Power Unit Oil Discard


750 APUHoursNOTE


332 -0001 andOn

Chapter 52 - Doors

52-10-00-210 Cabin Door Seal General VisualInspection 18 Months 5-12-01 812 -0001 and

On

52-10-00-220 Cabin Entry Door Internal DetailedInspection 72 Months 5-12-13 811 -0001 and

On

52-10-00-221 Cabin Door Detailed Inspection3200FlightHours

5-12-12 811, 812 -0001 andOn

52-10-00-720 Cabin Door Gas Strut FunctionalCheck

800 FlightHours 5-12-02 812 -0001 and

On

52-10-00-721 Cabin Door Locking FunctionalCheck

3200FlightHours

5-12-12 812 -0001 andOn

52-20-00-220 Emergency Exit Door DetailedInspection 72 Months 5-12-13 822, 823 -0001 and

On

52-20-00-710 Emergency Exit Door OperationalCheck 24 Months 5-12-03 225, 822,

823-0001 and

On

52-30-00-210 Baggage Door Internal GeneralVisual Inspection 72 Months 5-12-13 832 -0001 and

On

52-30-00-211 Baggage Door Seal General VisualInspection 96 Months 5-12-16 831 -0001 and

On

52-30-00-220 Baggage Door CounterbalanceCable Detailed Inspection

2400FlightHours

5-12-08 281 -0001 andOn


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52-80-00-210Landing Gear Doors andComponents General VisualInspection

2400FlightHours

5-12-08711, 712,721, 722,723, 724

-0001 andOn

Chapter 53 - Fuselage

53-00-00-210 Fuselage External Zonal GeneralVisual Inspection 72 months 5-12-13

111, 137,138,

147, 148,213, 214,231, 232,243, 244,253, 254,263, 264,273, 274,283, 284,331,361,362, 363,364, 811,822, 831,861, 862

-0001 andOn

53-00-00-250 Fuselage Skin Splices (EddyCurrent) Special Detailed Inspection

7200FlightHours

5-12-25

213, 214,231, 232,243, 244,253, 254,263, 264,273, 274,283, 284,

-0001 andOn

53-10-00-210Nose Section Internal ZonalStandalone EZAP General VisualInspection

72 Months 5-12-13112, 215,216, 851,

852-0001 and

On

53-10-00-211 Nose Section Standalone EZAP(Cleaning) Restoration 96 Months 5-12-16 215, 216 -0001 and

On

53-20-00-210Lower Cockpit Internal ZonalStandalone EZAP General VisualInspection

72 Months 5-12-13 131, 132 -0001 andOn

53-20-00-211Upper Cockpit, Forward and MidCabin Internal Zonal StandaloneEZAP General Visual Inspection

180Months 5-12-18

233, 234,241, 242,251, 252,267, 268,275, 276,812, 823

-0001 andOn

53-20-00-212Lower Cabin Internal ZonalStandalone EZAP General VisualInspection

72 Months 5-12-13

141, 142,153, 154,163, 164,175, 176,191, 192,193, 194

-0001 andOn


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53-20-00-213Baggage Compartment UpperInternal Zonal Standalone EZAPGeneral Visual Inspection

96 Months 5-12-16 281, 282,832

-0001 andOn

53-20-00-214Baggage Compartment LowerInternal Zonal Standalone EZAPGeneral Visual Inspection

96 Months 5-12-16 185, 186 -0001 andOn

53-20-00-215Cockpit Control Wheel and OverheadPanel Internal Zonal StandaloneEZAP General Visual Inspection

180Months 5-12-18

221, 222,223, 224,225, 226,227, 228,229, 235,236, 237,238, 239

-0001 andOn

53-20-00-216Lower Cockpit Main Cabin WireBundle and Electrical ComponentStandalone EZAP (Cleaning)Restoration

72 Months 5-12-13 131, 132 -0001 andOn

53-20-00-217Upper Cockpit Wiring and ElectricalComponent Standalone EZAP(Cleaning) Restoration

180Months 5-12-18

233, 234,241, 812,

823-0001 and

On

53-20-00-218Lower Cabin Wire BundleStandalone EZAP (Cleaning)Restoration

72 Months 5-12-13

141, 142,153, 154,163, 164,175, 176,192, 193,

194

-0001 andOn

53-20-00-219Aft Cabin and Baggage DoorStandalone EZAP (Cleaning)Restoration

96 Months 5-12-16 281, 282,832

-0001 andOn

53-20-00-2110 Aft Cabin Lower Standalone EZAP(Cleaning) Restoration 96 Months 5-12-16 185, 186 -0001 and

On

53-20-00-2111Cockpit Control Panel and PedestalStandalone EZAP (Cleaning)Restoration

180Months 5-12-18

221, 222,223, 224,225, 226,227, 228,229, 235,

236

-0001 andOn

53-20-00-220Fuselage to Wing Attachments(Borescope) Special DetailedInspection

72 Months 5-12-13166, 167,177, 178,261, 262,271, 272

-0001 andOn

53-30-00-210 Tailcone Internal Zonal StandaloneEZAP General Visual Inspection 72 Months 5-12-13

365,366,367,368,842

-0001 andOn

53-30-00-211 Stinger Internal Standalone EZAP(Cleaning) Restoration 72 Months 5-12-13 332 -0001 and

On


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53-30-00-212 Tailcone Internal Standalone EZAP(Cleaning) Restoration 72 Months 5-12-13 367, 368 -0001 and

On

53-40-00-210Fairings Internal and Lower CabinSkins External Zonal StandaloneEZAP General Visual Inspection

72 Months 5-12-13

135, 136,137, 138,146, 147,157, 158,167, 168,173, 174,177, 178,187, 188,311, 312,317, 318,323, 324

-0001 andOn

53-40-00-212Fuselage Fairing and TailconeAccess Door External Zonal GeneralVisual Inspection

72 Months 5-12-13

133, 134,143, 144,151, 152,161, 162,171, 172,261, 262,271, 272,313, 314,315, 316,321, 322,

841

-0001 andOn

53-40-00-213 Fairing Internal Standalone EZAP(Cleaning) Restoration 72 Months 5-12-13

145, 155,156, 165,166, 173,174, 265,266, 278,279, 311,312, 317,318, 323,

324

-0001 andOn

Chapter 54 - Pylons

54-50-00-210Cowling and Pylon InternalStandalone EZAP (Cleaning)Restoration

36 Months 5-12-05 415, 416,417, 418

-0001 andOn

54-50-00-220 Engine Mounts Detailed Inspection 96 Months 5-12-16 417, 418 -0001 andOn

Chapter 55 - Stabilizers

55-00-00-210Vertical and Horizontal StabilizerExternal Zonal General VisualInspection

72 Months 5-12-13341, 342,343, 344,351, 352

-0001 andOn

55-10-00-210 Horizontal Leading Edge InternalZonal General Visual Inspection 96 Months 5-12-16 353, 354 -0001 and

On


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55-10-00-221Horizontal Stabilizer, Internal(Borescope) Special DetailedInspection

180Months 5-12-18 353, 354 -0001 and

On

55-20-00-221Elevator and Elevator ServoTabs Non-Metallic Parts DetailedInspection

72 Months 5-12-13 351, 352 -0001 andOn

55-30-00-210 Vertical Tail Internal Zonal GeneralVisual Inspection 72 Months 5-12-13 345, 346,

348-0001 and

On

55-30-00-220

Vertical Stabilizer Rear Spar andCove Structural and Corrosion(Borescope) Special DetailedInspection


18 Months 5-12-01 342 -0001 andOn

55-40-00-221 Rudder Non-Metallic Parts DetailedInspection 72 Months 5-12-13 343 -0001 and

On

Chapter 56 - Windows

56-10-00-220 Cockpit and Passenger WindowsExternal Detailed Inspection 36 Months 5-12-05

231, 232,253, 254,263, 264,273, 274

-0001 andOn

56-10-00-221 Windshield Assembly Hump SealDetailed Inspection


5-12-15 231, 232 -0001 andOn

56-10-00-720 Windshield Assembly FastenerTorque Functional Check

2400FlightHours

5-12-08 231, 232 -0001 andOn

Chapter 57 - Wings

57-20-00-210 Wing Internal Zonal General VisualInspection 54 Months 5-12-11

514, 516,522, 533,543, 552,614, 616,622, 633,643, 652

-0001 andOn


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57-20-00-211 Wing External Zonal General VisualInspection 72 Months 5-12-13

511, 512,513, 521,531, 532,541, 542,551, 611,612, 613,621, 631,632, 641,642, 651

-0001 andOn

57-20-00-220

Left and Right Wing Rear Spar andControl Surface AttachmentsStructural and Corrosion(Borescope) Special DetailedInspection


18 Months 5-12-01513, 532,542, 613,632, 642

-0001 andOn

57-20-00-221 Wing Internal Detailed Inspection 54 Months 5-12-11

514, 515,522, 533,534, 543,544, 552,614, 615,622, 633,634, 644,

652

-0001 andOn

57-20-00-222Wing Internal Fuel MonitoringWiring Standalone EZAP DetailedInspection

54 Months 5-12-11514, 522,533, 543,614, 622,633, 643

-0001 andOn

57-50-00-220 Flap Assembly Special DetailedInspection 36 Months 5-12-05 513, 532,

613, 632-0001 and

On

57-60-00-221 Aileron Non-Metallic Parts DetailedInspection 72 Months 5-12-13 532, 542,

632, 642-0001 and

On

57-70-00-221 Spoilers Non-Metallic Parts DetailedInspection 72 Months 5-12-13 513, 532,

613, 632-0001 and

On

Chapter 71 - Power Plant

71-00-00-210Pylon and Cowling Internal ZonalStandalone EZAP General VisualInspection

36 Months 5-12-05 415, 416,417, 418

-0001 andOn

71-00-00-211 Engine Pylon and Cowling ExternalZonal General Visual Inspection 96 Months 5-12-16 411, 412,

413, 414-0001 and

On

71-00-00-212 Engine Nacelle Fire Seals andFirewall General Visual Inspection 54 Months 5-12-11 415, 416 -0001 and

On

Chapter 72 - Engine


ICA-700-25-00001 Form 2261 Rev 1

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Refer toHoneywellAerospace72-05-25

Engine LightMaintenance

Manual

Honeywell Engine PeriodicInspections

NOTE:Refer to Honeywell Aerospace72-05-25 Engine Light MaintenanceManual Chapter 5-20-00.

EngineHours orCyclesNOTE

Refer toChapter5-10-02 orHoneywellAerospace72-05-25Engine

Light Main-tenanceManual

415, 416 -0001 andOn

Chapter 78 - Exhaust

78-30-00-220 Thrust Reverser Assembly DetailedInspection

3200FlightHours

5-12-12 411, 412 -0001 andOn

NOTE 1: Components which have exceeded replacement times due to a current change in the inspectionprogram, may continue in service, if the component is serviceable, and the component is immediatelyordered and scheduled for replacement. Possible delays resulting from component shortage shall notresult in extending time past 60 days.

3. Component Time Limit Tasks

NOTE: Table 2 is a consolidated list of component time limit tasks (duplicated from Table 1), to assistoperators in maintenance planning.

NOTE: Refer to the Model 700 Airworthiness Limitations Manual, Chapter 4, Airworthiness LimitationsInspection Time Limits for a list of the Airworthiness Component Time Limit Tasks.

Table 2. Component Time Limit Tasks

Component Time Limit TasksMaintenanceManual Task Task Title Interval/

Note(s)InspectionDocument Zone Effectivity

Chapter 21 - Air Conditioning21-70-00-960 HEPA Filter Discard 2400

FlightHours

5-12-08 282-0001 and

On

Chapter 23 - Communications23-70-00-960 Cockpit Voice Recorder Underwater

Locator Beacon Battery DiscardCompo-nent Ex-pirationDate


366-0001 and

On



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MAINTENANCE MANUAL

Table 2. Component Time Limit Tasks (continued)Component Time Limit Tasks



24-30-00-910 Engine Direct-Current Generator(Bearing Replacement) Restoration

NOTE:You may contact Textron AviationParts Department (TAPD) at316-517-6002 for assistance withobtaining a properly restored EngineDirect-Current Generator and/orreference Component MaintenanceManual with Illustrated Parts List DCGenerator (Main)

3200FlightHoursor 60Months,WhicheverOccursFirstNOTE


415, 416

-0001 andOn

24-30-00-911 Auxiliary Power Unit Direct-CurrentGenerator (Bearing Replacement)Restoration

NOTE:You may contact Textron AviationParts Department (TAPD) at316-517-6002 for assistance withobtaining a properly restored APUDirect-Current Generator and/orreference Component MaintenanceManual with Illustrated Parts List DCGenerator (APU)

3200FlightHoursor 60Months,WhicheverOccursFirstNOTE


332

-0001 andOn

Chapter 25 - Equipment/Furnishings25-20-00-960 Inflatable Occupant Protection

System Component Discard




242, 267,275

-0001 andOn

25-60-00-960 Emergency Locator TransmitterBattery Discard



366-0001 and

On

25-61-00-910 P07074-207 Personal FlotationDevice (Accomplish Supplier 120Month Maintenance Inspection)Restoration




233, 234,242, 251,252, 267,268, 275,276, 282

-0001 andOn


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Chapter 26 - Fire Protection26-20-00-960 CT03200-1 and CT03300-1 Engine

Fire Bottle Cartridge (Squib) Discard


144MonthsTrackedby Com-ponentInstalla-tion DateNOTE


365, 366

-0001 andOn

26-21-00-960 CT03400-1 Auxiliary Power Unit FireBottle Cartridge (Squib) Discard


144MonthsTrackedby Com-ponentInstalla-tion DateNOTE


365

-0001 andOn

Chapter 29 - Hydraulic Power29-10-00-960 Hydraulic System Filters Discard 2400

FlightHours

5-12-08 317, 318-0001 and

On

Chapter 31 - Indicating/Recording Systems31-30-00-960 Flight Data Recorder Underwater

Locator Beacon Battery Discard (IfInstalled)



365-0001 and

On

Chapter 33 - Lights33-50-00-960 Crew Flashlight Batteries Discard (2

D-cell Type)(If Installed) 18 Months 5-12-01 233, 234 -0001 andOn

Chapter 35 - Oxygen


ICA-700-25-00001 Form 2261 Rev 1

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35-10-00-910 MC10-16-150 Crew Oxygen Mask(Accomplish Supplier Testing andFault Isolation Task) Restoration (IfInstalled)

NOTE:You may contact Textron AviationParts Department (TAPD) at316-517-6002 for assistance WithObtaining a Properly Restored CrewOxygen Mask and/or Reference35-13-63 Intertechnique AircraftSystems CMM with IPL CrewOxygen Mask Regulator


Time Lim-its NOTE


235, 236

-0001 andOn

35-10-00-911 MLD20-505 Full Face Crew OxygenMask (Accomplish Supplier Testingand Fault Isolation Task) Restoration(If Installed)



Time Lim-its NOTE


235, 236

-0001 andOn

35-10-00-912 MC10-15-109 or MC10-16-101Observer/Jump Seat Oxygen Mask(Accomplish Supplier Testing andFault Isolation Task) Restoration (IfInstalled)



Time Lim-its NOTE


241,

-0001 andOn

35-30-00-960 Protective Breathing EquipmentDiscard

NOTE:Per Supplier Recommendations.User Reference and ProceduresManual for the Essex CrewmemberPBE

Com-ponentExpira-tion DateNOTE


275

-0001 andOn


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Chapter 38 - Water/Waste38-10-00-961 Portable Water Cartridge Filter

Element Discard

NOTE:Per Supplier Recommendation.Reference Adams Rite Aerospace38-14-19 Component MaintenanceManual

1600FlightHoursNOTE

5-12-04 273

-0001 andOn

Chapter 49 - Auxiliary Power Unit (APU)49-10-00-960 Auxiliary Power Unit Compressor

Rotor Discard

NOTE:Per Supplier Recommendation.Reference Honeywell 49- 24-87,36-150 [EMB] APU ComponentMaintenance Manual

20,000APUCyclesNOTE


332

-0001 andOn

49-10-00-961 Auxiliary Power Unit Turbine RotorDiscard


10,000APUCyclesNOTE


332

-0001 andOn

49-10-00-962 Auxiliary Power Unit Fuel FilterDiscard

NOTE:Reference Honeywell 49-24-86,36-150 [EMB] APU LightMaintenance Manual.

1500 APUHoursNOTE


332

-0001 andOn

49-10-00-963 Auxiliary Power Unit Oil Filter Discard


750 APUHoursNOTE


332

-0001 andOn

49-10-00-964 Auxiliary Power Unit Oil Discard


750 APUHoursNOTE


332

-0001 andOn

Chapter 72 - Engine


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL






Manual

Engine Nozzle, Fuel Injection-Start(Detailed Inspection and FunctionalCheck) Restoration

NOTE:The Engine Nozzle, FuelInjection-Start is not field serviceable.You may contact Textron AviationParts Department (TAPD) at316-517-6002 for assistance withobtaining a properly restoredEngine Nozzle, Fuel Injection-Startand/or reference 72-05-25 LightMaintenance Manual.

2000EngineHoursNOTE


415, 416

-0001 andOn



Manual

Engine Nozzle, Fuel Injection-HiTemp (Detailed Inspection andFunctional Check) Restoration

NOTE:The Engine Nozzle, Fuel Injection-HiTemp is not field serviceable.You may contact Textron AviationParts Department (TAPD) at316-517-6002 for assistance withobtaining a properly restored EngineNozzle, Fuel Injection-Hi Tempand/or reference 72-05-25 LightMaintenance Manual.

4000EngineHoursNOTE


415, 416

-0001 andOn



Manual

Engine High Pressure TurbineInterstage Rotating-Seal Discard

NOTE:Per Supplier Recommendation.Honeywell Aerospace 72-05-25 LightMaintenance Manual.

15,000EngineCyclesNOTE


415, 416

-0001 andOn


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL






Manual

Engine Seal Assembly HighPressure Turbine Stage 2 Discard

NOTE:Per Supplier Recommendation.Honeywell Aerospace 72-05-25 LightMaintenance Manual

15,000EngineCyclesNOTE


415, 416

-0001 andOn



Manual

Engine Oil Filter Element Discard

NOTE:Reference Honeywell Aerospace72-05-25 Light Maintenance Manual.

750EngineHoursNOTE


415, 416

-0001 andOn



Manual

Engine Fuel Filter Assembly Discard

NOTE:Per Supplier Recommendation.Honeywell Aerospace 72-05-25 LightMaintenance Manual.

4000EngineHoursNOTE


415, 416

-0001 andOn

4. Baseline Corrosion Prevention and Control Program (CPCP) Tasks

NOTE: Table 3 is a consolidated list of the Baseline CPCP tasks (duplicated from Table 1), to assistoperators in maintenance planning.

NOTE: All initial intervals are repeat intervals unless otherwise noted.


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL

Table 3. Baseline Corrosion Prevention and Control Program (CPCP) Tasks

Baseline Corrosion Prevention and Control Program (CPCP) TasksMaintenanceManual Task Task Title Interval/


27-30-00-220

Horizontal Stabilizer Rear Sparand Cove Section Structureand Corrosion Special DetailedInspection


18 Months 5-12-01 351, 352 -0001 andOn

32-10-00-220

Main Landing Gear Assembly andWheel Well Structural and CorrosionDetailed Inspection


18 Months 5-12-01 721, 722,723, 724

-0001 andOn

32-20-00-220

Nose Landing Gear Assembly andWheel Well Structural and CorrosionDetailed Inspection


18 Months 5-12-01 711, 712 -0001 andOn

55-30-00-220

Vertical Stabilizer Rear Spar andCove Structural and Corrosion(Borescope) Special DetailedInspection


18 Months 5-12-01 342, 343 -0001 andOn

57-20-00-220

Left and Right Wing Rear Spar andControl Surface AttachmentsStructural and Corrosion(Borescope) Special DetailedInspection


18 Months 5-12-01513, 532,542, 613,632, 642

-0001 andOn


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL

SYSTEMS, APU, AND POWERPLANT INSPECTION TASKS

1. Purpose and UseA. This section includes all MSG-3 scheduled maintenance tasks related to the airplane Systems, APU,

and Powerplants. Refer to Figure 1 for a Systems, APU, and Powerplant Inspection Task DataSample.

NOTE: It is not necessary for operators using the Standard Manufacturer’s RecommendedContinuous Airworthiness Inspection Program to refer to this section.

NOTE: The tasks referenced in this section are duplicates of tasks listed in Chapter 5-10-01,MSG-3 Inspection Time Limits. However, the following sections organize the task data ina format similar to the MRBR along with the corresponding Maintenance Manual Task # -to - MRBR Task #(s) and other useful information to assist operators in developing and/oroptimizing a Custom Continuous Airworthiness Inspection Program.

B. Table 1 provides a cross-reference of MM Task Numbers and associated MRBR Task Numbers. Table1 also provides:(1) Useful information, such as the effect category (Cat), which may require special consideration

if an operator desires to escalate an interval. Refer to Chapter 5-10-00, Maintenance PlanningDocument, Program Rules, Inspection Intervals, Task and Interval Changes or Deletions.

(2) A column for operators to record labors for each task, if desired.

NOTE: In some cases, the same MM task number is listed for multiple MRBR tasks. Thisis due to task grouping (combining multiple MRBR tasks into one MM task) thatoccurs at the MM task writing level.

Table 1. Maintenance Planning Document Model 700 Systems, APU, and Powerplant Inspection Tasks

Model 700 Systems, APU, and Power Plant Inspection Tasks

MM TaskNumber

MRBR TaskNumberReference

Task TitleTaskTyp-e

La-borHo-urs

CatInter-val/

Note(s)Effectiv-

ity

Chapter 12 - Servicing

12-20-10-610 32-10-00-604 Main Landing Gear Oleo

Assembly Servicing SVC 5, 62400FlightHours

-0001and On

12-20-10-611 32-20-00-602 Nose Landing Shock Strut

Servicing SVC 5, 62400FlightHours

-0001and On

12-20-10-612

32-10-00-601,32-10-00-602,32-10-00-603,32-20-00-601,32-30-00-601,32-30-00-602,32-30-00-603,32-30-00-604,32-30-00-605,32-30-00-606,52-80-00-601

Landing Gear Lubrication LUB 5, 6,8

18Months

-0001and On


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL

Table 1. Maintenance Planning Document Model 700 Systems, APU, and Powerplant Inspection Tasks(continued)


MM TaskNumber


Task TitleTaskTyp-e

La-borHo-urs

CatInter-val/

Note(s)Effectiv-

ity

12-20-25-640

28-10-00-601,52-10-00-601,52-40-00-601,52-30-00-601,28-10-00-702,52-30-00-202

Key Lock Lubrication LUB 9 18Months

-0001and On

12-20-30-640

27-50-00-201,27-50-00-601,27-50-00-602

Flap Actuation System Lubrication LUB 6 36Months

-0001and On

12-20-30-641 27-40-00-601 Horizontal Stabilizer Trim System

Lubrication LUB 5 18Months

-0001and On

12-20-30-642 27-10-00-601 Outboard Aileron Control

Components Lubrication LUB 6 36Months

-0001and On

Chapter 21 - Air Conditioning

21-20-00-290 21-20-00-201

Conditioned Air Pressure VesselCheck Valves (Borescope)Special Detailed Inspection

SDI 9 36Months

-0001and On

21-30-00-710

21-30-00-701,21-30-00-702

Manual PressurizationOperational Check

NOTE:An Equivalent CertificationMaintenance Requirement existsthat may require a differentinterval.

OPC 9800FlightHoursNOTE

-0001and On

21-30-00-720

21-30-00-704,21-30-00-703

Pressurization Control SystemFunctional Check


FNC 91600FlightHoursNOTE

-0001and On

21-30-00-721 21-30-00-705

Recirculation Shutoff FunctionalCheck


FNC 51600FlightHoursNOTE

-0001and On

21-70-00-160 21-70-00-901 Ozone Converter (Cleaning)

Restoration RST 96600FlightHours

-0001and On


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL



MM TaskNumber


Task TitleTaskTyp-e

La-borHo-urs

CatInter-val/

Note(s)Effectiv-

ity

21-70-00-960 21-70-00-902 HEPA Filter Discard DIS 9

2400FlightHours

-0001and On

Chapter 23 - Communications23-60-00-720

23-60-00-701,23-60-00-702

Static Discharge SystemFunctional Check FNC 9 72

Months-0001and On

23-70-00-710 23-70-00-701

Cockpit Voice RecorderUnderwater Locator Beacon(Ping Test) Operational Check


OPC 6 24Months

-0001and On

23-70-00-960 23-70-00-901

Cockpit Voice RecorderUnderwater Locator BeaconBattery Discard

DIS 9Compo-nent Ex-pirationDate

-0001and On


24-30-00-210 24-30-00-201

Lithium-Ion Battery GeneralVisual Inspection

NOTE:Per supplier recommendation.True Blue Power InstallationManual and OperatingInstructions Manual Number9018041

GVI 6 18Months

-0001and On

24-30-00-720 24-30-00-701

Marathon Nickel-CadmiumBattery (Capacity) FunctionalCheck (If Installed)

NOTE:Per supplier recommendation.MarathonNorco AerospaceComponent Maintenance ManualDCR59577

FNC 6

800FlightHoursor 18Months,Whic-heverOccursFirst

-0001and On


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL



MM TaskNumber


Task TitleTaskTyp-e

La-borHo-urs

CatInter-val/

Note(s)Effectiv-

ity

24-30-00-721 24-30-00-702

Standby Battery (Capacity)Functional Check

NOTE:Per supplier recommendation.Securaplane ComponentMaintenance ManualMM-0070-01

FNC 6

54Monthsthen Ev-ery 18MonthsThere-afterUntil

Batteryis Re-placed

-0001and On

24-30-00-722 24-30-00-703

Lithium-Ion Battery (Capacity)Functional Check

NOTE:Per supplier recommendation.True Blue Power InstallationManual and OperatingInstructions Manual Number9018041

FNC 6 36Months

-0001and On

24-30-00-910 24-30-00-901

Engine Direct-Current Generator(Bearing Replacement)Restoration

NOTE:You may contact Textron AviationParts Department (TAPD) at316-517-6002 for assistancewith obtaining a properlyrestored Engine Direct-CurrentGenerator and/or referenceComponent Maintenance Manualwith Illustrated Parts List DCGenerator (Main)

RST 6

3200FlightHoursor 60Months,Whic-heverOccursFirstNOTE

-0001and On


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL



MM TaskNumber


Task TitleTaskTyp-e

La-borHo-urs

CatInter-val/

Note(s)Effectiv-

ity

24-30-00-911 24-30-00-902

Auxiliary Power UnitDirect-Current Generator(Bearing Replacement)Restoration

NOTE:You may contact Textron AviationParts Department (TAPD) at316-517-6002 for assistancewith obtaining a properlyrestored APU Direct-CurrentGenerator and/or referenceComponent Maintenance Manualwith Illustrated Parts List DCGenerator (APU)

RST 6

3200FlightHoursor 60Months,Whic-heverOccursFirstNOTE

-0001and On


25-10-00-220

25-10-00-201,25-10-00-201,25-10-00-201

Crew Seat, Seat Rail, and SeatRestraint Detailed Inspection DET 5, 6,

8, 92400FlightHours

-0001and On

25-10-00-221

25-20-00-208,25-20-00-209,25-20-00-210,25-20-00-211,25-20-00-703

Observer/Jump Seat, CarriagePlate, Seat Rail, and SeatRestraint Detailed Inspection (IfInstalled)

DET 8 54Months

-0001and On

25-20-00-210

25-20-00-205,25-20-00-206,25-20-00-207

Inflatable Occupant ProtectionSystem Component GeneralVisual Inspection


GVI 818

MonthsNOTE

-0001and On

25-20-00-220

25-20-00-201,25-20-00-203,25-20-00-204

Passenger Seat, Seat AttachmentFitting and Seat Restraint DetailedInspection

DET 8 54Months

-0001and On

25-20-00-221

25-20-00-202,25-20-00-203,25-20-00-204,25-20-00-701

Side Facing Couch FrameAssembly, Couch AttachmentFitting and Couch RestraintDetailed Inspection (If Installed)

DET 8 54Months

-0001and On


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL



MM TaskNumber


Task TitleTaskTyp-e

La-borHo-urs

CatInter-val/

Note(s)Effectiv-

ity

25-20-00-710 25-20-00-702

Inflatable Occupant ProtectionSystem Operational Check


OPC 818

MonthsNOTE

-0001and On

25-20-00-960

25-20-00-901,25-20-00-902



DIS 8

120MonthsTrackedby Com-ponentManu-factureDateNOTE

-0001and On

25-60-00-221 25-60-00-202

Emergency Locator TransmitterAntenna Detailed Inspection

NOTE:National Requirements mayexist with a different interval.Per Supplier Recommendation.Reference ARTEX Y1-03-0333Component Maintenance Manual.

DET 872

MonthsNOTE

-0001and On

25-60-00-720

25-60-00-20125-60-00-701,25-60-00-702,25-60-00-703,25-60-00-704,25-60-00-705

Artex ELT-4000 TransmitterDetailed Inspection andFunctional Check

NOTE:National Requirements mayexist with a different interval.Per Supplier Recommendation.Reference ARTEX Y1-03-0333Component Maintenance Manual.

DETFNC 8

12MonthsNOTE

-0001and On

25-60-00-960 25-60-00-901 Emergency Locator Transmitter

Battery Discard DIS 8Compo-nent Ex-pirationDate

-0001and On


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL



MM TaskNumber


Task TitleTaskTyp-e

La-borHo-urs

CatInter-val/

Note(s)Effectiv-

ity

25-61-00-210 25-60-00-207


NOTE:Per Supplier Recommendation.Life Raft Visual Check is to beaccomplished by an authorizedWinslow Life Raft Service Station.Reference Winslow Doc NoMFG-526/RS-457

VCK 8


-0001and On

25-61-00-211 25-60-00-208

Model FA-AV(SA) Life RaftGeneral Visual Inspection (IfInstalled)

NOTE:Per Supplier Recommendation.Reference Winslow Doc NoMFG-526/RS-457

GVI 8


-0001and On

25-61-00-220

25-60-00-203,25-60-00-205

Emergency Equipment DetailedInspection DET 8 18

Months-0001and On

25-61-00-221 25-60-00-204 Personal Flotation Device Storage

Pouch Detailed Inspection DET 8 54Months

-0001and On

25-61-00-222 25-60-00-206 Water Barrier Detailed Inspection DET 9 36

Months-0001and On

25-61-00-720 25-60-00-706


NOTE:Per Supplier Recommendation.Life Raft (Hydrostatic) FunctionalCheck is to be accomplishedby an authorized WinslowLife Raft Service Station.Reference Winslow Doc NoMFG-526/RS-457

FNC 8


-0001and On


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL



MM TaskNumber


Task TitleTaskTyp-e

La-borHo-urs

CatInter-val/

Note(s)Effectiv-

ity

25-61-00-910 25-60-00-902



RST 8

120MonthsTrackedby Man-ufactureDateNOTE

-0001and On

Chapter 26 - Fire Protection

26-10-00-210

26-10-00-201,26-10-00-202,26-10-00-203

Engine Nacelle Fire DetectorsGeneral Visual Inspection GVI 6 36

Months-0001and On

26-11-00-210 26-10-00-204 Auxiliary Power Unit Fire Detector

Loop General Visual Inspection GVI 6 72Months

-0001and On

26-20-00-220Chapter5-50-00

26-20-00-201 Engine Fire Deployment CheckTee Special Detailed Inspection SDI 8

AnytimeBottle 1and/or 2EngineFireExtin-guisheris Dis-charged

-0001and On

26-20-00-710

26-20-00-701,26-20-00-702,26-20-00-703,26-20-00-704,26-20-00-708

Engine Fire Extinguishing SystemOperational Check OPC 8, 9

800FlightHoursNOTE

-0001and On

26-20-00-720 26-20-00-701

Engine Fire Extinguishing BottleLow Pressure Switch FunctionalCheck

NOTE:This Task is Accomplished Duringthe Hydrostatic Check. PerSupplier Recommendation MASSSystems 26-22-02 ComponentMaintenance Manual andSupplement 26-22-02 FX04900-1Fire Extinguisher, Dual Outlet.

FNC 9

Coin-cidewith

Hydro-staticTest (ifapplica-ble) notto Ex-ceed 60MonthsNOTE

-0001and On


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL



MM TaskNumber


Task TitleTaskTyp-e

La-borHo-urs

CatInter-val/

Note(s)Effectiv-

ity

26-20-00-960 26-20-00-901

CT03200-1 and CT03300-1Engine Fire Bottle Cartridge(Squib) Discard

NOTE:Per Supplier Recommendation.The service life of the cartridgeinstalled is 144 Months. The totallife of the cartridge including shelflife is 180 Months. ReferenceMASS Systems 26-22-02Component Maintenance Manual.

DIS 8

144MonthsTrackedby Com-ponentInstal-lationDate

-0001and On

26-21-00-710

26-20-00-705,26-20-00-706,26-20-00-707,26-20-00-709

Auxiliary Power Unit FireExtinguishing System OperationalCheck

OPC 8800FlightHours

-0001and On

26-21-00-720 26-20-00-711

Auxiliary Power Unit FireExtinguishing Bottle LowPressure Switch FunctionalCheck


FNC 8

Coin-cidewith

Hydro-staticTest (ifapplica-ble) notto Ex-ceed 60MonthsNOTE

-0001and On

26-21-00-960 26-20-00-902

CT03400-1 Auxiliary Power UnitFire Bottle Cartridge (Squib)Discard

NOTE:Per Supplier Recommendation.The service life of the cartridgeinstalled is 144 Months. The totallife of the cartridge including shelflife is 180 Months. ReferenceMASS Systems 26-22-02Component Maintenance Manual.

DIS 8

144MonthsTrackedby Com-ponentInstal-lationDate

-0001and On

26-22-00-720 26-20-00-712 Portable Fire Extinguisher

(Weight Check) Functional Check FNC 6 12Months

-0001and On

Chapter 27 - Flight Controls


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL



MM TaskNumber


Task TitleTaskTyp-e

La-borHo-urs

CatInter-val/

Note(s)Effectiv-

ity

27-10-00-220

27-10-00-201,27-10-00-202,27-10-00-203,27-10-00-204,27-10-00-205,27-10-00-206,27-10-00-208,27-10-00-209,27-10-00-210,27-10-00-211

Aileron Control System DetailedInspection DET 6

2400FlightHours

-0001and On

27-10-00-720

27-10-00-701,27-10-00-702,27-10-00-703

Aileron Control System (Tension)Functional Check FNC 6

2400FlightHours

-0001and On

27-10-00-721 27-10-00-708 Aileron Servo Tab (Free Play)

Functional Check FNC 62400FlightHours

-0001and On

27-12-00-710

27-10-00-704,27-10-00-705,27-10-00-706,27-30-00-701,27-30-00-702

Pitch/Roll Disconnect SystemOperational Check OPC 6, 8,

92400FlightHours

-0001and On

27-20-00-220

27-20-00-201,27-20-00-203

Cockpit Rudder Control SystemDetailed Inspection DET 6

2400FlightHours

-0001and On

27-20-00-221 27-20-00-202 Rudder Assembly Detailed

Inspection DET 62400FlightHours

-0001and On

27-30-00-222

27-30-00-201,27-30-00-203,27-30-00-204,27-30-00-205

Elevator System DetailedInspection DET 6, 7

2400FlightHours

-0001and On

27-30-00-720 27-30-00-703 Elevator System (Tension)

Functional Check FNC 6, 72400FlightHours

-0001and On

27-50-00-220 27-50-00-202 Flap Actuation System Detailed

Inspection DET 6 36Months

-0001and On

Chapter 28 - Fuel28-10-00-220

28-10-00-201,28-10-00-202

Fuel Panel and Fuel Panel SealDetailed Inspection DET 6 54

Months-0001and On

28-40-00-710 28-40-00-701 Low Fuel Level Sensor

Operational Check OPC 8 54Months

-0001and On

Chapter 29 - Hydraulic Power


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL



MM TaskNumber


Task TitleTaskTyp-e

La-borHo-urs

CatInter-val/

Note(s)Effectiv-

ity

29-10-00-210 29-10-00-201 Hydraulic System Ecology Bottle

General Visual Inspection GVI 92400FlightHours

-0001and On

29-10-00-960

29-10-00-901,29-10-00-902,29-10-00-903,29-10-00-904

Hydraulic System Filters Discard DIS 92400FlightHours

-0001and On

29-20-00-710

29-20-00-701,29-20-00-201

Rudder Standby SystemOperational Check OPC 9 36

Months-0001and On

Chapter 30 - Ice and Rain Protection

30-40-00-720

30-40-00-701,30-40-00-702

Cockpit Windshield and SideWindow Surface Seal (MistSpray) Functional Check

FNC 9


-0001and On

30-70-00-710

30-70-00-701,30-70-00-702 Heated Drains Operational Check OPC 9 36

Months-0001and On

Chapter 31 - Indicating/Recording Systems

31-30-00-710 31-30-00-701

Flight Data Recorder UnderwaterLocator Beacon (Ping Test)Operational Check (If Installed)


OPC 9 24Months

-0001and On

31-30-00-960 31-30-00-901

Flight Data Recorder UnderwaterLocator Beacon Battery Discard(If Installed)

DIS 9Compo-nent Ex-pirationDate

-0001and On


32-10-00-221

32-10-00-202,32-10-00-203,32-10-00-204

Main Landing Gear DetailedInspection DET 5

6600FlightHours

-0001and On

32-20-00-221 32-20-00-201 Nose Landing Gear Trunnion

Assembly Detailed Inspection DET 56600FlightHours

-0001and On


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL



MM TaskNumber


Task TitleTaskTyp-e

La-borHo-urs

CatInter-val/

Note(s)Effectiv-

ity

32-30-00-720

32-30-00-709,32-30-00-710

Nose and Main Landing GearActuator (Lash Check) FunctionalCheck

FNC 56600FlightHours

-0001and On

32-32-00-220

32-30-00-201,32-30-00-202

Main Landing Gear EmergencyExtension Component DetailedInspection

DET 8 36Months

-0001and On

32-32-00-710

32-30-00-701,32-30-00-702,32-30-00-703,32-30-00-704,32-30-00-705,32-30-00-706,32-30-00-707,32-30-00-708,32-30-00-711,32-30-00-712,32-30-00-713,32-30-00-714

Landing Gear EmergencyExtension Operational Check OPC 8 36

Months-0001and On

32-40-00-280 32-40-00-201

Nose Landing Gear WheelAssembly Special DetailedInspection


SDI 9

Basedon TireCha-nges,Calen-dar andLand-ingsNOTE

-0001and On

32-40-00-281 32-40-00-202

Main Landing Gear WheelAssembly Special DetailedInspection


SDI 9

Basedon TireCha-nges,Calen-dar andLand-ingsNOTE

-0001and On

32-41-00-220 32-40-00-203 Main Landing Gear Brake

Assembly Detailed Inspection DET 6EveryWheelRe-moval

-0001and On

32-41-00-720 32-40-00-701

Main Landing Gear BrakeAssembly Wear Pin FunctionalCheck

FNC 6EveryWheelRe-moval

-0001and On


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL



MM TaskNumber


Task TitleTaskTyp-e

La-borHo-urs

CatInter-val/

Note(s)Effectiv-

ity

32-43-00-710 32-40-00-702 PARK BRAKE EICAS Message

Operational Check OPC 8 36Months

-0001and On

32-50-00-220 32-50-00-201 Nose Wheel Steering Cable

Assembly Detailed Inspection DET 63200FlightHours

-0001and On

Chapter 33 - Lights

33-50-00-710 33-50-00-704

LED Rechargeable FlashlightSystem Operational Check (IfInstalled)

OPC 8 18Months

-0001and On

33-50-00-720

33-50-00-701,33-50-00-702,33-50-00-703

Emergency Lighting SystemFunctional Check FNC 8, 9 36

Months-0001and On

33-50-00-960 33-50-00-901 Crew Flashlight Batteries Discard

(2 D-cell Type)(If Installed) DIS 8 18Months

-0001and On

Chapter 35 - Oxygen

35-10-00-220

35-10-00-201,35-10-00-202

Crew Oxygen Mask and StorageBox Detailed Inspection DET 5

800FlightHours

-0001and On

35-10-00-221 35-10-00-204 Oxygen Bottle Detailed Inspection DET 5, 8

800FlightHours

-0001and On

35-10-00-222 35-10-00-205

Observer/Jump Seat OxygenMask Detailed Inspection (IfInstalled)

DET 5800FlightHours

-0001and On

35-10-00-910 35-10-00-901

MC10-16-150 CrewOxygenMask(Accomplish Supplier Testing andFault Isolation Task) Restoration(If Installed)

NOTE:You may contact Textron AviationParts Department (TAPD) at316-517-6002 for assistanceWith Obtaining a ProperlyRestored Crew Oxygen Maskand/or Reference 35-13-63Intertechnique Aircraft SystemsCMM with IPL Crew OxygenMask Regulator

RST 5

72MonthsTrackedby Com-ponentTimeLimitsNOTE

-0001and On


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL



MM TaskNumber


Task TitleTaskTyp-e

La-borHo-urs

CatInter-val/

Note(s)Effectiv-

ity

35-10-00-911 35-10-00-902

MLD20-505 Full Face CrewOxygen Mask (AccomplishSupplier Testing and FaultIsolation Task) Restoration (IfInstalled)

NOTE:You may contact Textron AviationParts Department (TAPD) at316-517-6002 for assistanceWith Obtaining a ProperlyRestored Full Face CrewOxygen Mask and/or ReferenceEROS (Intertechnique) 35-13-64Component Maintenance Manual

RST 5


-0001and On

35-10-00-912 35-10-00-903

MC10-15-109 or MC10-16-101Observer/Jump Seat OxygenMask (Accomplish SupplierTesting and Fault Isolation Task)Restoration (If Installed)


RST 5


-0001and On

35-20-00-220 35-10-00-203 Passenger Oxygen Canister and

Mask Detailed Inspection DET 8, 9800FlightHours

-0001and On

35-20-00-720

35-10-00-701,35-10-00-702,35-10-00-703,35-10-00-704,35-10-00-705,35-10-00-706,21-30-00-706

Passenger Oxygen SystemFunctional Check FNC 6, 8,

9800FlightHours

-0001and On

35-30-00-210 35-30-00-201

Protective Breathing EquipmentGeneral Visual Inspection

NOTE:User Reference and ProceduresManual for the EssexCrewmember PBE

GVI 818

MonthsNOTE

-0001and On


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MM TaskNumber


Task TitleTaskTyp-e

La-borHo-urs

CatInter-val/

Note(s)Effectiv-

ity

35-30-00-960 35-30-00-901


NOTE:Per Supplier Recommendations.User Reference and ProceduresManual for the EssexCrewmember PBE

DIS 8

Compo-nent Ex-pirationDateNOTE

-0001and On

Chapter 38 - Water/Waste38-10-00-160 38-10-00-901 Potable Water Storage Tank

(Cleaning) Restoration RST 9 18Months

-0001and On

38-10-00-961 38-10-00-903 Potable Water Cartridge Filter

Element Discard DIS 91600FlightHoursNOTE

-0001and On

38-30-00-210 38-30-00-201

Toilet Catch Pan and WasteTubes (Borescope) SpecialDetailed Inspection

SDI 9 24Months

-0001and On


49-10-00-220 49-40-00-201


NOTE:Reference Honeywell49-24-09, 36-150 [EMB] APUInspection/Repair Manual

DET 61500APUHoursNOTE

-0001and On

49-10-00-221 49-40-00-202


NOTE:Reference HoneywellService Information LetterD201608000071.


-0001and On

49-10-00-222

49-22-00-20149-26-00-20149-90-00-201

Auxiliary Power Unit MagneticChip Collector Detailed Inspection



-0001and On


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MM TaskNumber


Task TitleTaskTyp-e

La-borHo-urs

CatInter-val/

Note(s)Effectiv-

ity

49-10-00-960 49-22-00-901


NOTE:Per Supplier Recommendation.Reference Honeywell 49- 24-87,36-150 [EMB] APU ComponentMaintenance Manual.

DIS 620000APUCyclesNOTE

-0001and On

49-10-00-961 49-24-00-901

Auxiliary Power Unit TurbineRotor Discard


DIS 610000APUCyclesNOTE

-0001and On

49-10-00-962 49-30-00-901



DIS 91500APUHoursNOTE

-0001and On

49-10-00-963 49-90-00-901

Auxiliary Power Unit Oil FilterElement Discard



-0001and On

49-10-00-964 49-90-00-902




-0001and On

Chapter 52 - Doors52-10-00-210 52-10-00-208 Cabin Door Seal General Visual

Inspection GVI 6 18Months

-0001and On


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Task TitleTaskTyp-e

La-borHo-urs

CatInter-val/

Note(s)Effectiv-

ity

52-10-00-221

52-10-00-201,52-10-00-202,52-10-00-203,52-10-00-204,52-10-00-205,52-10-00-206,52-10-00-207

Cabin Door Detailed Inspection DET 5, 63200FlightHours

-0001and On

52-10-00-720 52-10-00-701 Cabin Door Gas Strut Functional

Check FNC 91200FlightHours

-0001and On

52-10-00-721

52-10-00-702,52-10-00-703

Cabin Door Locking FunctionalCheck FNC 8

3200FlightHours

-0001and On

52-20-00-220

52-20-00-201,52-20-00-202,52-20-00-203

Emergency Exit Door DetailedInspection DET 6, 8,

972

Months-0001and On

52-20-00-710

52-20-00-701,52-20-00-702

Emergency Exit Door OperationalCheck OPC 8, 9 24

Months-0001and On

52-30-00-211 52-30-00-202 Baggage Door Seal General

Visual Inspection GVI 6 96Months

-0001and On

52-30-00-220 52-30-00-201 Baggage Door Counterbalance

Cable Detailed Inspection DET 62400FlightHours

-0001and On

52-80-00-210

52-80-00-201,52-80-00-202,52-80-00-203,52-80-00-204,52-80-00-205,52-80-00-206,52-80-00-207,52-80-00-208,52-80-00-209,52-80-00-210,52-80-00-211,52-80-00-212

Landing Gear Doors andComponents General VisualInspection

GVI 52400FlightHours

-0001and On

Chapter 56 - Windows


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Task TitleTaskTyp-e

La-borHo-urs

CatInter-val/

Note(s)Effectiv-

ity

56-10-00-221 56-10-00-201 Windshield Assembly Hump Seal

Detailed Inspection DET 6


-0001and On

56-10-00-720 56-10-00-701 Windshield Assembly Fastener

Torque Functional Check FNC 92400FlightHours

-0001and On

Chapter 71 - Power Plant

71-00-00-212

71-30-00-201,71-30-00-202,71-30-00-203,71-30-00-204,71-30-00-205,71-30-00-206,71-30-00-207

Engine Nacelle Fire Seals andFirewall General Visual Inspection GVI 8 54

Months-0001and On

Chapter 72 - Engine

Refer toHoneywellAerospace72-05-25EngineLightMainte-nanceManual

73-10-00-902

Engine Nozzle, FuelInjection-Start (DetailedInspection and FunctionalCheck) Restoration

NOTE:The Engine Nozzle, FuelInjection-Start is not fieldserviceable. You maycontact Textron AviationParts Department (TAPD) at316-517-6002 for assistancewith obtaining a properlyrestored Engine Nozzle, FuelInjection-Start and/or referenceHoneywell Aerospace 72-05-25Light Maintenance Manual.

DET 62000EngineHoursNOTE

-0001and On


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MM TaskNumber


Task TitleTaskTyp-e

La-borHo-urs

CatInter-val/

Note(s)Effectiv-

ity


73-10-00-901

Engine Nozzle, Fuel Injection-HiTemp (Detailed Inspection andFunctional Check) Restoration

NOTE:The Engine Nozzle, FuelInjection-Hi Temp is notfield serviceable. You maycontact Textron AviationParts Department (TAPD) at316-517-6002 for assistance withobtaining a properly restoredEngine Nozzle, Fuel Injection-HiTemp and/or reference HoneywellAerospace 72-05-25 LightMaintenance Manual.

RST 64000EngineHoursNOTE

-0001and On


72-71-00-20275-21-00-90175-21-00-902

Engine Fan Blade (FluorescentPenetrant Inspection) SpecialDetailed Inspection

NOTE:Per Supplier Recommendation.Honeywell Aerospace 72-05-25Light Maintenance Manual.

SDI,DIS 5, 6

15000EngineCyclesNOTE

-0001and On


75-21-00-901

Engine High Pressure TurbineInterstage Rotating-Seal Discard

NOTE:Per Supplier Recommendation.Honeywell Aerospace 72-05-25Light Maintenance Manual

DIS 515000EngineCyclesNOTE

-0001and On


75-21-00-902

Engine Seal Assembly HighPressure Turbine Stage 2 Discard

NOTE:Per Supplier Recommendation.Honeywell Aerospace 72-05-25Light Maintenance Manual

DIS 515000EngineCyclesNOTE

-0001and On


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MM TaskNumber


Task TitleTaskTyp-e

La-borHo-urs

CatInter-val/

Note(s)Effectiv-

ity


72-60-00-201

Engine Accessory Gearbox(AGB) Assembly General VisualInspection


GVI 6800

EngineHoursNOTE

-0001and On


72-71-00-203

Engine Fan Stator Vane AssemblyGeneral Visual Inspection


GVI 6800

EngineHoursNOTE

-0001and On


79-20-00-901

Engine Oil Filter Element Discard

NOTE:Reference Honeywell Aerospace72-05-25 Light MaintenanceManual.

DIS 7800

EngineHoursNOTE

-0001and On


79-20-00-902

Engine Oil Discard


DIS 71600EngineHoursNOTE

-0001and On


71-70-00-201

Engine Drain Tubes GeneralVisual Inspection

NOTE:Per Supplier Recommendation.Honeywell Aerospace 72-05-25Light Maintenance Manual(LMM).

GVI 94000EngineHoursNOTE

-0001and On


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MAINTENANCE MANUAL



MM TaskNumber


Task TitleTaskTyp-e

La-borHo-urs

CatInter-val/

Note(s)Effectiv-

ity


71-70-00-202

Engine Accessory GearboxBreather Adapter General VisualInspection



-0001and On


71-70-00-203

Engine Fuel Manifold Drip ShieldGeneral Inspection



-0001and On


72-30-00-201

Engine Compressor Guide VaneActuating System General VisualInspection



-0001and On


72-30-00-203

Engine Compressor/DiffuserCase Detailed Inspection


DET 6, 84000EngineHoursNOTE

-0001and On


72-30-00-204

Engine Compressor/DiffuserCase Attachment Flange andHardware Detailed Inspection



-0001and On


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MM TaskNumber


Task TitleTaskTyp-e

La-borHo-urs

CatInter-val/

Note(s)Effectiv-

ity


72-40-00-201

Engine Combustor Module(Borescope) Special DetailedInspection


SDI 6, 94000EngineHoursNOTE

-0001and On


72-40-00-202

Engine Combustor Case andAttachment Hardware GeneralVisual Inspection



-0001and On


72-51-00-201

Engine HP Turbine Module(Borescope) Special DetailedInspection



-0001and On


72-55-00-201

Engine LP Turbine Module(Borescope) Special DetailedInspection



-0001and On


72-55-00-202

Engine Exit Guide Vane (EGV)Assembly General VisualInspection


GVI 6, 84000EngineHoursNOTE

-0001and On


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MM TaskNumber


Task TitleTaskTyp-e

La-borHo-urs

CatInter-val/

Note(s)Effectiv-

ity


72-71-00-204

Engine Fan Inlet Housing GeneralVisual Inspection



-0001and On


72-71-00-205

Engine Mount Pad General VisualInspection



-0001and On


72-72-00-201

Engine Inner Fan Bypass DuctsGeneral Visual Inspection



-0001and On


72-72-00-202

Engine Fan Bypass Outer DuctGeneral Visual Inspection



-0001and On


73-10-00-201

Engine Fuel Filter AssemblyDiscard


DIS 64000EngineHoursNOTE

-0001and On


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MAINTENANCE MANUAL



MM TaskNumber


Task TitleTaskTyp-e

La-borHo-urs

CatInter-val/

Note(s)Effectiv-

ity


73-20-00-201

Engine P3 Sensor Line DetailedInspection


DET 6, 94000EngineHoursNOTE

-0001and On


74-20-00-201

Engine Ignition Lead DetailedInspection



-0001and On


75-21-00-201

Engine Low Pressure TurbineCooling Tube General VisualInspection


GVI 6, 94000EngineHoursNOTE

-0001and On


75-21-00-202

Engine High Pressure TurbineModule (Borescope) SpecialDetailed Inspection


SDI 54000EngineHoursNOTE

-0001and On


75-21-00-203

Engine Rotor Assembly, HPT- Stage 1 (Borescope) SpecialDetailed Inspection



-0001and On


ICA-700-25-00001 Form 2261 Rev 1

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MAINTENANCE MANUAL



MM TaskNumber


Task TitleTaskTyp-e

La-borHo-urs

CatInter-val/

Note(s)Effectiv-

ity


75-21-00-204

Engine Combustor Support(Borescope) Special DetailedInspection

NOTE:Per Supplier Recommendation,Honeywell Aerospace 72-05-25Light Maintenance Manual.


-0001and On


75-21-00-205

Engine High Pressure TurbineModule (Borescope) SpecialDetailed Inspection



-0001and On


75-21-00-206

Engine Exit Guide Vane (EGV)Assembly General VisualInspection



-0001and On


75-21-00-701

Engine Cooling Tube Check ValveFunctional Check


FNC 84000EngineHoursNOTE

-0001and On


78-10-00-201

Engine Exhaust Mixer NozzleGeneral Visual Inspection



-0001and On


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MAINTENANCE MANUAL



MM TaskNumber


Task TitleTaskTyp-e

La-borHo-urs

CatInter-val/

Note(s)Effectiv-

ity


78-10-00-202

Engine Exhaust Center BodyGeneral Visual Inspection



-0001and On


79-21-00-201

Engine External-Plumbing ofthe Oil System General VisualInspection



-0001and On


72-30-00-202

Engine Compressor Section(Borescope) Special DetailedInspection



-0001and On


72-71-00-201

Engine Fan Rotor AssemblyDetailed Inspection



-0001and On

Chapter 78 - Exhaust


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Systems, APU, and Powerplant Inspection Task Data SampleFigure 1 (Sheet 1)


ICA-700-25-00001 Form 2261 Rev 1

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MM TaskNumber


Task TitleTaskTyp-e

La-borHo-urs

CatInter-val/

Note(s)Effectiv-

ity

78-30-00-220

78-30-00-201,78-30-00-202,78-30-00-203,78-30-00-204

Thrust Reverser AssemblyDetailed Inspection DET 6

3200FlightHours

-0001and On

Chapter 80 - StartingRefer toHoneywellAerospace72-05-25EngineLightMainte-nanceManual

80-11-00-901

Air Turbine Starter Oil Discard


DIS 9800

EngineHoursNOTE

-0001and On


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MSG-3 INSPECTION DOCUMENTS AND OTHER REQUIRED TASKS

1. Purpose and UseA. This section provides an overview of all Model 700 scheduled inspection requirements.

B. Inspection Documents and other required tasks listed in Table 1, Table 2, and Table 3 below,provide the basis for the basis for the maintenance tracking system provider used to set upthe maintenance tracking and reporting system for the Standard Manufacturer’s RecommendedContinuous Airworthiness Inspection Program.

C. Inspection documents (packaging of MSG-3 Tasks listed in Chapter 5, MSG-3 Inspection Time Limits)are provided to group various tasks with the same interval, and facilitate completing the tasks at aspecified downtime. Inspection documents are numbered as shown below in sequential order, withInspection Document 5-12-01 the first Inspection Document due.

Chapter Section Inspection Document 15- 12 -01

D. The following Table 1 MSG-3 Airframe Inspection Documents and Tasks provide links to all Model700 MSG-3 scheduled airframe inspection documents and tasks associated to the StandardManufacturer’s Recommended Continuous Airworthiness Inspection Program.(1) Some intervals in the MRBR and the Maintenance Planning Document use a Note referring

to special conditions, such as supplier publication, or regulatory requirement (such as NFPAdocument). In these cases, the MSG-3 ISC agreed with the supplier or regulatory recommendedinterval for all operators. However, in other cases where an Access Defined was used, theinterval is contingent on circumstances, such as Anytime Bottle 1 or 2 Engine Fire ExtinguishingSystem is Fired. In these cases, the task requirement is event driven and not typically alignedwith hard flight hour or calendar intervals.

Table 1. MSG-3 Airframe Inspection Documents and Tasks

InspectionDocument Title Interval/Note(s) Effectivity

5-12-01 Inspection Document 1 18 Months -0001 and On

5-12-02 Inspection Document 2 800 Flight Hours -0001 and On




5-12-06 Not Currently Used N/A -0001 and On









5-12-15 Inspection Document 15 800 Flight Hours or 18 Months,Whichever Occurs First -0001 and On


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Table 1. MSG-3 Airframe Inspection Documents and Tasks (continued)InspectionDocument Title Interval/Note(s) Effectivity





5-12-20 Inspection Document 20 800 Flight Hours or 18 Months,Whichever Occurs First -0001 and On


5-12-22 Inspection Document 2254 Months, Then Every 18

Months Thereafter Until Batteryis Replaced

-0001 and On


4-12-00 Airworthiness Inspections Refer to Airworthiness LimitationsInspections Documents -0001 and On

E. In addition to Table 1 MSG-3 Airframe Inspection Documents and Tasks above, operators areresponsible for ensuring all MSG-3 Supplier Inspection Intervals and Inspection tasks listed in Table2, below, are completed when due.

Table 2. MSG-3 Supplier Inspection Intervals and Inspection Reference Documents

Task/ChapterNumber orSupplier

InformationReference

Title Interval/Note(s) Effectivity

Chapter 23 - Communications

23-70-00-960Cockpit Voice RecorderUnderwater Locator BeaconBattery Discard

Component Expiration Date -0001 and On


24-30-00-910

Engine Direct-Current Generator(Bearing Replacement)

Restoration

NOTE:You may contact Textron AviationParts Department (TAPD) at316-517-6002 for assistancewith obtaining a properlyrestored Engine Direct-CurrentGenerator and/or referenceComponent Maintenance Manualwith Illustrated Parts List DC

Generator (Main)

3,200 Flight Hours or 60 Months,Whichever Occurs First NOTE -0001 and On


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Table 2. MSG-3 Supplier Inspection Intervals and Inspection Reference Documents (continued)Task/ChapterNumber orSupplier



24-30-00-911

Auxiliary Power UnitDirect-Current Generator(Bearing Replacement)

Restoration

NOTE:You may contact Textron AviationParts Department (TAPD) at316-517-6002 for assistancewith obtaining a properlyrestored APU Direct-CurrentGenerator and/or referenceComponent Maintenance Manualwith Illustrated Parts List DC

Generator (APU)

3,200 Flight Hours or 60 Months,Whichever Occurs First NOTE -0001 and On


25-20-00-960



120 Months Tracked byComponent Manufacture Date

NOTE-0001 and On

25-60-00-960 Emergency Locator TransmitterBattery Discard Component Expiration Date -0001 and On

25-61-00-210


NOTE:Per Supplier Recommendation.Life Raft Visual Check is to beaccomplished by an authorizedWinslow Life Raft Service Station.Reference Winslow Doc NoMFG-526/RS-457.


NOTE-0001 and On

25-61-00-211

Model FA-AV(SA) Life RaftGeneral Visual Inspection (IfInstalled)

NOTE:Per Supplier Recommendation.Reference Winslow Doc NoMFG-526/RS-457.


NOTE-0001 and On


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MAINTENANCE MANUAL




25-61-00-720


NOTE:Per Supplier Recommendation.Life Raft (Hydrostatic) FunctionalCheck is to be accomplishedby an authorized WinslowLife Raft Service Station.Reference Winslow Doc NoMFG-526/RS-457.


NOTE-0001 and On

25-61-00-910


NOTE:You may contact Textron AviationParts Department (TAPD) at316-517-6002 for assistance withobtaining a properly restoredPersonal Flotation Device.

120 Months Tracked byManufacture Date

NOTE-0001 and On

Chapter 26 - Fire Protections

26-20-00-720

Engine Fire Extinguishing BottleLow Pressure Switch FunctionalCheck


Coincide with HydrostaticTest (if applicable) not to

Exceed 60 MonthsNOTE

-0001 and On

26-20-00-960

CT03200-1 and CT03300-1Engine Fire Bottle Cartridge(Squib) Discard

NOTE:Per Supplier Recommendation.The maximum service life ofthe cartridge installed is 144Months. The total life of thecartridge including shelf life is180 Months. Reference MASSSystems 26-22-02 ComponentMaintenance Manual.

144 Months Tracked byComponent Installation Date

NOTE-0001 and On


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26-21-00-720

Auxiliary Power Unit FireExtinguishing Bottle LowPressure Switch FunctionalCheck


Coincide with HydrostaticTest (If Applicable) not to

Exceed 60 MonthsNOTE

-0001 and On

26-21-00-960

CT03400-1 Auxiliary Power UnitFire Bottle Cartridge (Squib)Discard

NOTE:Per Supplier Recommendation.The maximum service life ofthe cartridge installed is 144Months. The total life of thecartridge including shelf life is180 Months. Reference MASSSystems 26-22-02 ComponentMaintenance Manual.

144 Months Tracked byComponent Installation Date

NOTE-0001 and On

Chapter 31 - Indicating/Recording Systems

31-30-00-960Flight Data Recorder UnderwaterLocator Beacon Battery Discard

(If Installed)Component Expiration Date -0001 and On


32-40-00-220 Main Landing Gear Wheel andTire Detailed Inspection

Every Tire Change Not toExceed 36 Months -0001 and On

32-40-00-221 Nose Landing Gear Wheel andTire Detailed Inspection

Every Tire Change Not toExceed 36 Months -0001 and On

32-40-00-280

Nose Landing Gear WheelAssembly Special DetailedInspection


Based on Tire Changes, Calendarand Landings

NOTE-0001 and On


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32-40-00-281

Main Landing Gear WheelAssembly Special DetailedInspection

NOTE:Per Supplier Recommendation.Reference BF Goodrich 32-45-56Component Maintenance Manual.

Based on Tire Changes, Calendarand Landings

NOTE-0001 and On

32-41-00-220 Main Landing Gear BrakeAssembly Detailed Inspection Every Wheel Removal -0001 and On

32-41-00-720Main Landing Gear BrakeAssembly Wear Pin FunctionalCheck

Every Wheel Removal -0001 and On

Chapter 35 - Oxygen

35-10-00-910

MC10-16-150 CrewOxygenMask(Accomplish Supplier Testing andFault Isolation Task) Restoration(If Installed)

NOTE:You may contact Textron AviationParts Department (TAPD) at316-517-6002 for assistanceWith Obtaining a ProperlyRestored Crew Oxygen Maskand/or Reference 35-13-63Intertechnique Aircraft SystemsCMM with IPL Crew OxygenMask Regulator

72 Months Tracked byComponent Time Limits

NOTE-0001 and On

35-10-00-911

MLD20-505 Full Face CrewOxygen Mask (AccomplishSupplier Testing and FaultIsolation Task) Restoration (IfInstalled)



NOTE-0001 and On


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35-10-00-912

MC10-15-109 or MC10-16-101Observer/Jump Seat OxygenMask (Accomplish SupplierTesting and Fault Isolation Task)Restoration (If Installed)



NOTE-0001 and On

35-30-00-960


NOTE:Per Supplier Recommendations.User Reference and ProceduresManual for the EssexCrewmember PBE.

Component Expiration DateNOTE -0001 and On


49-10-00-960


NOTE:Reference Honeywell 49- 24-87,36-150 [EMB] APU ComponentMaintenance Manual.

20,000 APU CyclesNOTE -0001 and On

49-10-00-961

Auxiliary Power Unit TurbineRotor Discard

NOTE:Reference Honeywell 49- 24-87,36-150 [EMB] APU ComponentMaintenance Manual.

10,000 APU CyclesNOTE -0001 and On

49-10-00-962



1500 APU HoursNOTE -0001 and On


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49-10-00-220


NOTE:Reference Honeywell49-24-09, 36-150 [EMB] APUInspection/Repair Manual


49-10-00-221


NOTE:Reference HoneywellService Information LetterD201608000071


49-10-00-222

Auxiliary Power Unit MagneticChip Collector Detailed Inspection



49-10-00-963

Auxiliary Power Unit Oil FilterDiscard



49-10-00-964




Chapter 72 - EngineRefer toHoneywellAerospace72-05-25

Engine LightMaintenanceManual,Chapter5-20-00

Honeywell Engine PeriodicInspections and AirworthinessLimitations

NOTE:Refer to Honeywell Aerospace72-05-25 Engine LightMaintenance Manual Chapter5-20-00

Engine Hours or CyclesNOTE -0001 and On

NOTE 1: Access Defined is an Interval that is event driven and/or to be coordinated with the removal of acomponent. Access defined task intervals cannot be set at a hard time because it is not possible toaccomplish the tasks until the event occurs and/or the component is removed.


ICA-700-25-00001 Form 2261 Rev 1

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F. In addition to Inspection Documents and tasks listed in Table 1 and Table 2 above, operators areresponsible for ensuring all Regulatory Inspections, Airworthiness Directives, Inspection Checksrelated to Instructions for Continued Airworthiness Supplements, Supplemental Type Certificate(STC) Modifications, Service Letters and Service Bulletins (associated to Scheduled Inspections)listed in Table 3 are completed when due (if applicable).

Table 3. Other Scheduled Maintenance Inspections

Task/ChapterNumber Title Interval/Note(s) Effectivity

5-13-00

Regulatory Inspections/TimeLimits

NOTE:Maintenance Inspections Listedin Chapter 5-13-00 are notIncluded in MSG-3 ProgramBecause the Tasks may notbe Required for InternationalOperators. InternationalOperators Should Check withLocal Regulatory Authority forSimilar Requirements.

Refer to 5-13-00 for intervals. -0001 and On

5-14-00 Airworthiness Directives Refer to 5-14-00 for intervals. -0001 and On

5-15-00 Instructions for ContinuedAirworthiness (ICA) Supplements


5-16-00 Supplemental Type Certificates(STC)


5-17-00 Service Letters and ServiceBulletins


G. The information listed in Table 4 Discretionary Maintenance is not required by MSG-3, but may beapplicable and/or effective for certain operators.

Table 4. Discretionary Maintenance

Task/ChapterNumber Title Interval/Note(s) Effectivity

5-18-00 Supplier Information Refer to 5-18-00 for intervals. -0001 and On

5-19-00 Discretionary Maintenance Refer to 5-19-00 for intervals. -0001 and On


ICA-700-25-00001 Form 2261 Rev 1

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INSPECTION DOCUMENT 2

Date Completed _______________

Airplane Serial Number _______________

Airplane Registration Number _______________

Airplane Total Time _______________

Airplane Total Landings _______________

1. DescriptionA. Inspection Document 5-12-02 gives a list of MSG-3 Tasks to be completed every 800 Flight Hours.

B. A task number and hyperlink provides detailed information about each inspection in individual chaptersof this manual.

C. The right portion of each page provides space for mechanic and inspector initials and remarks. Youcan use copies of these pages as a checklist while you complete the tasks.

2. General Inspection CriteriaA. As you complete each inspection task, examine the adjacent area while access is available to find

conditions that need more maintenance.

B. If it is necessary to replace/adjust a component or system during a task, complete any required returnto service procedures for that system before the remaining steps of the task are completed.

C. Refer to Chapter 5-10-01, MSG-3 Inspection Time Limits for Zone definitions (ENG, AUX, etc).

3. Task FindingsA. Enter the Task Findings into the maintenance tracking system used or provide them to Textron

Aviation, Maintenance Engineering, Department 753, 2121 South Hoover Road, Wichita, Kansas67209, Phone: 316-517-9370, , Email: [email protected].

NOTE: An Inspection Document or Inspection Task should only be recorded as completed in theaircraft log after the findings have been entered into the maintenance tracking systemused or sent to Textron Aviation, Maintenance Engineering.

4. Inspection Document 2 TasksA. Task 21-30-00-710: Manual Pressurization Operational Check

Zone Task Findings For Task 21-30-00-710 (Check All That Apply) Mech InspManual Pressurization System

[__] No Fault Found [__] Incorrect CabinPressureControllerOperation

[__] Incorrect OutflowValve Operation

233,234

[__] IncorrectPressure ReliefValve Operation

[__] Other

Notes:

B. Task 26-20-00-710: Engine Fire Extinguishing System Operational Check


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Zone Task Findings For Task 26-20-00-710 (Check All That Apply) Mech InspEngine Fire Extinguishing System

[__] No Fault Found [__] Fuel Shutoff ValveFailed to Close(Any)

[__] Hydraulic ShutoffValve Failed toClose (Any)

173,174,233,234,317,318,365,366

[__] ENGINE FIRESwitch/LightFailed toilluminate

[__] No VoltagePresent at Squibs(Any)

[__] Other

Notes:

C. Task 26-21-00-710: Auxiliary Power Unit Fire Extinguishing System Operational Check

Zone Task Findings For Task 26-21-00-710 (Check All That Apply) Mech InspAPU Fire Extinguishing System

[__] No Fault Found [__] APU Fuel ShutoffValve Failed toClose

[__] APU FIRESwitch/LightFailed toilluminate

174,229,365,366

[__] No VoltagePresent at Squib

[__] Other

Notes:

D. Task 35-10-00-220: Crew Oxygen Mask and Storage Box Detailed Inspection

Zone Task Findings For Task 35-10-00-220 (Check All That Apply) Mech InspStorage Boxes (Any)

[__] No Fault Found [__] Security ofInstallation

[__] Cracks

235,236

[__] Other

Notes:Crew Oxygen Mask (Any)

[__] No Fault Found [__] Damage [__] Deterioration

235,236

[__] Leaks [__] Other

Notes:

E. Task 35-10-00-221: Oxygen Bottle Detailed Inspection

Zone Task Findings For Task 35-10-00-221 (Check All That Apply) Mech InspOxygen Bottle (Any)

[__] No Fault Found [__] Corrosion [__] Damage

215,216

[__] Security ofInstallation

[__] Other

Notes:

F. Task 35-10-00-222: Observer/Jump Seat Oxygen Mask Detailed Inspection (If Installed)


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Zone Task Findings For Task 35-10-00-222 (Check All That Apply) Mech InspStorage Boxes (Any)


[__] Cracks

241,

[__] Other

Notes:Crew Oxygen Mask


241,


Notes:

G. Task 35-20-00-220: Passenger Oxygen Canister and Mask Detailed Inspection

NOTE: It is recommended to perform this task at the same time as Task 35-20-00-720.

Zone Task Findings For Task 35-20-00-220 (Check All That Apply) Mech InspOxygen Canister (Any)


[__] Damage

241,242,251,252,267,268,275,276

[__] Cracks [__] Other

Notes:Passenger Oxygen Mask (Any)


241,242,251,252,267,268,275,276


Notes:

H. Task 35-20-00-720: Passenger Oxygen System Functional Check

NOTE: It is recommended to perform this task at the same time as Task 35-20-00-220.

Zone Task Findings For Task 35-20-00-720 (Check All That Apply) Mech InspPassenger Oxygen System227

[__] No Fault Found [__] Fails to Operate [__] Other

Notes:

I. Task 52-10-00-720: Cabin Door Gas Strut Functional Check


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Zone Task Findings For Task 52-10-00-720 (Check All That Apply) Mech InspCabin Door Gas Strut812

[__] No Fault Found [__] Out of Tolerance [__] Other

Notes:


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INSPECTION DOCUMENT 11

Date Completed _______________

Airplane Serial Number _______________

Airplane Registration Number _______________

Airplane Total Time _______________

Airplane Total Landings _______________

1. DescriptionA. Inspection Document 5-12-11 gives a list of MSG-3 Tasks to be completed every 54 Months.

B. A task number and hyperlink provides detailed information about each inspection in individual chaptersof this manual.

C. The right portion of each page provides space for mechanic and inspector initials and remarks. Youcan use copies of these pages as a checklist while you complete the tasks.

2. General Inspection CriteriaA. As you complete each inspection task, examine the adjacent area while access is available to find

conditions that need more maintenance.

B. If it is necessary to replace/adjust a component or system during a task, complete any required returnto service procedures for that system before the remaining steps of the task are completed.

C. Refer to Chapter 5-10-01, MSG-3 Inspection Time Limits for Zone definitions (ENG, AUX, etc).

3. Task FindingsA. Enter the Task Findings into the maintenance tracking system used or provide them to Textron

Aviation, Maintenance Engineering, Department 753, 2121 South Hoover Road, Wichita, Kansas67209, Phone: 316-517-9370, Email: [email protected].

NOTE: An Inspection Document or Inspection Task should only be recorded as completed in theaircraft log after the findings have been entered into the maintenance tracking systemused or sent to Textron Aviation, Maintenance Engineering.

4. Inspection Document 11 TasksA. Task 25-10-00-221: Observer/Jump Seat, Carriage Plate, Seat Rail, and Seat Restraint Detailed

Inspection (If Installed)

Zone Task Findings For Task 25-10-00-221 (Check All That Apply) Mech InspObserver/Jump Seat (Check All That Apply)

[__] No Fault Found [__] UpholsteryDamage

[__] Roller Damage

[__] Guide Damage [__] Security ofInstallation

[__] Frame Cracked

241

[__] Fails to Operate [__] Other

Notes:


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Zone Task Findings For Task 25-10-00-221 (Check All That Apply) Mech InspCarriage Plate (Check All That Apply)

[__] No Fault Found [__] Corrosion [__] Damage

241

[__] Security ofInstallation

[__] Other

Notes:Seat Rail(s) (Check All That Apply)

[__] No Fault Found [__] Corrosion [__] Cracked

241

[__] FastenersMissing

[__] Worn [__] Other

Notes:Seat Restraint (Check All That Apply)

[__] No Fault Found [__] Torn [__] Frayed

[__] Worn [__] Security ofInstallation

[__] Fails to Lock

241

[__] Other

Notes:

B. Task 25-20-00-220: Passenger Seat, Seat Attachment Fitting and Seat Restraint Detailed Inspection

Zone Task Findings For Task 25-20-00-220 (Check All That Apply) Mech InspPassenger Seat (Any)

[__] No Fault Found [__] Damage [__] Frame Cracked

251,252,267,268,275,276

[__] Other

Notes:Seat Attachment Fitting (Any)251,

252,267,268,275,276

[__] No Fault Found [__] Cracked [__] Other

Notes:Seat Restraint (Any)

[__] No Fault Found [__] Frayed/Torn [__] Fails to Operate

251,252,267,268,275,276

[__] Security [__] Other

Notes:

C. Task 25-20-00-221: Side Facing Couch Frame Assembly, Couch Attachment Fitting and CouchRestraint Detailed Inspection (If Installed)


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Zone Task Findings For Task 25-20-00-221 (Check All That Apply) Mech InspCouch Frame (Any)

[__] No Fault Found [__] Damage [__] Frame Cracked

242,267,275

[__] Other

Notes:Couch Attachment Fitting (Any)242,

267,275 [__] No Fault Found [__] Cracked [__] Other

Notes:Couch Restraint (Any)

[__] No Fault Found [__] Frayed/Torn [__] Fails to Operate

242,267,275

[__] Security [__] Other

Notes:

D. Task 25-61-00-221: Personal Flotation Device Storage Pouch Detailed Inspection

Zone Task Findings For Task 25-61-00-221 (Check All That Apply) Mech InspPFD Pouch (Any)233,

234,242,251,252,267,268,275,276,282

[__] No Fault Found [__] Pouch Torn [__] Other

Notes:

E. Task 28-10-00-220: Fuel Panel and Fuel Panel Seal Detailed Inspection

Zone Task Findings For Task 28-10-00-220 (Check All That Apply) Mech InspFuel Panel(s)

[__] No Fault Found [__] Corrosion [__] Seal Damage161,162,171,172,512,612

[__] Integrity ofProtectiveCoatings

[__] Other

Notes:Fuel Panel(s)

[__] No Fault Found [__] Corrosion [__] Seal Damage

521,531,541,621,631,641

[__] Integrity ofProtectiveCoatings

[__] Other

Notes:

F. Task 28-40-00-710: Low Fuel Level Sensor Operational Check


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Zone Task Findings For Task 28-40-00-710 (Check All That Apply) Mech InspLow Fuel Level Sensor (Left Wing, Right Wing)225

[__] No Fault Found [__] Fails Check [__] Other

Notes:

G. Task 57-20-00-210: Wing Internal Zonal General Visual Inspection

NOTE: It is recommended to perform this task at the same time as Task 28-10-00-210, Task28-10-00-211, Task 28-11-00-210, Task 28-20-00-210, Task 28-20-00-220, and Task28-40-00-210.

Zone Task Findings For Task 57-20-00-210 (Check All That Apply) Mech InspLeft and Right Wings, Inboard

[__] No Fault Found [__] Debris [__] MycrobacterialGrowth

[__] Security ofComponents

[__] Level 1 Corrosion [__] Level 2 Corrosion

514,614

[__] Level 3 Corrosion [__] Other

Notes:Wing Leading Edge

[__] No Fault Found [__] Wires Chaffed [__] Wires Damaged

516,616


[__] Signs of Arcing [__] Other

Notes:Left and Right Wing

[__] No Fault Found [__] Debris [__] Security ofComponents

[__] Level 1 Corrosion [__] Level 2 Corrosion [__] Level 3 Corrosion

522,533,543,622,633,643

[__] Other

Notes:Winglets


552,652


[__] Signs of Arcing [__] Other

Notes:

H. Task 57-20-00-221: Wing Internal Detailed Inspection

NOTE: It is recommended to perform this task at the same time as Task 28-10-00-210,Task 28-10-00-211, Task 28-10-00-212, Task 28-11-00-210 Task 28-20-00-210, Task28-20-00-220, and Task 28-40-00-210.


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Zone Task Findings For Task 57-20-00-221 (Check All That Apply) Mech InspLeft and Right Wings

[__] No Fault Found [__] Security ofFasteners

[__] Damage

[__] Level 1 Corrosion [__] Level 2 Corrosion [__] Level 3 Corrosion

514,515,522,533,534,543,544,614,615,622,633,634,644

[__] Other

Notes:Winglets

[__] No Fault Found [__] Security ofFasteners

[__] Damage

552,652

[__] Cracks [__] Delamination [__] Other

Notes:

I. Task 57-20-00-222: Wing Internal Fuel Monitoring Wiring Standalone EZAP Detailed Inspection

NOTE: It is recommended to perform this task at the same time as Task 28-10-00-210, Task28-10-00-211, Task 28-11-00-210, Task 28-20-00-210, Task 28-20-00-220, and Task28-40-00-210.

Zone Task Findings For Task 57-20-00-222 (Check All That Apply) Mech InspLeft and Right Wings, Inboard


514,614

[__] Security of Wires [__] Signs of Arcing [__] Other

Notes:Left and Right Wings


522,533,543,622,633,643

[__] Security of Wires [__] Signs of Arcing [__] Other

Notes:

J. Task 71-00-00-212: Engine Nacelle Fire Seals and Firewall General Visual Inspection

Zone Task Findings For Task 71-00-00-212 (Check All That Apply) Mech InspEngine Nacelle

[__] No Fault Found [__] Seals Damaged [__] CowlingsDamaged

415,416

[__] Other

Notes:


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Zone Task Findings For Task 71-00-00-212 (Check All That Apply) Mech InspFirewalls415,

416 [__] No Fault Found [__] Cracked [__] Other

Notes:


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MAINTENANCE MANUAL

SUPPLIER INFORMATION

1. Purpose and Use

NOTE: This MM is updated, supplemented, and changed with reference to Supplier Information.Some inspection tasks refer to Supplier Information that must be referenced to comply with theStandard Manufacturer’s Recommended Continuous Airworthiness Inspection Program.

NOTE: This section only provides a list of supplier and related reference documents that may beneeded to comply with continuous airworthiness inspections. For a comprehensive list ofsuppliers, refer to the Introduction - Supplier Publication List.

A. The owner/operator must make sure that all specific Supplier Information is referenced to comply withcertain tasks in the Standard Manufacturer’s Recommended Continuous Airworthiness InspectionProgram. The list below only provides reference to Supplier Information that is associated to theairplane continuous airworthiness inspections.

B. Table 1 should be cross-checked with the airplane installed equipment list in preparation for eachscheduled inspection to make sure that all new and repetitive supplier information is complied with.

NOTE: Textron Aviation provides an electronic copy of the documents listed in Table 1 to the firstairplane owner at time of delivery; however it is each owner/operators responsibility toreplace or obtain the revision service for these documents, if desired.

Table 1. Supplier Information

MaintenanceManual Task #

Task Title SupplierPublication #

Supplier SupplierPublication Title

23-70-00-710 Cockpit VoiceRecorderUnderwater LocatorBeacon (Ping Test)Operational Check

03-TM-0037 Dukane SeacomDiv.

Dukane Seacom03-TM-0037Technical ManualUnderwaterAcoustic Beacon

24-30-00-210 Lithium-Ion BatteryGeneral VisualInspection

9018041 True Blue Power True Blue PowerInstallation Manualand OperatingInstructions

24-30-00-720 MarathonNickel-CadmiumBattery (Capacity)Functional Check (IfInstalled)

DCR59577 Marathon NorcoAerospace

MarathonNorcoAerospaceComponentMaintenanceManual

24-30-00-721 Standby Battery(Capacity)Functional Check

0070-01 Securaplane SecuraplaneComponentMaintenanceManual

24-30-00-722 Lithium-IonBattery (Capacity)Functional Check

9018041 True Blue Power True Blue PowerInstallation Manualand OperatingInstructions


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Table 1. Supplier Information (continued)MaintenanceManual Task #



24-30-00-910 Engine Direct-Current Generator(BearingReplacement)Restoration

24-31-41 Safran Power USA,LLC

ComponentMaintenanceManual withIllustrated PartsList DC Generator(Main)

24-30-00-911 Auxiliary PowerUnit Direct-CurrentGenerator (BearingReplacement)Restoration

24-31-42 Safran Power USA,LLC

ComponentMaintenanceManual withIllustrated PartsList DC Generator(APU)

25-20-00-210 Inflatable OccupantProtection SystemComponentGeneral VisualInspection

01.01.00.03 Aviation OccupantSafety

Aviation OccupantSafety 01.01.00.03ComponentMaintenanceManual

25-20-00-710 Inflatable OccupantProtection SystemOperational Check



25-20-00-960 Inflatable OccupantProtection SystemComponent Discard



25-60-00-221 EmergencyLocator TransmitterAntenna DetailedInspection

ARTEX Y1-03-0333 Artex AircraftSupplies

ARTEX Y1-03-0333ComponentMaintenanceManual

25-60-00-720 Artex ELT-4000TransmitterDetailed Inspectionand FunctionalCheck

ARTEX Y1-03-0333 Artex AircraftSupplies

ARTEX Y1-03-0333ComponentMaintenanceManual

25-61-00-210 Model FA-AV(SA)Life Raft VisualCheck (If Installed)

526/RS-457 Winslow Life RaftCompany

Winslow Doc NoMFG-526/RS-457

25-61-00-720 Model FA-AV(SA)Life Raft FunctionalCheck (If Installed)

526/RS-457 Winslow Life RaftCompany

Winslow Doc NoMFG-526/RS-457

25-61-00-910 P07074-207Personal FlotationDevice (AccomplishSupplier 120 MonthMaintenanceInspection)Restoration

25-60-41 EAM Worldwide Eastern AeroMarine 25-60-41ComponentMaintenanceManual


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26-20-00-720 Engine FireExtinguishing BottleLow PressureSwitch FunctionalCheck

26-22-02 MASS Systems, Inc 26-22-02ComponentMaintenanceManual andSupplement26-22-02FX04900-1 FireExtinguisher, DualOutlet

26-20-00-960 CT03200-1 andCT03300-1 EngineFire Bottle Cartridge(Squib) Discard

26-22-02 MASS Systems, Inc MASS Systems26-22-02ComponentMaintenanceManual

26-21-00-720 Auxiliary Power UnitFire ExtinguishingBottle Low PressureSwitch FunctionalCheck

26-22-02 MASS Systems, Inc 26-22-02ComponentMaintenanceManual andSupplement26-22-02FX05000-1 FireExtinguisher, DualOutlet

26-21-00-960 CT03400-1Auxiliary PowerUnit Fire BottleCartridge (Squib)Discard

26-22-02 MASS Systems, Inc MASS Systems26-22-02ComponentMaintenanceManual

31-30-00-710 Flight DataRecorderUnderwater LocatorBeacon (Ping Test)Operational Check(If Installed)

03-TM-0037 Dukane SeacomDiv

Dukane Seacom03-TM-0037Technical ManualUnderwaterAcoustic Beacon

32-40-00-280 Nose Landing GearWheel AssemblySpecial DetailedInspection

32-47-43 BF GoodrichCompany

BF Goodrich32-47-43ComponentMaintenanceManual

32-40-00-281 Main Landing GearWheel AssemblySpecial DetailedInspection

32-45-56 BF GoodrichCompany

BF Goodrich32-45-56ComponentMaintenanceManual


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35-10-00-910 MC10-16-150Crew OxygenMask (AccomplishSupplier Testingand Fault IsolationTask) Restoration(If Installed)

35-13-63 Intertechique SA (Intertechnique)Aircraft Systems35-13-63ComponentMaintenanceManual with IPLCrew Oxygen MaskRegulator

35-10-00-911 MLD20-505 FullFace Crew OxygenMask (AccomplishSupplier Testingand Fault IsolationTask) Restoration(If Installed)

35-13-64 Intertechique SA EROS(Intertechnique)35-13-64ComponentMaintenanceManual

35-10-00-912 MC10-15-109 orMC10-16-101Observer/JumpSeat OxygenMask (AccomplishSupplier Testingand Fault IsolationTask) Restoration(If Installed)

35-13-64 Intertechique SA EROS(Intertechnique)35-13-64ComponentMaintenanceManual

35-30-00-960 ProtectiveBreathingEquipment Discard

PRM-01 Essex Industries PRM-01 forthe EssexCrewmember PBE

49-10-00-960 Auxiliary Power UnitCompressor RotorDiscard

49-24-87 Honeywell 36-150 [EMB] APULight MaintenanceManual

49-10-00-220 Auxiliary PowerUnit Igniter PlugsDetailed Inspection


49-10-00-221 Auxiliary PowerUnit Starter MotorBrushes DetailedInspection

SILD201608000071

Honeywell Honeywell ServiceInformation LetterD201608000071

49-10-00-222 Auxiliary PowerUnit Magnetic ChipCollector DetailedInspection


49-10-00-961 Auxiliary PowerUnit Turbine RotorDiscard


49-10-00-962 Auxiliary Power UnitFuel Filter Discard



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49-10-00-963 Auxiliary Power UnitOil Filter Discard


49-10-00-964 Auxiliary Power UnitOil Discard


5-12-00 HoneywellEngine PeriodicInspections

72-05-25 Honeywell HoneywellAerospace72-05-25 EngineLight MaintenanceManual


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FLIGHT COMPARTMENT - INSPECTION/CHECK

1. GeneralA. This section gives the inspections and checks necessary to keep the flight compartment in a

serviceable condition.

Task 25-10-00-220

2. Crew Seat, Seat Rail, and Seat Restraint Detailed InspectionA. Tools and Equipment

NOTE: For the tool, equipment, and special consumable part numbers and the manufacturerdata, refer to Chapter 25, Equipment/Furnishings - General. For the supplier publicationpart number and manufacturer data, refer to the Introduction - Supplier Publication List.

(1) Tools and Equipment• None.

(2) Special Consumables• None.

(3) Reference Material• Chapter 25, Flight Crew Seat - Removal/Installation.

B. Prepare the Airplane for the Crew Seat, Seat Rail, and Seat Restraint Detailed Inspection.(1) Remove the pilot's and the copilot's crew seats from the airplane. Refer to Chapter 25, Flight

Crew Seat - Removal/Installation.

C. Do the Crew Seat Detailed Inspection.(1) Examine the crew seats for rips, tears, cleanliness, security of installation, and other damage.

D. Do the Seat Rail Detailed Inspection.(1) Examine the seat rails and the seat rail holes for cleanliness, cracks, corrosion, loose or missing

fasteners, and other damage.(a) Repair or replace the seat rails as necessary.

E. Do the Seat Restraint Detailed Inspection.(1) Examine the seat restraints for tears, cleanliness, security of installation, and other damage.(2) Make sure that the seat restraints operate correctly.

F. Put the Airplane Back to its Initial Condition.(1) Install the pilot's and the copilot's crew seats. Refer to Chapter 25, Flight Crew Seat - Removal/

Installation.

G. Task Findings.(1) Enter the Task Findings into the maintenance tracking system used, or provide them to Textron

Aviation, Maintenance Engineering, Department 753, 2121 South Hoover Road, Wichita,Kansas 67209, Phone: 316-517-9370, Email: [email protected].

NOTE: An Inspection Document or Inspection Task should only be recorded as completedin the aircraft log after the findings have been entered into the maintenance trackingsystem used, or sent to Textron Aviation, Maintenance Engineering.


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***Findings For Task 25-10-00-220 (Check All That Apply)***Crew Seat(s)

ZONE: 233, 234

No Fault Found Upholstery Damage Roller Damage

Guide Damage Security of Installation Frame Cracked

Fails to Operate Other

NOTES: Mech Insp

Seat Rail(s)ZONE: 233, 234

No Fault Found Corrosion Cracked

Fasteners Missing Worn Other

NOTES: Mech Insp

Seat RestraintZONE: 233, 234

No Fault Found Torn Frayed

Worn Security of Installation Fails to Lock

Other

NOTES: Mech Insp

End of task

Task 25-10-00-221

3. Observer/Jump Seat, Carriage Plate, Seat Rail, and Seat Restraint Detailed Inspection (If Installed)A. Tools and Equipment

NOTE: For the tool, equipment, and special consumable part numbers and the manufacturerdata, refer to Chapter 25, Equipment/Furnishings - General. For the supplier publicationpart number and manufacturer data, refer to the Introduction - Supplier Publication List.



(3) Reference Material• Model 700 Interior Maintenance Manual and Illustrated Parts Catalog.


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B. Prepare the Airplane for the Observer/Jump Seat, Carriage Plate, Seat Rail, and Seat RestraintDetailed Inspection (If Installed).(1) Remove the observer/jump seat from the airplane. Refer to the Model 700 Interior Maintenance

Manual and Illustrated Parts Catalog.

C. Do the Observer/Jump Seat Detailed Inspection.(1) Examine the seat for rips, tears, cleanliness, security of installation, and other damage.

D. Do the Carriage Plate Detailed Inspection.(1) Examine the carriage plate for damage, corrosion, and security of installation.

E. Do the Seat Rail Detailed Inspection.(1) Examine the seat rails and the seat rail holes for cleanliness, cracks, corrosion, loose or missing

fasteners, and other damage.(a) Repair or replace the seat rails as necessary.

F. Do the Seat Restraint Detailed Inspection.(1) Examine the seat restraints for tears, cleanliness, security of installation, and other damage.(2) Make sure that the seat restraints operate correctly.

G. Put the Airplane Back to its Initial Condition.(1) Install the observer/jump seat in the airplane. Refer to the Model 700 Interior Maintenance

Manual and Illustrated Parts Catalog.

H. Task Findings.(1) Enter the Task Findings into the maintenance tracking system used, or provide them to Textron




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***Findings For Task 25-10-00-221 (Check All That Apply)***Observer/Jump Seat

ZONE: 241

No Fault Found Upholstery Damage Roller Damage

Guide Damage Security of Installation Frame Cracked

Fails to Operate Other

NOTES: Mech Insp

Carriage PlateZONE: 241

No Fault Found Corrosion Damage

Security of Installation Other

NOTES: Mech Insp

Seat Rail(s)ZONE: 241

No Fault Found Corrosion Cracked

Fasteners Missing Worn Other

NOTES: Mech Insp

Seat RestraintZONE: 241

No Fault Found Torn Frayed

Worn Security of Installation Fails to Lock

Other

NOTES: Mech Insp

End of task


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CREW OXYGEN SYSTEM - DESCRIPTION AND OPERATION

1. GeneralA. This section gives a description and the operation of the crew oxygen system. The line replaceable

units (LRU's) in the crew oxygen system are the oxygen bottle assembly, crew oxygen mask, crewoxygenmask stowage box, oxygen indicator blow-out disc, oxygen pressure transducer, charge valve,oxygen supply pressure switch, oxygen check valve, and oxygen pressure gage.

B. Refer to Figure 1 for a general view of the crew oxygen system.

2. DescriptionA. Oxygen Bottle Assembly

(1) The oxygen bottle assemblies (77.1 cubic-foot or 115.7 cubic-foot) are installed in the left and theright nose compartment, adjacent to the nose wheel well. The 77.1 cubic-foot bottle assemblyis standard and the 115.7 cubic-foot bottle assembly is optional. The standard configuration hastwo standard oxygen bottle assemblies installed on the left and the right nose compartment,adjacent to the nose wheel well. The extended configuration has one optional oxygen bottleinstalled on the left nose compartment and one standard oxygen bottle installed on the right nosecompartment, adjacent to the nose wheel well. The bottle assembly is a lightweight cylinderwith a seamless aluminum liner that is wound longitudinally and circumferentially with epoxyimpregnated Kevlar. Its usual pressure is 1800 psi (12,411 kPa) at 70°F (21°C).

(2) An integral pressure regulator manifold is installed directly to the end of the oxygen bottle. Youcan select the regulator to the ON or the OFF position with the attached control handle. With thehandle selected to the OFF position, the regulator operates as a shutoff valve. With the handleset and safetied to the ON position, the regulator supplies 70 psi, +10 or -10 psi (482.63 kPa,+68.95 or -68.95 kPa) to each crew outlet and the passenger oxygen control valve.

(3) The oxygen bottle regulator has four ports with lines that connect to each regulator port. Oneport supplies regulated oxygen. The other three ports are a fill port, overboard vent port, andgage port. The fill port lets you do the servicing of the oxygen bottle. The overboard vent portreleases the oxygen from the bottle if an overpressure condition occurs. The gage port lets youmonitor the oxygen bottle pressure.

B. Crew Oxygen Mask(1) The crew oxygen masks are installed in the left and the right side consoles in the cockpit, in the

crew oxygen mask stowage boxes. They are installed near the pilot's and the copilot's outboardleg. Each mask has a mask-installed regulator that supplies independent diluter demand, 100%demand, and pressure demand oxygen flow with regulator adjustments. The N-100% PUSHlever on the mask switches oxygen content between normal (N) and 100% oxygen. For diluterdemand, the N-100% PUSH lever must be lifted to the N position. The diluter demand modesupplies a mixture of air and oxygen. The ratio of air to oxygen is a function of cabin pressure assensed by a regulator on the mask. For 100% oxygen, the crew member pushes the N-100%PUSH lever. If diluter demand or 100% oxygen is selected, oxygen flows through the mask whenthe crew member inhales and stops when they exhale.

(2) If the optional observer/jump seat is installed, an additional crew oxygen mask is installed in theleft cabinet aft of the flight compartment.

(3) When you turn the emergency rotary knob to the full clockwise position, the emergency modeoperates and supplies oxygen under positive pressure in the mask during the breathing cycle.The emergency mode prevents ambient air infiltration if there is smoke or fumes. When youpush one of the two inflation buttons on the mask, the mask's harness inflates and lets it easilyfit over your head. When you release the buttons on the mask, the harness deflates for a tightfit. The mask have internal microphones that let you talk when in use.

(4) The flight crew can talk with the crew oxygen masks on. A microphone is installed in each mask.When you select the MIC SEL switch/light, each microphone operates. TheMIC SEL switch/lightfor the pilot's mask is installed on the left switch panel. The MIC SEL switch/light for the copilot'smask is installed on the right switch panel. The MIC SEL switch/lights let the applicable flightcrew member select between the oxygen mask microphone (MASK) or the headset microphone(HEADSET).


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL

Crew Oxygen SystemFigure 1 (Sheet 1)


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL



ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL

C. Crew Oxygen Mask Stowage Box(1) The crew oxygen mask stowage boxes are installed in the left and the right side consoles

between FS 132.00 and FS 147.50. They are installed near the pilot's and the copilot's outboardleg. Two crew oxygen masks are installed in the cockpit, one in each stowage box. An integralflow indicator and test switch lets the flight crew member do a check of the assembly while thecrew oxygen mask is stowed in the stowage box.

D. Oxygen Indicator Blow-Out Disc(1) The oxygen indicator blow-out disc is installed at FS 48.61, on the right side of the bottom part

of the nose section. The oxygen bottle regulator has overpressure protection. It uses a blow-outdisc that will break and discharge the contents out of the fuselage if the oxygen bottles pressureis more than 2500 to 2775 psi (17,237 to 19,133 kPa). The broken disc releases to an overboardport which is covered with a green blow-out disc. A missing green blow-out disc shows that theoxygen bottle assembly has released.

(2) When the oxygen bottle assembly has released, you must examine it and replace the blow-outdisc. The oxygen bottle regulator is connected to the blow-out disc through a 0.25 inch (6.35-mm) diameter vent line.

E. Oxygen Pressure Transducer(1) The oxygen pressure transducers are installed in the left and right side of the nose compartment

and inboard of the oxygen bottle regulator. The oxygen bottle regulator sends the oxygen bottlepressure to the oxygen pressure transducer through a high-pressure copper capillary gage line.The oxygen pressure transducer connects to an inline tee fitting that is installed between thecapillary line from the oxygen bottle regulator and the capillary line from the oxygen pressuregage. The transducer then supplies the oxygen bottle pressure as an electrical signal to themultifunction display (MFD) in the cockpit. The MFD shows the PSI status of the oxygen bottle.The transducer will cause the amber O2 PRESS LOW L-R crew alerting system (CAS) messageto come on if one of the oxygen bottle pressures decreases to less than 400 psi, +50 or -50 psi(2757.90 kPa, +344.74 or -344.74 kPa).

F. Charge Valve(1) The charge valves are installed in the oxygen service bracket, adjacent to the oxygen pressure

gages in the left side of the nose compartment. The charge valve has an integral filter andorifice and functions as a check valve. The charge valves are connected to the oxygen bottleassemblies through the fill lines. The fill line is a 3/16-inch (4.76 mm) diameter high-pressurecopper line that includes a pressure sealing cap to prevent the contamination.

G. Oxygen Supply Pressure Switch(1) Two oxygen supply pressure switches (left and right) are installed in-line with the oxygen supply

tubes to sense if an oxygen bottle is set to off (closed). The pressure switch operates whenit senses a line pressure less than a minimum of 45 psi (310.26 kPa). When it senses thispressure, the amber O2 BOTTLE OFF L-R CAS message will come on. The pressure switchwill reset and the amber O2 BOTTLE OFF L-R CAS message will go off when it senses a linepressure of 50 to 55 psi (344.74 to 379.21 kPa).

H. Oxygen Check Valve(1) Two oxygen system check valves are installed in the nose section of the airplane, below the

oxygen bottle assemblies. The check valves are installed in-line, between its related oxygenpressure switches and the oxygen tubes. The flow arrows on the check valves must point aftafter you install them. The check valves let the oxygen bottles supply oxygen pressure at equalrates and to prevent backflow from one oxygen bottle into the other.

I. Oxygen Pressure Gage(1) The oxygen pressure gages are installed adjacent to the charge valves in the oxygen service

bracket. They are installed in the left side of the nose compartment and above the nose wheelwell. The gages monitor the oxygen bottle assemblies pressure during servicing. The gagesconnect to the oxygen bottle regulators with a high-pressure copper capillary line.


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL

3. OperationA. General

(1) The oxygen system supplies pressure regulated oxygen to the flight crew constantly and to thepassengers when necessary. The pilot can select the oxygen flow for the flight crew only. Theoxygen system operates at a maximum airplane altitude of 45,000 feet (13,716 m). The oxygensystem is necessary during cabin decompression. The oxygen system takes into considerationthe rate of cabin pressure decrease, flight crew reaction time, and airplane descent rate from45,000 feet (13,716 m). The cabin altitude must not go more than 39,000 feet (11,887 m). Theoxygen systems LRU's can operate from sea level up to 40,000 feet (12,192 m) cabin altitude.The oxygen system operates with oxygen that agrees withMilitary SpecificationMIL-PRF-27210.

B. Crew Oxygen System(1) Oxygen is available to the flight crew at all times. The oxygen pressure is regulated at the two

high-pressure oxygen bottle assemblies with an integral regulator assemblies and downstreamof the bottles by the oxygen sequence regulators. When the regulators on the oxygen bottlesare set to the ON position, the oxygen pressure is supplied to the gages, fill, and supply lines.

(2) Before flight, the pilot will do a check of the oxygen quantity and select the oxygen flow schedule.The two oxygen pressure gages, in the nose, show the pressure in the oxygen bottles. Thepermitted preflight pressure range is shown with a green arc on each gage. The oxygen pressureof each bottle also shows on the multifunction display (MFD) in the cockpit. The permittedpreflight pressure range will show with green text and a green pointer on the MFD. If the oxygenpressure is less than 400 psi (2757.90 kPa), the amber O2 PRESS LOW crew alerting system(CAS) message will come on. If one of the oxygen bottle assemblies is off or if the oxygenpressure is 45 psi (310.26 kPa), the amber O2 BOTTLE OFF L-R CAS message will come on.


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL

CREW OXYGEN SYSTEM - INSPECTION/CHECK

1. GeneralA. This section gives the inspections and checks necessary to keep the crew oxygen system in a

serviceable condition.

Task 35-10-00-220

2. Crew Oxygen Mask and Storage Box Detailed InspectionA. Tools and Equipment

NOTE: For the tool, equipment, and special part numbers and the manufacturer data, refer toChapter 35, Oxygen - General. For the supplier publication part number and manufacturerdata, refer to the Introduction - Supplier Publication List.



(3) Reference Material• Chapter 24, External Electrical Power - Maintenance Practices• Chapter 35, Oxygen - Maintenance Practices• Chapter 35, Crew Oxygen Mask - Removal/Installation.

B. Prepare the Airplane for the Crew Oxygen Mask and Storage Box Detailed Inspection.

WARNING: Before you do maintenance on the oxygen system, obey theoxygen system safety precautions and warnings given inChapter 35, Oxygen - Maintenance Practices.

(1) Disconnect external electrical power from the airplane. Refer to Chapter 24, External ElectricalPower - Maintenance Practices.

(2) Remove the crew oxygenmask. Refer to Chapter 35, CrewOxygenMask - Removal/Installation.

C. Do the Crew Oxygen Mask and Storage Box Detailed Inspection.(1) Examine the crew oxygen mask stowage box for debris, cracks, and security of components.(2) Examine the crew oxygenmasks and the hoses for correct installation, deterioration, cleanliness,

correct stowage, holes, cuts, or tears.(3) Visually examine the crew oxygen mask and the microphone connections for condition and

security of installation.(4) Make sure that the microphone cord on the crew oxygen masks is connected to the fitting on

the pilot's and the copilot's side console.

D. Put the Airplane Back to its Initial Condition.(1) Install the crew oxygen masks. Refer to Chapter 35, Crew Oxygen Mask - Removal/Installation.

E. Task Findings.(1) Enter the Task Findings into the maintenance tracking system used, or provide them to Textron




ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL

***Findings For Task 35-10-00-220 (Check All That Apply)***Storage Boxes (Any)

ZONE: 235, 236

No Fault Found Security of Installation Cracks

Other

NOTES: Mech Insp

Crew Oxygen Mask (Any)ZONE: 235, 236

No Fault Found Damage Deterioration

Leaks Other

NOTES: Mech Insp

End of task

Task 35-10-00-221

3. Oxygen Bottle Detailed InspectionA. Tools and Equipment




(3) Reference Material• Chapter 6, Dimensions and Areas - Description and Operation• Chapter 35, Oxygen - Maintenance Practices.

B. Prepare the Airplane for the Oxygen Bottle Detailed Inspection.


(1) Open the left and the right nose access doors to get access to the left and the right oxygen bottleassemblies. Refer to Chapter 6, Dimensions and Areas - Description and Operation.

C. Do the Oxygen Bottle Detailed Inspection.(1) Examine the oxygen bottle assemblies for correct installation, corrosion, and other damage.


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL

D. Put the Airplane Back to its Initial Condition.(1) Close the left and the right nose access doors. Refer to Chapter 6, Dimensions and Areas -

Description and Operation.




***Findings For Task 35-10-00-221 (Check All That Apply)***Oxygen Bottle (Any)

ZONE: 215, 216

No Fault Found Corrosion Damage

Security of Installation Other

NOTES: Mech Insp

End of task

Task 35-10-00-222

4. Observer/Jump Seat Oxygen Mask Detailed Inspection (If Installed)A. Tools and Equipment




(3) Reference Material• Chapter 24, External Electrical Power - Maintenance Practices• Chapter 35, Oxygen - Maintenance Practices• Chapter 35, Crew Oxygen Mask - Removal/Installation.

B. Prepare the Airplane for the Observer/Jump Seat Oxygen Mask Detailed Inspection (If Installed).



(2) Remove the crew oxygenmask. Refer to Chapter 35, CrewOxygenMask - Removal/Installation.

C. Do the Observer/Jump Seat Oxygen Mask Detailed Inspection (If Installed).(1) Examine the crew oxygen mask stowage box for debris, cracks, and security of components.


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL

(2) Examine the crew oxygen mask and the hoses for correct installation, deterioration, cleanliness,correct stowage, holes, cuts, or tears.

(3) Visually examine the crew oxygen mask and the microphone connections for condition andsecurity of installation.

(4) Make sure that the microphone cord on the crew oxygen mask is connected to the fitting on thejump seat oxygen panel assembly.

D. Put the Airplane Back to its Initial Condition.(1) Install the crew oxygen mask. Refer to Chapter 35, Crew Oxygen Mask - Removal/Installation.




***Findings For Task 35-10-00-222 (Check All That Apply)***Storage Boxes (Any)

ZONE: 241

No Fault Found Security of Installation Cracks

Other

NOTES: Mech Insp

Crew Oxygen MaskZONE: 241

No Fault Found Damage Deterioration

Leaks Other

NOTES: Mech Insp

End of task

Task 35-10-00-780

5. Oxygen Bottle Assembly Restoration (Hydrostatic)A. Tools and Equipment



(2) Special Consumables


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL

• None.(3) Reference Material

• Chapter 35, Oxygen Bottle Assembly - Removal/Installation.

B. Prepare the Airplane for the Oxygen Bottle Assembly Restoration (Hydrostatic).(1) Remove the oxygen bottle assembly. Refer to Chapter 35, Oxygen Bottle Assembly - Removal/

Installation.

C. Do the Oxygen Bottle Assembly Restoration (Hydrostatic).(1) Send the oxygen bottle assembly to an approved repair facility to do the hydrostatic check.

NOTE: You may contact Textron Aviation Parts Department (TAPD) at 316-517-6002for assistance with obtaining a properly restored oxygen bottle assembly and/orreference AVOX System CMM 35-28-98 for 804882 Series Oxygen Bottles.

D. Put the Airplane Back to its Initial Condition.(1) Install the oxygen bottle assembly. Refer to Chapter 35, Oxygen Bottle Assembly - Removal/

Installation.




***Findings For Task 35-10-00-780 (Check All That Apply)***Not Applicable

NOTES: Mech Insp

End of task

Task 35-10-00-910

6. MC10-16-150CrewOxygenMask (Accomplish Supplier Testing and Fault Isolation Task) Restoration(If Installed)A. Tools and Equipment




(3) Reference Material• Chapter 35, Crew Oxygen Mask - Removal/Installation.

B. Prepare the Airplane for the MC10-16-150 CrewOxygenMask (Accomplish Supplier Testing and FaultIsolation Task) Restoration (If Installed).(1) None.


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL

C. Do the MC10-16-150 Crew Oxygen Mask (Accomplish Supplier Testing and Fault Isolation Task)Restoration (If Installed).

NOTE: You may contact Textron Aviation Parts Department (TAPD) at 316-517-6002 forassistance With Obtaining a Properly Restored Full Face Crew Oxygen Mask and/orReference EROS (Intertechnique) 35-13-64 Component Maintenance Manual.

(1) Replace the crew oxygenmask. Refer to Chapter 35, CrewOxygenMask - Removal/Installation.

D. Put the Airplane Back to its Initial Condition.(1) None.





NOTES: Mech Insp

End of task

Task 35-10-00-911

7. MLD20-505 Full Face Crew Oxygen Mask (Accomplish Supplier Testing and Fault Isolation Task)Restoration (If Installed)A. Tools and Equipment





B. Prepare the Airplane for the MLD20-505 Full Face Crew Oxygen Mask (Accomplish Supplier Testingand Fault Isolation Task) Restoration (If Installed).(1) None.


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL

C. Do the MLD20-505 Full Face Crew Oxygen Mask (Accomplish Supplier Testing and Fault IsolationTask) Restoration (If Installed).








NOTES: Mech Insp

End of task

Task 35-10-00-912

8. MC10-15-109 or MC10-16-101 Observer/Jump Seat Oxygen Mask (Accomplish Supplier Testing andFault Isolation Task) Restoration (If Installed)A. Tools and Equipment





B. Prepare the Airplane for the MC10-15-109 or MC10-16-101 Observer/Jump Seat Oxygen Mask(Accomplish Supplier Testing and Fault Isolation Task) Restoration (If Installed).(1) None.


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL

C. Do the MC10-15-109 or MC10-16-101 Observer/Jump Seat Oxygen Mask (Accomplish SupplierTesting and Fault Isolation Task) Restoration (If Installed).








NOTES: Mech Insp

End of task

Task 35-10-00-960

9. Oxygen Bottle Assembly DiscardA. Tools and Equipment




(3) Reference Material• Chapter 35, Oxygen Bottle Assembly - Removal/Installation.

B. Prepare the Airplane for the Oxygen Bottle Assembly Discard.(1) None.

C. Do the Oxygen Bottle Assembly Discard.(1) Remove and discard the oxygen bottle assembly. Refer to Chapter 35, Oxygen Bottle Assembly

- Removal/Installation.


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL

D. Put the Airplane Back to its Initial Condition.(1) Install a replacement oxygen bottle assembly. Refer to Chapter 35, Oxygen Bottle Assembly -

Removal/Installation.

NOTE: You may contact Textron Aviation Parts Department (TAPD) at 316-517-6002 forassistance with obtaining a replacement oxygen bottle assembly.





NOTES: Mech Insp

End of task


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL

CREW OXYGEN MASK - REMOVAL/INSTALLATION

1. GeneralA. This section gives the removal and installation procedures for the crew oxygen mask. For a general

description of the crew oxygen mask, refer to Chapter 35, Crew Oxygen System - Description andOperation.

2. Tools and Equipment

NOTE: For the tool, equipment, and special consumable part numbers and the manufacturer data,refer to Chapter 35, Oxygen - General. For the suppliers publication part number andmanufacturer data, refer to the Introduction - Supplier Publication List.

A. Tools and Equipment• Protective Covers.

B. Special Consumables• None.

C. Reference Material• Chapter 24, External Electrical Power - Maintenance Practices• Chapter 35, Oxygen - Maintenance Practices.

3. SetupA. Prepare the Airplane for the Crew Oxygen Mask Removal.

WARNING: Before you do maintenance on the oxygen system, obey theoxygen system safety precautions and warnings given in Chapter35, Oxygen - Maintenance Practices.

(1) Make sure that you follow the maintenance precautions before you remove and install the crewoxygen mask. Refer to Chapter 35, Oxygen - Maintenance Practices.


(3) If the optional observer/jump seat is installed, open the pocket door on the left forward jump seatcloset to get access to the crew oxygen mask.

4. Crew Oxygen Mask RemovalA. Remove the Crew Oxygen Mask (Refer to Figure 401).

NOTE: The removal of the left and the right crew oxygen masks is typical.

NOTE: If the optional observer/jump seat is installed, an additional crew oxygen mask is locatedin the left forward jump seat closet.

(1) Open the doors on the crew oxygen mask stowage box.(2) Remove the crew oxygen mask from the crew oxygen mask stowage box.(3) Disconnect the oxygen line from the inner side of the crew oxygen mask stowage box.(4) Disconnect the radio connector from the inner side of the crew oxygen mask stowage box.(5) Remove the crew oxygen mask from the airplane.(6) Put protective covers on the open ports.(7) For the observer/jump seat crew oxygen mask, do as follows:

(a) Remove the crew oxygen mask from the left forward jump seat closet.


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL

Crew Oxygen Mask InstallationFigure 401 (Sheet 1)


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL

Crew Oxygen Mask InstallationFigure 401 (Sheet 2)


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL

5. Crew Oxygen Mask InstallationA. Install the Crew Oxygen Mask (Refer to Figure 401).

NOTE: The installation of the left and the right crew oxygen masks is typical.

NOTE: Before you install the crew oxygen mask into the crew oxygen mask stowage box, putthe smoke goggles inside the bag provided and put the bag at the bottom of the crewoxygen mask stowage box.

NOTE: Put the crew oxygen mask on top of the smoke goggles inside the crew oxygen maskstowage box.

(1) For the observer/jump seat crew oxygen mask, do as follows:(a) Install the crew oxygen mask in the left forward jump seat closet.

(2) Remove the protective covers from the ports.(3) Connect the oxygen line to the bottom of the crew oxygen mask stowage box.(4) Connect the radio connector to the bottom of the crew oxygen mask stowage box.(5) Make sure that the oxygen line and the radio connector are correctly installed in the crew oxygen

mask stowage box.(6) With the harness deflated, hold the facepiece with one hand and let the harness hang below the

facepiece.(7) Wind the hose into a coil.

(a) Put the coil in the crew oxygen mask stowage box.(8) Put the harness in the crew oxygen mask stowage box.

(a) Make sure that the harness is installed between the coiled hose and the crew oxygenmask.(9) Make sure that the last six inches (152.4 mm) of the hose is installed between the doors.

NOTE: This will let the doors close correctly.

(10) Push the crew oxygen mask into the crew oxygen mask stowage box until it is installed againstthe top stop.

CAUTION: Do not operate the red levers on the regulator facepiece. This willcause the harness to inflate and will push the stowed harness outof the crew oxygen mask stowage box.

(11) Close the doors.(12) Make sure that you can see the OXY ON flag on the right side of the left door.

6. Crew Oxygen Mask Post-Maintenance ChecksA. Do the Crew Oxygen Mask Post-Maintenance Checks.

(1) Push the PRESS TO TEST AND RESET button on the crew oxygen mask.(a) Make sure that the OXY ON flag goes out of view.(b) Engage the door pin on the left door.(c) Close the right door and make sure that the crew oxygen mask is correctly installed in the

crew oxygen mask stowage box.(2) To do a check of the crew oxygen mask with the mask stowed, do as follows:

(a) Push the PRESS TO TEST ANDRESET button on the crew oxygenmask and hold it down.1 Make sure that the blinker shows yellow and then shows black.2 If the blinker stays yellow and does not turn to black, then there is a leak in the system

and you must correct it.3 While you continue to push the PRESS TO TEST AND RESET button on the crew

oxygen mask, push the PRESS TO TEST knob on the oxygen sequence regulatorfor one second.

4 Make sure that the blinker shows yellow and then black, which will show that thedemand from the oxygen sequence regulator is correct.


ICA-700-25-00001 Form 2261 Rev 1

CESSNA®MODEL 700

MAINTENANCE MANUAL

(b) Release the PRESS TO TEST AND RESET button on the crew oxygen mask.

7. CloseoutA. Put the Airplane Back to its Initial Condition.

(1) If the optional observer/jump seat is installed, close the pocket door on the left forward jump seatcloset.


ICA-700-25-00001 Form 2261 Rev 1



SUPPLEMENT NO: ICA-700-25-00001

APPENDIX A: ILLUSTRATED PARTS CATALOG

NOT APPLICABLE





APPENDIX B: WIRING DIAGRAM MANUAL

NOT APPLICABLE





APPENDIX C: INTERIOR MAINTENANCE MANUAL AND ILLUSTRATED PARTSCATALOG


Subject Forward Maintenance Parts

CESSNA®

MODEL 700INTERIOR MAINTENANCE MANUAL AND ILLUSTRATED PARTS CATALOG

Left-Hand Forward Closet..................................................................................25-20-35 .................25-20-36

Table of Contents

Passenger Compartment

ICA-700-25-00001

25-20-35 Sep 26/2019

CESSNA®


LEFT-HAND FORWARD CLOSET WITH JUMPSEAT - MAINTENANCE

1. General

A. The forward closet is located in the forward section of the passenger compartment on the left-hand side,forward of entry door.

B. For interior wiring diagrams and routings, refer to 25-90 - Electrical.

CAUTION: All electrical components should be properly secured and have electrical wire bundle(s)properly routed and secured.

2. Left-Hand Forward Closet Removal/Installation

A. Remove Left-Hand Forward Closet.

(1) Disengage appropriate circuit breakers. Circuit breaker is located in the aft electrical rackin the aft baggage compartment.

NOTE: Remove loose items from closet (fire extinguisher, removable shelves, flight manuals, etc.). Closet doors can be removed prior to closet removal to lighten closet and prevent damage to doors.

(2) Remove entryway acoustic curtain. Refer to Chapter 25-20-13 Acoustic Curtain - Maintenance in thismanual.

(3) Position crew seat forward or remove if necessary to gain access to navigation chart case and screws.(4) Remove two (2) screws securing chart case to divider and pull chart case inboard slightly and

disconnect electrical wiring.(5) Once wiring is disconnected, remove chart case, being careful to not damage chart case or aircraft

surroundings. Refer to Chapter 25-10-07 Chart Case - Maintenance in this manual. Tag screws forinstallation.

(6) Remove cockpit curtain or cockpit divider. Refer to Chapter 25-20-01 in this manual.(7) Remove jumpseat. Refer to instructions below.(8) Open cabinet door to gain access to screws securing removable header to closet cabinet. Four (4)

screws are located in top of this compartment and screw up and into header above. Remove headerand tag screws for installation.

(9) Remove pin closeout on upper aft side of left-hand forward closet. Closeout is held in place withmagnets.

(10) Retract two (2) upper installation pins.(11)Remove four (4) screws securing outboard access panel and remove panel from closet to gain access

to installation pin.(12) Remove button plug on forward lower outboard side of forward closet. Retract outboard installation pin.(13) Remove floor panel by pulling upward on panel. Floor panel is held in place with grabber catches(14) Remove one (1) plug, one (1) bolt and one (1) washer securing closet to floorboard attach brackets

and tag for installation.(15) Disconnect all electrical wiring between closet and shipside.

CAUTION: Two people are required to maneuver closet to prevent damage or injury.

(16) Cover closet and remove from aircraft, being careful not to damage closet or surroundings.

B. Install Left-Hand Forward Closet.

(1) Position closet in aircraft near installed position.

CAUTION: Two people are required to maneuver closet to prevent damage or injury.

(2) Reconnect electrical wiring between closet and shipside.

ICA-700-25-00001

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CESSNA®



(3) Install three (3) closet installation pins, two (2) on upper side and one (1) on outboard side.(4) Install one (1) bolt, one (1) washer and one (1) plug securing closet to floorboards.(5) Install floor panel by putting in installed position and pressing firmly to engage grabber latches.(6) Secure header to cabinet with four (4) screws.(7) Install cockpit curtain or cockpit divider. Refer to Chapter 25-20-01 in this manual.(8) Re-install jumpseat. Refer to instructions below.(9) Place chart case near installed position and reconnect electrical wiring.(10) Secure to chart case to cabinet with two (2) screws.(11) Re-install entryway acoustic curtain. Refer to Chapter 25-20-13 Acoustic Curtain - Maintenance in this

manual.(12) Engage appropriate circuit breakers.(13) Check electrical components for proper operation.

NOTE: Replace loose items previously removed from closet. Replace closet doors if previously removed.

(14) Check electrical equipment for proper operation.

3. XM Receiver Removal/Installation

A. Remove XM Receiver.

(1) Disengage FWD CLOSET circuit breaker.(2) Remove closet. Refer to instructions above.(3) Remove four (4) screws securing XM receiver to outboard side of cabinet.(4) Remove XM Reciever from aircraft.

B. Install XM Receiver.

(1) Place XM Receiver back in installed position and secure with four (4) screws.(2) Re-install left-hand forward closet. Refer to instruction above..(3) Check controls and electrical equipment for proper operation.(4) Check electrical equipment for proper operation.

4. Microwswitch Removal/Installation

A. Remove Microswitch.

(1) Disengage FWD CLOSET circuit breaker.(2) Remove two (2) screws securing microswitch closeout to cabinet.(3) Disconnect electrical wiring.(3) Remove Microswitch.

B. Install Microswitch.

(1) Place microswitch in proper position.(2) Reconnect electrical wiring.(3) Place microswitch cover in installed position and secure to cabinet wtih two (2) screws.(4) Engage FWD CLOSET circuit breaker.(5) Check controls and electrical equipment for proper operation.

ICA-700-25-00001

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CESSNA®



5. Observer/Jump Seat Removal/Installation

A. Remove observer/Jump Seat.

(1) Open observer/jump seat closet door and slide outboard to stow.(2) Lift seat track foot lever and slide observer/jump seat out of closet until seat track pin locks into deployed

position.(3) Lift gas spring lever to release pressure from gas spring.(4) Remove detent clevis pin securing gas spring to carriage plate. Tag pin for installation.(5) Remove detent clevis pin securing aft leg linkage to carriage plate. Tag pin for installation.(6) Remove two (2) positive lock pins securing seat base to carriage plate.(7) Remove observer/jump seat from aircraft, being careful not to damage seat, closet or interior furnishings.

A. Install Observer/Jump Seat.

(1) Place observer/jump seat into position on carriage plate.(2) Secure seat base to carriage plate with two (2) positive lock pins.(3) Secure aft leg linkage to carriage plate with detent clevis pin.(4) Secure gas spring to carriage plate with detent clevis pin.(5) Lower gas spring lever.(6) Check observer/jump seat for proper operation.(7) Recline seat back, fold seat pan up, unlock aft leg, fold seat up, and slide jump seat into closet until

seat track pin locks in place.(8) Close closet door.

ICA-700-25-00001

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CESSNA®


DETAIL A

A

7,26,55

6,56,57

8

15,16,19

1,3,25,27

13,24 30

33

14,54

2,3

6364

7,26,46,55

34

31,47,48,49,50

4

12,62

61

29,51,52,53

28,59

35

515,16,21

36,37,3842,43,44

39,40,41

17

15,16,19

25,60

18 28,58

22

23

32

45

15,16,20

ICA-700-25-00001

25-20-36-01 Sep 26/2019

CESSNA®


B

DETAIL B

DETAIL C

DETAIL D

DETAIL E

9

10

11

E

E

DE

C

ICA-700-25-00001

25-20-36-01 Sep 26/2019

No. Part Number Description Qty. Vendor

CESSNA®


- 3679046-1 LH FWD JUMPSEAT CLOSET - PASSENGER 1 . CLE106-02-30 6” CABINET LIGHT - 3000K 2 0GZF32 . CLE305-01-30 5” FLOOD LIGHT 1 0GZF33 . DALCLP-105 MOUNTING CLIP 4 0GZF34 . PIN100-01 PIN SPOT LIGHT - 3000K 1 0GZF35 . S-1025-1 BLACK RUBBER BUMPER 2 4W9536 . SAM320-1 LATCH ASSY - SINGLE POINT 2 318457 . SAM320-60 LATCH ASSY - TWO POINT 3 318458 . SWP500-01 CABIN ENTRY DOOR SWITCH 1 0GZF39 . S4500-12 SILKSCREEN - WEIGHT LIMIT(40LBS) 1 7EK5010 . S4500-60 SILKSCREEN - WEIGHT LIMIT(75LBS) 1 7EK5011 . S4500-7 SILKSCREEN - WEIGHT LIMIT(15LBS) 3 7EK5012 . V7-1B17D8-263 MICROSWITCH 1 9192913 . V7-6B19D8-057 MICROSWITCH 2 9192914 . 1DM1 MICROSWITCH (LONG) 1 9192915 . 12325-17 WIRE STRIKER 7 7EK5016 . 12325-19 STRIKER CLAMP 8 7EK5017 . 12325-41-250 WIRE STRIKER 1 7EK5018 . 12325-47-12 SPACER/STOP BLOCK 1 7EK5019 . 12325-47-25 SPACER/STOP BLOCK 4 7EK5020 . 12325-47-38 SPACER/STOP BLOCK 2 7EK5021 . 12325-47-50 SPACER/STOP BLOCK 1 7EK5022 . 12670-11 4.50” LID/DOOR STAY 2 7EK5023 . 12670-9 3.90” LID/DOOR STAY 1 7EK5024 . 12951-1 MICROSWITCH MOUNTING BLOCK 1 4W95325 . 13011-31 LIGHT LENS 2 7EK5026 . 13065-23 BOLT HOUSING ASSY 5 7EK5027 . 13078-3 COVER PLATE KIT 2 7137928 . 175H7100 MOUNTING PLATE 7 0BN6029 . 175H9160 MOUNTING PLATE 4 0BN6030 . 3679002-25 ENTRY SWITCH BRACKET 1 7137931 . 3679009-5 LIGHT LENS 1 7137932 . 3679046-3 JUMP SEAT DOOR INSTL 1 71379

NOTE: Parts not available as complete installations.When ordering plated parts, the plating number found in section 25-00-06 must follow the part number without a space.

ICA-700-25-00001

25-20-36-01 Sep 26/2019


CESSNA®


- 3679046-1 LH FWD JUMPSEAT CLOSET - PASSENGER CONT’D 33 . 3679047-1 LH JUMPSEAT CLOSET SHELL 1 7137934 . 3679047-15 FIRE EXTINGUISHER STOP BLOCK 1 7137935 . 3679047-16 FIRE EXTINGUISHER CRADLE 1 7137936 . 3679047-17 REMOVABLE SHELF ASSY 1 7137937 . . 2055785-1 HINGE/L 2 8301438 . . 2055785-2 HINGE/R 2 8301439 . 3679047-24 ADJUSTABLE SHELF ASSY 3 7137940 . . 2055785-1 HINGE/L 6 8301441 . . 2055785-2 HINGE/R 6 8301442 . 3679047-25 ADJUSTABLE SHELF ASSY 3 7137943 . . 2055785-1 HINGE/L 6 8301444 . . 2055785-2 HINGE/R 6 8301445 . 3679047-27 COVER PANEL 1 7137946 . 3679047-9 BOLT HOUSING ASSY 1 7137947 . 3679071-4 LIGHT ASSEMBLY 1 7137948 . . LTBLK-4X8-02-30 LIGHT BLOCK 1 0GZF349 . . S-1070-10-0050 STANDOFF 4 4W95350 . . 3679071-5 LIGHT MOUNTING PLATE 1 7137951 . 3679074-14 HINGE - MOD 4 7137952 . . T090S00687T TRUSS HEAD STEEL RIVET 4 9U73553 . . 79A5493BT BLUM - 15 ANGLE HINGE 4 0BN6054 . 3679074-9 MICROSWITCH CLOSEOUT 1 7137955 . 3679176-7 BACK PLATE 3 7137956 . 3679203-2 LATCH BACKER INSTL 2 7137957 . . 3679203-3 LATCH BLOCK BACKER - AL 2 7137958 . 70T3550.TL BLUM HINGE - 110 DEGREE 3 0BN6059 . 70T3650.TL BLUM HINGE 2 0BN6060 . 70T3750.TL BLUM HINGE - 110 DEGREE F/S 2 0BN6061 . 81329-1-3-1036 COAT ROD ASSY 1 7EK5062 . 81413-57 MICRO SWITCH SPACER 1 4W95363 . 99K32.13 CIRCULAR MAGNET - 1” 6 LVTL64 . 99K32.55 STEEL CUP - 1” 6 LVTL


ICA-700-25-00001

25-20-36-02 Sep 26/2019

CESSNA®


A

DETAIL A

B

DETAIL BDETAIL C

C

C

C

1

11

7

6,8

5

2,3

4

9,107

7

7

9,107

7

7

ICA-700-25-00001

25-20-36-02 Sep 26/2019


CESSNA®


- 3679046-3 JUMP SEAT DOOR INSTL 1 . S-1070-1 CAP 1 4W9532 . 3679047-20 HINGE ASSY 3 713793 . . MS20001-4-150 HINGE 3 969064 . . MS20001-9-150 HINGE 3 969065 . . NAS561C3-24 PIN 3 802056 . 3679047-3 DOOR CARRIER ASSY 1 713797 . . MS21075-08N NUTPLATE 10 802058 . . 3679047-4 MOUNTING PLATE 1 713799 . . 3679047-8 TRACK ASSY 2 7137910 . . . 408.11.354 BALLBEARING SLIDE 2 HAAM11 . 3679047-5 DOOR GUIDE 1 71379


ICA-700-25-00001

25-20-36-03 Sep 26/2019

CESSNA®


A

DETAIL A

36

35,371

224

25,26 2827,29

4,5,6,7,8

42,43,44,45

3

32,33

19

34

11,12,13,14,15

30,3120

22

21,23

2

16,17,18

38

39,40,41,46

2

9

10

ICA-700-25-00001

25-20-36-03 Sep 26/2019


CESSNA®


- 3679047-1 LH JUMPSEAT CLOSET SHELL 1 . AEP1035-08C375 INSERT FLOATING NUT 2 08ST22 . NAS451-30 BUTTON PLUG 3 802053 . NAS451-52 BUTTON PLUG 1 802054 . 3619142-35 SPRING PIN ASSEMBLY 1 713795 . . NAS561P4-16 PIN 1 802056 . . S2951-61 SPRING 1 7EK507 . . 3619142-33 SPRING PIN HOUSING 1 713798 . . 3619142-34 SPRING PIN 1 713799 . 3679010-3 FWD PANEL CONTOUR - FWD 1 7137910 . 3679010-4 FWD PANEL CONTOUR - AFT 1 7137911 . 3679012-4 SPRING PIN ASSY 1 7137912 . . NAS561P4-16 PIN 1 8020513 . . S2951-61 SPRING 1 7EK5014 . . 4479043-11 HOUSING 1 7137915 . . 4479043-9 PIN 1 7137916 . 3679030-10 RECEPTACLE PLATE ASSY 2 7137917 . . S1115-19 RECEPTACLE 2 7137918 . . 3679030-11 RECEPTACLE PLATE 2 7137919 . 3679047-13 ACCESS PANEL 1 7137920 . 3679047-14 ACCESS PANEL 1 7137921 . 3679047-18 ANGLE ASSY 2 7137922 . . MS21059L08 NUTPLATE 4 9690623 . . 3679047-19 ANGLE 2 7137924 . 3679047-21 MOTOR ACCESS PANEL 1 7137925 . . S1115-71 FASTENER 2 7137926 . . S1115-9 RING 2 7137927 . 3679047-22 ANGLE ASSY 2 7137928 . . MS21059L06 NUTPLATE 2 9690629 . . 3679047-23 ANGLE 2 7137930 . 3679047-26 BACKSHELL BRACKET 1 7137931 . . S2821-18 CUTOUT - ELECTRICAL CONN 1 7137932 . 3679047-6 TOE KICK ASSEMBLY 1 7137933 . . DALCLP-105 MOUNTING CLIP 2 0GZF334 . 3679047-7 JUMPSEAT RUB STRIP 2 7137935 . 3679074-10 MOUNT PLATE ASSEMBLY 1 7137936 . . MS21062L3 NUTPLATE 4 8020537 . . 3679074-11 PLATE 1 7137938 . 3679074-5 HEADER ASSEMBLY 1 7137939 . 3679089-6 PIN COVER 1 7137940 . . 99K32.03 CIRCULAR MAGNET 3/8” 4 LVTL41 . 4479043-11 HOUSING 1 7137942 . 4769014-89 PIN ASSY 1 7137943 . . NAS561-4-6 PIN 1 8020544 . . 4769014-88 PIN 1 7137945 . . . BLC6RC50SF QUICK RELEASE PIN 1 8425646 . 99K32.62 WASHER 3/8” MAGNET 4 LVTL


ICA-700-25-00001

25-20-36-04 Sep 26/2019

CESSNA®


A

DETAIL A

DETAIL B

B

1

2

3

5

6

7

4

ICA-700-25-00001

25-20-36-04 Sep 26/2019


CESSNA®


- 3679047-9 BOLT HOUSING ASSY 1 . MS35206-227 SCREW 1 802052 . NAS1149FN632P WASHER 1 802053 . NAS43DD1-7N SPACER 1 802054 . S-2237-11 END FITTING ASSY 1 318455 . 3679047-10 BOLT HOUSING 1 713796 . 3679047-11 BELL CRANK 1 713797 . 3679047-12 BOLT 1 71379


ICA-700-25-00001

25-20-36-05 Sep 26/2019

CESSNA®


DETAIL A

A

1

9

4

8

10,12

11

3

6 5

2

39

7

37

36,38,40,42

41

43

47

49

44,46,48

45

ICA-700-25-00001

25-20-36-05 Sep 26/2019

CESSNA®


B

DETAIL B

DC

E

F

DETAIL C DETAIL D DETAIL E

DETAIL F18

22

16

26

13,25,27

29,31

30

18

18

15

18

22

16

24

20

17

2314

28

19

32,34

35

33

21

22

16

ICA-700-25-00001

25-20-36-05 Sep 26/2019


CESSNA®


- 3619384-1 JUMPSEAT CLOSET WITH CURTAIN INSTL 1 . AN525-8R6 SCREW 1 802052 . CM2-110AST SHOCK MOUNT 1 79413 . MS27039-0804 SCREW 2 802054 . MS27039-1-09 SCREW 2 802055 . MS27039-4-09 SCREW 4 802056 . MS35307-360 BOLT 1 802057 . MS35335-35 WASHER 1 969068 . NAS1149F0332P WASHER 2 802059 . 3619384-3 COCKPIT FLOOR BRACKET 1 7137910 . 3619384-4 FLOOR PLATE ASSY 1 7137911 . . SL2337-08 ISOLATOR MOUNT 1 9739312 . . 3619384-5 FLOOR PLATE 1 7137913 . 7491044-1 FLOORBOARD INSTL 1 7137914 . . MS21075L08N NUTPLATE 2 8020515 . . MS21075L3N NUTPLATE 6 8020516 . . MS21083N3 NUT 4 8020517 . . MS24693-S25 SCREW 2 8020518 . . MS24694-S55 SCREW 28 8020519 . . MS27039-1-07 SCREW 4 8020520 . . MS35206-226 SCREW 2 8020521 . . NAS1149FN616P WASHER 2 8020522 . . NAS1149G0316P WASHER 4 8020523 . . 7491044-11 SPACER 2 7137924 . . 7491044-12 COVER 1 7137925 . . 7491044-2 SUPPORT FITTING ASSY CAB FL 1 7137926 . . . MS21209F1-15P INSERT 7 8020527 . . . 7491044-3 SUPPORT FITTING CAB FLOOR 1 7137928 . . 7491044-4 SUPPORT FITTING CAB FLOOR 1 7137929 . . 7491044-5 FLOORBOARD ASSY - CTR FWD 1 7137930 . . . GAA588B-3 INSERT 4 08ST231 . . . 7491044-6 FLOORBOARD - CTR FWD 1 7137932 . . 7491044-7 FLOORBOARD ASSY - LH FWD 1 7137933 . . . 7491044-10 FLOORBOARD SHIM 1 7137934 . . . 7491044-8 FLOORBOARD - LH FWD 1 7137935 . . . 7491044-9 FLOORBOARD SHIM 1 7137936 . 7498156-11 JUMP SEAT ANCHOR MOD 1 7137937 . . NAS1351-3-8P SCREW 4 8020538 . . 7498156-13 ANCHOR ASSY - LH JUMPSEAT MOD 1 7137939 . . . MS21055L3 NUTPLATE 2 8020540 . . . 7408906-116 ANCHOR CLIP ASSY 1 7137941 . . . . S1741-1 ANCHOR 8 7137942 . . . . 7408906-117 ANCHOR CLIP 1 7137943 . . . 7498156-15 ANCHOR MOD SHIM 1 7137944 . . 7498156-14 ANCHOR ASSY - RH JUMPSEAT MOD 1 7137945 . . . MS21055L3 NUTPLATE 2 8020546 . . . 7408906-116 ANCHOR CLIP ASSY 1 7137947 . . . . S1741-1 ANCHOR 8 7137948 . . . . 7408906-117 ANCHOR CLIP 1 7137949 . . . 7498156-15 ANCHOR MOD SHIM 1 71379


ICA-700-25-00001

25-20-36-06 Sep 26/2019

CESSNA®


DETAIL B

A

DETAIL A

B4

ICA-700-25-00001

25-20-36-06 Sep 26/2019

CESSNA®


DETAIL C

1

2

1

22

1

1

1

1

5

3

C

1

11

ICA-700-25-00001

25-20-36-06 Sep 26/2019


CESSNA®


- 3619461-1 JUMPSEAT INSTL 1 . MS16996-14 SCREW 7 802052 . MS16996-16 SCREW 3 802053 . 301751016949000 HSR20 - 826LE RAIL 1 1GHA44 . 3619462-1 JUMPSEAT ASSY 1 713795 . 3619464-24 CARRIAGE ASSY 1 71379


ICA-700-25-00001

25-20-36-07 Sep 26/2019

CESSNA®


DETAIL A

A

7,9

1

8

1

4

5

11

6

6

3

10

2

ICA-700-25-00001

25-20-36-07 Sep 26/2019


CESSNA®


- 3619464-24 CARRIAGE ASSY 1 . DEC-1-C DETENT CLEV PIN .440 GRP 2 0CUJ42 . LC-026E-13 SPRING 1 848303 . MS16996-14 SCREW 8 802054 . MS21042-3 NUT 8 802055 . NAS1149F0332P WASHER 8 802056 . 301361018890400 HSR20B1SSE BLOCK 2 1GHA47 . 3619464-25 FOOT LEVER ASSY 1 713798 . . S4509-6 PLACARD - LIFT 1 7EK509 . . 3619464-27 FOOT LEVER 1 7137910 . 3619464-26 CARRIAGE PIN 1 7137911 . 3619464-51 CARRIAGE PLATE 1 71379


ICA-700-25-00001

25-20-36-08 Sep 26/2019

CESSNA®


A

DETAIL A

7,8,9,10,11

13,14,15,16,17

12

18

1

1

1

1

2

2

3,4,5,6

ICA-700-25-00001

25-20-36-08 Sep 26/2019


CESSNA®


- 3619462-1 JUMPSEAT ASSY 1 . AN525-832R9 SCREW 4 802052 . PL5-1250 POSITIVE LOCK PINS 2 0CUJ43 . 3619463-1 HEADREST UPHOLSTERY ASSY 1 713794 . . 3619463-4 COVER ASSY - HEADREST 1 713795 . . 3619463-6 HEADREST PAD ASSY 1 713796 . . 6519801-66 I.D. TAG 1 713797 . 3619463-2 BACK CUSHION UPHOLSTERY ASSY 1 713798 . . 3619463-13 COVER ASSY 1 713799 . . 3619463-16 BACK PAD ASSY 1 7137910 . . 3619463-23 BOXING PAD 2 7137911 . . 6519801-66 I.D. TAG 1 7137912 . 3619463-21 BACK SHROUD 1 7137913 . 3619463-3 BOTTOM CUSHION UPHOLSTERY ASSY 1 7137914 . . 3619463-17 COVER ASSY 1 7137915 . . 3619463-20 BUCKET PAD 1 7137916 . . 3619463-24 BOXING PAD 1 7137917 . . 6519801-66 I.D. TAG 1 7137918 . 3619464-1 JUMPSEAT FRAME ASSY 1 71379


ICA-700-25-00001

25-20-36-09 Sep 26/2019

CESSNA®


DETAIL A

A20

22

21

25

26

ICA-700-25-00001

25-20-36-09 Sep 26/2019

CESSNA®


B

DETAIL B

1513

15

13

10

11

17

18

13

13

9

18

ICA-700-25-00001

25-20-36-09 Sep 26/2019

CESSNA®


C

DETAIL C

1

2

14

128

16

12

14

12

18

18

ICA-700-25-00001

25-20-36-09 Sep 26/2019

CESSNA®


24

7

5,6

D

DETAIL DDETAIL E

E

4

4

3

23

19

12

8

12 12

12 1212

ICA-700-25-00001

25-20-36-09 Sep 26/2019


CESSNA®


- 3619464-1 JUMPSEAT FRAME ASSY 1 . AN4-17A BOLT 2 880442 . AN970-4 WASHER 2 802053 . C16-18802 GAS SPRING 1 5V3134 . DEC-1-C DETENT CLEV PIN .440 GRP 2 0CUJ45 . JRS-135/24-1 GLIDE PAD 46 0JFH86 . JRS-135/24FS-1 GLIDE PAD 2 0JFH87 . MS16996-24 SCREW 10 802058 . MS21042-4 NUT 12 802059 . MS21042-5 NUT 2 8020510 . MS24694-S51 SCREW 2 8020511 . MS35206-231 SCREW 2 8020512 . NAS1149F0432P WASHER 22 8020513 . NAS1149F0532P WASHER 4 8020514 . NAS43DD4-8N SPACER 2 8020515 . NAS464P5A27 BOLT 2 8020516 . SSLR375 HEX DRIVE PLUNGER 1 122617 . SSMD50A BALL PLUNGER 2 122618 . S1438-43 WASHER 4 7EK5019 . 3619464-2 SWIVEL PLATE ASSY 1 7137920 . 3619464-3 HEADREST STRUCTURE ASSY 1 7137921 . 3619464-4 BACK STRUCTURE ASSY 1 7137922 . 3619464-5 SEAT BUCKET ASSY 1 7137923 . 3619464-52 END FITTING 2 7137924 . 3619464-59 SWIVEL COLLAR 1 7137925 . 3619464-6 BASE ASSY 1 7137926 . 9919193-1 4 - PT RESTRAINT ASSY 1 71379


ICA-700-25-00001

25-20-36-10 Sep 26/2019

CESSNA®


DETAIL A

A

103

4

4

7

8

9

3

104

4

2 6

51

26

1

5

ICA-700-25-00001

25-20-36-10 Sep 26/2019


CESSNA®


- 3619464-2 SWIVEL PLATE ASSY 1 . MS21042-4 NUT 4 802052 . MS21042-5 NUT 4 802053 . MS24694-S120 SCREW 4 802054 . MS24694-S150 SCREW 4 802055 . NAS1149F0432P WASHER 4 802056 . NAS1149F0532P WASHER 4 802057 . 3619464-12 PIVOT BRACKET - RH 1 713798 . 3619464-13 PIVOT BRACKET - LH 1 713799 . 3619464-20 SWIVEL PLATE 1 7137910 . 3619464-44 PIN BLOCK - SWIVEL 2 71379


ICA-700-25-00001

25-20-36-11 Sep 26/2019

CESSNA®


DETAIL A

A

1

1

3

4

4

2

2

ICA-700-25-00001

25-20-36-11 Sep 26/2019


CESSNA®


- 3619464-3 HEADREST STRUCTURE ASSY 1 . AN316-8R NUT 4 880442 . S1050-1-2.57 GROMMET 2 713793 . 3619464-48 HEADREST PLATE 1 713794 . 3619464-8 HEADREST TUBE 2 71379


ICA-700-25-00001

25-20-36-12 Sep 26/2019

CESSNA®


DETAIL A

16

2,5,11

23,25

24

428

3

14

15

428

3

14

15

13

13

21

20

19 22 10

17

23,25

24

27

27

1 11

111

18

26

8

7

9

12

7

11 6

6,11

A

10

10

10

10

ICA-700-25-00001

25-20-36-12 Sep 26/2019


CESSNA®


- 3619464-4 BACK STRUCTURE ASSY 1 . AN3-13A BOLT 2 802052 . AN525-832R7 SCREW 4 802053 . LC-026E-13 SPRING 2 848304 . MS20392-1R7 PIN 2 802055 . MS21042-08 NUT 4 802056 . MS21042-3 NUT 8 802057 . MS24694-S50 SCREW 4 802058 . MS24694-S71 SCREW 2 802059 . MS24694-S84 SCREW 2 8020510 . MS51021-115 SETSCREW 6 8020511 . NAS1149F0332P WASHER 14 8020512 . 3619464-10 TORQUE TUBE 1 7137913 . 3619464-11 BACK BEAM 2 7137914 . 3619464-21 PIN 2 7137915 . 3619464-22 LINK 2 7137916 . 3619464-35 BACK PAN 1 7137917 . 3619464-37 ROD 2 7137918 . 3619464-38 CROSS MEMBER 1 7137919 . 3619464-45 BACK PLATE 1 7137920 . 3619464-46 BACK PLATE - CENTER 1 7137921 . 3619464-47 BACK PLATE - TOP 1 7137922 . 3619464-49 COUPLING 1 7137923 . 3619464-56 LEVER ASSY 2 7137924 . . S4509-9 PLACARD - BACK RELEASE 2 7EK5025 . . 3619464-23 LEVER 2 7137926 . 3619464-9 TOP BRACE 1 7137927 . 4319141-15 HEADREST BUSHING 2 7137928 . 98335A031 R - CLIP PIN 2 39428


ICA-700-25-00001

25-20-36-13 Sep 26/2019

CESSNA®


DETAIL A

A

11

5

8

4

8

5

8 4

85

8

18910

3

122 7

13

12

8

76

8

4

58

14

ICA-700-25-00001

25-20-36-13 Sep 26/2019


CESSNA®


- 3619464-5 SEAT BUCKET ASSY 1 . AN3-10A BOLT 1 802052 . MS21042-06 NUT 2 802053 . MS21042-3 NUT 1 802054 . MS27039-1-07 SCREW 4 802055 . MS27039-1-18 SCREW 4 802056 . MS35206-229 SCREW 2 802057 . NAS1149FN632P WASHER 4 802058 . NAS1149F0332P WASHER 10 802059 . NAS43DD3-36N SPACER 1 8020510 . S1551-1 ROLLER 1 7137911 . 3619464-15 BUCKET PAN 1 7137912 . 3619464-18 BUCKET SIDE FRAME 2 7137913 . 3619464-19 BUCKET CROSS MEMBER 1 7137914 . 3619464-55 ROLLER BRACKET 1 71379


ICA-700-25-00001

25-20-36-14 Sep 26/2019

CESSNA®


DETAIL A

A 1

2428

27

2824

3126229

22

20

19

13

23

10

36

35

30

241111

2430

33

2428

41

40,42

27

4

34

29

3

25 6529

237

38 8

2114

32

65

3

9,15,22

7,20

46

43

22

222

944

821

39

1722

2212

21

16

172318

22

17

22

45

5

6

4712

66

ICA-700-25-00001

25-20-36-14 Sep 26/2019

CESSNA®


B

6362,64

53

49

50

61

48,56

52

53

5957,58

5960

5154

55

DETAIL B

ICA-700-25-00001

25-20-36-14 Sep 26/2019


CESSNA®



- 3619464-6 BASE ASSY 1 . AN3-10A BOLT 1 802052 . AN3-7A BOLT 2 802053 . DEC-1-C DETENT CLEV PIN .440 GRP 2 0CUJ44 . DEC-1-C1 DETENT CLEVIS PIN 1 0CUJ45 . LC-026E-13 SPRING 1 848306 . MS20392-1R21 PIN 1 802057 . MS21042-06 NUT 2 802058 . MS21042-08 NUT 6 802059 . MS21042-3 NUT 15 8020510 . MS21042-4 NUT 4 8020511 . MS21042-5 NUT 6 8020512 . MS24693-S24 SCREW 4 8020513 . MS24694-S108 SCREW 3 8020514 . MS24694-S6 SCREW 2 8020515 . MS24694-S66 SCREW 2 8020516 . MS27039-0808 SCREW 4 8020517 . MS27039-1-10 SCREW 11 8020518 . MS27039-4-10 SCREW 1 8020519 . MS35206-229 SCREW 2 8020520 . NAS1149FN632P WASHER 4 8020521 . NAS1149FN832P WASHER 10 8020522 . NAS1149F0332P WASHER 28 8020523 . NAS1149F0432P WASHER 5 8020524 . NAS1149F0532P WASHER 10 8020525 . NAS43DD3-10N SPACER 1 8020526 . NAS43DD3-36N SPACER 1 8020527 . NAS517-5-26 SCREW 2 8020528 . NAS6605-12 BOLT 4 8020529 . S1438-13 WASHER 2 7EK5030 . S1438-43 WASHER 2 7EK5031 . S1551-1 ROLLER 1 7137932 . 3619464-14 CROSS TUBE 1 7137933 . 3619464-16 SWIVEL BASE PLATE 1 7137934 . 3619464-17 MAIN LEG - INBOARD 1 7137935 . 3619464-33 MAIN LEG - LOWER OUTBOARD 1 7137936 . 3619464-36 MAIN LEG - UPPER OUTBOARD 1 7137937 . 3619464-40 LINKAGE 1 7137938 . 3619464-41 LINKAGE 1 7137939 . 3619464-42 BRACE 1 7137940 . 3619464-43 LEVER ASSY 1 7137941 . . S4509-7 PLACARD - SWIVEL 1 7EK5042 . . 3619464-50 LEVER 1 7137943 . 3619464-53 GAS SPRING BRACKET 1 71379

ICA-700-25-00001

25-20-36-14 Sep 26/2019


CESSNA®


44 . 3619464-54 GAS SPRING LEVER 1 7137945 . 3619464-55 ROLLER BRACKET 1 7137946 . 3619464-58 SWIVEL PIN 1 7137947 . 3619464-61 LEVER BRACKET 1 7137948 . 3619464-7 AFT LEG ASSY 1 7137949 . . GFI-1011-06 BEARING 1 0JFH850 . . LC-036G-12S SPRING 1 8483051 . . MS21042-3 NUT 4 8020552 . . MS24694-S62 SCREW 4 8020553 . . MS51021-48 SETSCREW 2 8020554 . . MYI-08-06 CLIP BEARING 1 0JFH855 . . NAS1149F0332P WASHER 4 8020556 . . 3619464-28 AFT LEG 1 7137957 . . 3619464-29 LOCK PIN ASSY 1 7137958 . . . 3619464-31 PIN BODY 1 7137959 . . . 3619464-32 SHEAR PIN 2 7137960 . . 3619464-30 CLAMP BLOCK 1 7137961 . . 3619464-34 LOCK TUBE 1 7137962 . . 3619464-57 LOCK HANDLE ASSY 1 7137963 . . . S4509-8 PLACARD - LOCK HANDLE 1 7EK5064 . . . 3619464-39 HANDLE 1 7137965 . 6455K1 BEARING 2 3942866 . 98335A031 R - CLIP PIN 1 39428


ICA-700-25-00001

25-20-36-15 Sep 26/2019

CESSNA®


A

DETAIL AB

DETAIL B

1

1

3,6,11

1918

16

15,17

4,5

7

1213

148,9

21

10

ICA-700-25-00001

25-20-36-15 Sep 26/2019

CESSNA®


C

DETAIL C

20

2

2

ICA-700-25-00001

25-20-36-15 Sep 26/2019


CESSNA®


- 3619522-1 JUMPSEAT FLOOR PLUG COVER INSTL 1 . MS24693-S54 SCREW 2 802052 . MS24694-S57 SCREW 2 802053 . 3619523-1 JUMPSEAT FLOOR PLUG COVER ASSY 1 713794 . . 3619523-10 HINGE SPRING 1 713795 . . . 9287K74 TORSION SPRING 1 394286 . . 3619523-2 PLUG COVER LID ASSY 1 713797 . . . MS24693-3B SCREW 4 802058 . . . 3619523-4 KNOB ASSY 1 713799 . . . . 3619523-5 LID KNOB 1 7137910 . . . . 97395A451 DOWL PIN 1 3942811 . . . 3619523-6 COVER LID 1 7137912 . . . 3619523-7 INNER LID CAP 1 7137913 . . . 7488K13 THRUST BEARING 1 3942814 . . . 9002T15 COMPRESSION SPRING 2 3942815 . . 3619523-3 FLOOR PLUG BASE ASSY 1 7137916 . . . MS24693-C3 SCREW 1 8020517 . . . 3619523-8 FLOOR PLUG BEZEL 1 7137918 . . . 3619523-9 LATCH STRIKER 1 7137919 . . 98380A494 DOWL PIN 1 3942820 . 3619523-11 THRESHOLD 1 7137921 . 3619523-12 SPACER 1 71379


ICA-700-25-00001