minimum equipment list: dassault falcon 2000 lx nav doc.pdf · 2021. 1. 6. · minimum equipment...

MINIMUM EQUIPMENT LIST: Dassault Falcon 2000 LX

Amendment #: Original 15 August 2020 i 2020 This document is confidential and proprietary to The Company Aviation Department and cannot be used, disclosed, or duplicated without the prior written consent of the

company.

Main eMenu ****Working Links are in RED

Fault Guide for Dispatch Assistance (FGDA) 21 - Air Conditioning

22 - Auto Flight

23 - Communications

24 - Electrical & Power

25 - Equipment & Furnishings

26 - Fire Protection

27 - Flight Controls

28 - Fuel

29 - Hydraulics

30 - Ice & Rain Protection

31 - Indicating / Recording Systems

32 - Landing Gear

33 - Lights

34 - Navigation

35 - Oxygen

36 - Pneumatic

45 - Central Maintenance System

46 - Information System

49 - Airborne Auxillary Power

52 - Doors

73 - Engine Fuel and Control

74 - Ignition

77 - Engine Indicating

78 - Thrust Reverser

79 - Oil


Amendment #: Original 15 August 2020 i 2020 This document is confidential and proprietary to The Company Aviation Department and cannot be used, disclosed, or duplicated without the prior written consent of the

company.

Minimum Equipment List

Dassault Falcon 2000LX

Copy #: 1 Issued to: Aviation Manager


Amendment #: Original 15 August 2020 ii 2020 This document is confidential and proprietary to The Company Aviation Department and cannot be used, disclosed, or duplicated without the prior written consent of the

company.

COMPANY CERTIFICATION

This MEL has been developed in accordance with the following documents: - JAA Master Minimum Equipment List - Revision 9 dated 11/03/2013 was typed in and formatted in the Transport Canada format as per Transport Canada document “TP9155”. - Any reference to regulations were changed to CAR references and the appropriate CAR reference added. - Maintenance & Operating procedures were added from Dassault Aviation supplied procedures. Reference Document – Falcon 2000EX-EASy Maintenance and Operating Procedures (Revision 9 dated 11/03/2013). - The MEL was developed to the standards as shown in the Transport Canada document “MMEL Guidance Book, Revision 7, issued 27 April 2009” and “Minimum Equipment List Policy and Procedures Manual, Second Edition, issued January 2006”. A Standard Preamble and definitions section was added. This document is used for Falcon 2000LX aircraft operated under CAR 604 and CAR 704 by The Company Approved by: ______________________ ______________ 15 August 2020 Director of Maintenance Name Date ______________________ ____________ 15 August 2020 Operations Manager Name Date


Amendment #: Original 15 August 2020 iii 2020 This document is confidential and proprietary to The Company Aviation Department and cannot be used, disclosed, or duplicated without the prior written consent of the

company.

PREAMBLE

All equipment installed on an aircraft in compliance with the Airworthiness Standards and the Operating Rules must be operative. However, CAR 605.07, permits the publication of a Master Minimum Equipment List (MMEL) where compliance with certain equipment requirements is not necessary under all operating conditions. Experience has shown that with the various levels of redundancy designed into aircraft, operation of every system or installed component may not be necessary when the remaining operative equipment can provide the required level of safety.

A Master Minimum Equipment List (MMEL) is developed by Transport Canada, with participation by the aviation industry, to improve aircraft utilization and thereby provide more


Amendment #: Original 15 August 2020 iv 2020 This document is confidential and proprietary to The Company Aviation Department and cannot be used, disclosed, or duplicated without the prior written consent of the

company.

TABLE OF CONTENTS

Title Page ........................................................................................................................................ i Company Certification .................................................................................................................... ii Preamble ...................................................................................................................................... iii Table of Contents .......................................................................................................................... iv MEL Handling Procedures .............................................................................................................. v Minimum Equipment List Notes & Definitions ................................................................................ vi Use of FGDA ................................................................................................................................ vii Acnomyms & Abbreviations ........................................................................................................... ix List of Effective Pages .................................................................................................................... x Amendment Record ...................................................................................................................... xii Amending Procedures and Distribution List ................................................................................. xiii Systems by ATA Chapter 21 Air Conditioning .........................................................................................21-01 to 21-25 22 Auto Flight .................................................................................................22-01 to 22-13 23 Communications ........................................................................................23-01 to 23-14 24 Electrical Power .........................................................................................24-01 to 24-02 25 Equipment Furnishings ..............................................................................25-01 to 25-15 26 Fire Protection ........................................................................................................ 26-01 27 Flight Controls ...........................................................................................27-01 to 27-12 28 Fuel ...........................................................................................................28-01 to 28-20 29 Hydraulic Power ........................................................................................29-01 to 29-07 30 Ice and Rain Protection .............................................................................30-01 to 30-15 31 Indicating/Recording Systems ...................................................................31-02 to 31-06 32 Landing Gear ............................................................................................32-01 to 32-07 33 Lights ........................................................................................................33-01 to 33-24 34 Navigation .................................................................................................34-01 to 34-27 35 Oxygen ......................................................................................................35-01 to 35-04 36 Pneumatic .................................................................................................36-01 to 36-12 45 Central Maintenance System .....................................................................45-01 to 45-02 46 Information System ................................................................................................ 46-01 49 Airborne Auxiliary Power ...........................................................................49-01 to 49-05 52 Doors ........................................................................................................52-01 to 52-02 73 Engine Fuel and Control ............................................................................73-01 to 73-02 74 Ignition ................................................................................................................... 74-01 77 Engine Indicating .................................................................................................... 77-01 78 Thrust Reverser .........................................................................................78-01 to 78-03 79 Oil..............................................................................................................79-01 to 79-06

Appendix “A” Maintenance and Operational Procedures Manual


Amendment #: Original 15 August 2020 v 2020 This document is confidential and proprietary to The Company Aviation Department and cannot be used, disclosed, or duplicated without the prior written consent of the

company.

MEL HANDLING PROCEDURES

1.0 MEL DEFECT DEFERRAL PROCEDURES Note: Use of this MEL may not guarantee compliance with Regulations outside of Canada nor other procedures such as; Company Operation Specifications, ETOPs, RVSM, CAT II/III, etc.


Amendment #: Original 15 August 2020 vi 2020 This document is confidential and proprietary to The Company Aviation Department and cannot be used, disclosed, or duplicated without the prior written consent of the

company.

NOTES AND DEFINITIONS

1. Systems Definitions: Systems numbers are based on the Air Transport Association (ATA) Specification Number 100 and items are numbered sequentially.

“Item” (Column 1) means the equipment, system, component, or function listed in the “Item” column.

“Number Installed” (Column 2) is the number (quantity) of items normally installed in the aircraft. This number represents the aircraft configuration considered in developing this MMEL. Should the number be a variable (e.g., passenger cabin items) a number is not required.

“” symbol in Column 1 indicates an item which is not required by regulation but which may have been installed on some models of aircraft covered by this MMEL. This item may be included on the operator's MEL after the approving office has determined that the item has been installed on one or more of the operator's aircraft. The symbol, however, shall not be carried forward into the operator's MEL. It should be noted that neither this policy nor the use of this symbol provide authority to install or remove an item from an aircraft. The “” symbol may be considered equivalent to the term “if installed”.


Amendment #: Original 15 August 2020 vii 2020 This document is confidential and proprietary to The Company Aviation Department and cannot be used, disclosed, or duplicated without the prior written consent of the

company.

USE OF FAULT GUIDE FOR DISPATCH ASSISTANCE (FGDA)

The FGDA has been designed by Dassault Aviation to provide Falcon 2000 LX operators with assistance when dispatch decision is to be considered in operation.

Introduction

With regard to regulation the input(s) of this MEL must be a piece of equipment, a system or a function.

In all cases it remains operator's responsibility to determine the faulty piece of equipment, system or function.

In addition to the MEL and associated M&O procedures referenced hereafter, the FGDA provides dispatch assistance when a failure effect occurs in the flight deck of the aircraft (mainly computers fault codes); dispatch decision is always given by MEL.

When the FGDA addresses an item of the MEL, the operator has to consider the dispatch cases of this item itself, and not the dispatch cases related to its sub-item(s) if any.

When the FGDA addresses a sub-item of the MMEL, the operator may consider the dispatch cases of this sub-item itself, or the dispatch cases related to its item, if any.

Although any page of thie FGDA document undergoes a careful and strict correction process to ensure that the data contained within the document and those contained in the airplane certified documents (AFM and MMEL) are in coherence, the Airplane Flight Manual and this Transp[ort Canada approved MEL are the final authority in case of differences.

If a Fault code is triggered but is not referenced in this document, it is NO GO unless a dedicated troubleshooting is performed to determine the faulty piece of equipment, system or function which is in the MEL. If needed, contact Dassault Aviation Technical Support.


Amendment #: Original 15 August 2020 viii 2020 This document is confidential and proprietary to The Company Aviation Department and cannot be used, disclosed, or duplicated without the prior written consent of the

company.

USE OF FGDA FOR DISPATCH DECISION

The following figure provides a synthetic description of the different steps to be followed by the flight crew and/or the maintenance engineer when a dispatch decision is to be made when the aircraft is on ground:


Amendment #: Original 15 August 2020 ix 2020 This document is confidential and proprietary to The Company Aviation Department and cannot be used, disclosed, or duplicated without the prior written consent of the

company.

ACRONYMS & ABBREVIATIONS

# Hydraulic circuit number A/C Aircraft A/I Anti Ice A/T Auto Throttle AAL Above Airport Level AB Airbrakes ACCU Accumulator ACP Audio Control Panel ADC Air Data Computer ADF Automatic Direction Finder ADI Attitude Director Indicator ADM Air Data Module ADS Air Data System AFCS Automatic Flight Control System AFM Airplane Flight Manual AFU Artificial Feel Unit AGL Above Ground Level AGM Advanced Graphics Module AHC Attitude Heading Computer AHRS Attitude Heading Reference System AHS Attitude Heading System AIL Aileron ALT Altitude ALTN Alternate ANTICOL Anticollision AOA Angle Of Attack AP Auto Pilot APP Approach APPR Approach APR Automatic Power Reserve APS Altitude Preselection APU Auxiliary Power Unit ARP Air data Reference Panel ASEL Altitude Select AT Auto Throttle ATA Actual Time of Arrival ATC Air traffic Control ATT Attitude AUTO Automatic AUX Auxiliary Avoidance System TRM Trim B/C Back Course B−RNAV Basic RNAV BAG Baggage BAT Battery BKUP Backup BOOST Booster

BRG Bearing BRK Brake BRT Brightness BSCU Braking System Control Unit C/B Circuit Breaker CAB Cabin Computer CAS Calibrated Airspeed CAS Crew Alerting System CAT Category CCD Cursor Control Device CCW Counter Clock Wise CDI Course Deviation Indicator CDL Configuration Deviation List CDU Control and Display Unit Control System CG Center of Gravity CHK Check CKPT Cockpit CLB Climb CLC Check−List Controller CMC Centralized Maintenance CMPTR Computer COM Communication COMPT Computer COND Conditioning COND’G Conditioning COPIL Copilot CPCS Centralized Pressurization CPL Couple CRS Course CTL Circle To Land CVR Cockpit Voice Recorder CW Clock Wise DAU Data Acquisition Unit DC Direct Current DCP Display Control Panel DEEC Digital Electronic Engine Control DEST Destination DFDR Digital Flight Data Recorder DGAC Direction Générale de l’Aviation Civile DGR Degraded DGRAD Degraded DGT Direction Générale Technique


Amendment #: Original 15 August 2020 x 2020 This document is confidential and proprietary to The Company Aviation Department and cannot be used, disclosed, or duplicated without the prior written consent of the company.

LIST OF EFFECTIVE PAGES

Item Page Description Revision Date i Title Page Original Aug 15, 2020

ii Company Certification Original Aug 15, 2020 iii Preamble Original Aug 15, 2020 iv Preamble Original Aug 15, 2020 v Table of Contents Original Aug 15, 2020 vi MEL Handling Procedures Original Aug 15, 2020 vii MEL Handling Procedures Original Aug 15, 2020 viii MEL Handling Procedures Original Aug 15, 2020 ix Notes & Definitions Original Aug 15, 2020 x Notes & Definitions Original Aug 15, 2020 xi Notes & Definitions Original Aug 15, 2020 xii Notes & Definitions Original Aug 15, 2020 xiii Notes & Definitions Original Aug 15, 2020 xiv Notes & Definitions Original Aug 15, 2020 xv Use of FGDA Original Aug 15, 2020 xvi Use of FGDA for Dispatch Decision Original Aug 15, 2020 xvii Acronyms & Abbreviations Original Aug 15, 2020 xviii Acronyms & Abbreviations Original Aug 15, 2020 xix Acronyms & Abbreviations Original Aug 15, 2020 xx Acronyms & Abbreviations Original Aug 15, 2020 xxi List of Effective Pages Original Aug 15, 2020 xxii List of Effective Pages Original Aug 15, 2020 xxiii List of Effective Pages Original Aug 15, 2020 xxiv List of Effective Pages Original Aug 15, 2020 xv List of Effective Pages Original Aug 15, 2020 xvi List of Effective Pages Original Aug 15, 2020 xxvii List of Effective Pages Original Aug 15, 2020 xxviii List of Effective Pages Original Aug 15, 2020 xxix List of Effective Pages Original Aug 15, 2020 xxx List of Effective Pages Original Aug 15, 2020 xxxi Amendment Record Original Aug 15, 2020 xxxii Amending Procedures and Dist. List Original Aug 15, 2020


Amendment #: Original 15 August 2020 xi 2020 This document is confidential and proprietary to The Company Aviation Department and cannot be used, disclosed, or duplicated without the prior written consent of the company.

.

****Working Links are in RED

21 AIR CONDITIONING

21-1 21-01-1 Cabin Pressure Controller (CPC) Original Aug 15, 2020

21-2 21-02-1 UP-DN Manual Regulator (on instrument panel)

Original Aug 15, 2020

21-3 21-03-1 Pressurization Indications (on ECS synoptic page)


21-4 21-04-1 LOW Soft-key (on ECS synoptic

page)


21-5 21-05-1 Outflow Pressurization Valves Original Aug 15, 2020

21-6 21-06-1 Environmental Control Unit (ECU) Original Aug 15, 2020

21-7 21-07-1 Cold Conditioning Valves Original Aug 15, 2020

21-8 21-08-1 Hot Conditioning Valves Original Aug 15, 2020

21-9 21-09-1 Cabin Air Recirculation Valve Original Aug 15, 2020

21-10 21-10-1 Jet Pump Valve Original Aug 15, 2020

21-11 21-11-1 Temperature Regulation Controller (TCS): AUTO mode


21-11 21-11-2 Temperature Regulation Controller (TCS): AUTO mode


21-13 21-13-1 Temperature Regulation Controller (TCS): MANUAL mode


21-15 21-15-1 Remote Soft-key Control of

Temperature (on ECS synoptic page)


21-16 21-16-1 CABIN Temperature Indication (on ECS synoptic page)


21-17 21-17-1 Cabin Duct Temperature Indication (on ECS synoptic page)


21-18 21-18-1 Cold Fan Pressure Control Valve Original Aug 15, 2020

21-19 21-19-1 Pilot / Copilot Gaspers Original Aug 15, 2020

21-20 21-20-1 Air Conditioning Distribution Levers Original Aug 15, 2020

21-21 21-21-1 Glare Shield Cold Air Manual Control Original Aug 15, 2020

21-22 21-22-1 ECS By-pass Valve Original Aug 15, 2020

21-24 21-24-1 Nose Cone Blower Fan Original Aug 15, 2020

21-25 21-25-1 Temperature Regulation System Original Aug 15, 2020

22 AUTOFLIGHT

22-1 22-01-1 Autopilot Functions (AP1 and AP2)


22-2 22-02-1 Yaw Damper Functions (YD1 and YD2) Original Aug 15, 2020

22-3 22-03-1 Autothrottle Function (AT) Original Aug 15, 2020

22-4 22-04-1 Mach Trim Functions (MT) Original Aug 15, 2020


Amendment #: Original 15 August 2020 xii 2020 This document is confidential and proprietary to The Company Aviation Department and cannot be used, disclosed, or duplicated without the prior written consent of the company.

AMENDMENT RECORD

Amend # Amend Date Date Entered Entered By

1

2

3

4

5

6

7

8

9

10

11

12

13

14

15

16

17

18

19


Amendment #: Original 15 August 2020 xiii 2020 This document is confidential and proprietary to The Company Aviation Department and cannot be used, disclosed, or duplicated without the prior written consent of the company.

AMENDING PROCEDURES AND DISTRIBUTION LIST

Amending Procedures

Manual amendments will be promulgated as required by the Operations Manager. After approval by the Department of Transport, they will be issued to manual holders. Each amended page shall show the appropriate amendment number and date. All changes will be indicated by a vertical black bar adjacent to the item that has been changed. When a manual is amended, a copy of the amendment is to be forwarded to the Transport Canada along with the appropriate amendment instructions. Amendment instructions shall include a "Remove Pages" and "Insert Pages" and "Reason for Change" list. The amended text shall be identified by a vertical line in the right-hand margin. When a manual or amendments thereto are superseded, instructions should be issued to all manual holders to destroy the superseded copies.

Minimum Equipment List Distribution and Control

The Operations Manager will maintain a master list of manual holders and control their distribution. The following operational personnel will hold copies of this Minimum Equipment List and will be responsible for its amendment: Transport Canada, Operations Manager, Chief Pilot and Maintenance Manager. A manual will also be assigned to each aircraft and will be amended by the Operations Manager or his representative.

Manuals may be issued as eManuals or hardcopy manuals.

Copy # Issued To:

1 Operations Manager – Master Copy

2 Transport Canada

3 Pilots Library

4 Maintenance Library

5 Aircraft C-F

MINIMUM EQUIPMENT LIST Falcon 2000LX Revision #: Original

Date: 15/08/2020 Page No: 21-01-1

ATA. SYSTEM & SEQUENCE NUMBERS

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

2020 This document is confidential and proprietary to The Company Aviation Department and cannot be used, disclosed, or duplicated without the prior written consent of the company.

21 AIR CONDITIONING

21-1 Cabin Pressure Controller (CPC)

B 1 0 (M#) May be inoperative provided:

- UP-DN manual regulator and DUMP mode are verified operative before each departure,

- CABIN ALTITUDE red CAS message and "Cabin..." voice warning are operative,

- UP-DN manual regulator is set to the middle of white range,

- MAN is correctly displayed on ECS synoptic page,

- Cabin altitude, Cabin rate of change and Cabin differential pressure Δp indications are operative,

- Pressurization indications on ECS synoptic page are regulary monitored,

- Destination airfield landing elevation and current airfield altitude are below 8,000 ft.

C 1 0 (O) May be inoperative provided the flight is

conducted in an unpressurized configuration.

PLACARDING:

1. Placard as specified in the Maintenance Control System. 2. Where an (M) or (O) procedure is specified, and not shown below, refer to Appendix A – “Falcon 2000EX-EASy

Maintenance and Operating Procedures Manual” for specific placarding information. 3. Where practical affix placard on or adjacent to the affected indicator and/or control, if not then to a location on the

flight deck clearly visible to both flight crew-members.

OPERATIONAL PROCEDURES:

Refer to Appendix A - “Falcon 2000EX-EASy Maintenance and Operating Procedures Manual” 1. Perform the procedure referenced at OPER 21-0 on section 2-21

MAINTENANCE PROCEDURES:

Refer to Appendix A - “Falcon 2000EX-EASy Maintenance and Operating Procedures Manual” 1. Perform the procedure referenced at MAINT 21-1.1 on section 3-21 2. Perform the procedure referenced at MAINT 21-1.2 on section 3-21


Date: 15/08/2020 Page No: 21-02-1


1. REPAIR CATEGORY

2. NUMBER INSTALLED




21 AIR CONDITIONING

21-2 UP-DN Manual Regulator (on instrument panel)

C 1 0 (O) May be inoperative provided the flight is conducted in an unpressurized configuration.

PLACARDING:





Refer to Appendix A - “Falcon 2000EX-EASy Maintenance and Operating Procedures Manual” 1. Perform OPER 21-0 on section 2-21


None required.


Date: 15/08/2020 Page No: 21-03-1


1. REPAIR CATEGORY

2. NUMBER INSTALLED




21 AIR CONDITIONING

21-3 Pressurization Indications (on ECS synoptic page)

1) ALTITUDE Indication C 1 0 (O) May be inoperative provided the flight is conducted in an unpressurized configuration.

2) Δ PCAB Indication C 1 0 (O) May be inoperative provided ALTITUDE

indication is operative.


3) RATE Indication C 1 0 May be inoperative provided ALTITUDE indication is

operative.


PLACARDING:





CASE 1 / 3 /5: Refer to Appendix A - “Falcon 2000EX-EASy Maintenance and Operating Procedures Manual” 1. Perform the procedure referenced at OPER 21-0 on section 2-21 CASE 2: Refer to Appendix A - “Falcon 2000EX-EASy Maintenance and Operating Procedures Manual” 1. Perform the procedure referenced at OPER 21-3.2 on section 2-21


None required.


Date: 15/08/2020 Page No: 21-04-1


1. REPAIR CATEGORY

2. NUMBER INSTALLED




21 AIR CONDITIONING

21-4 LOW Soft-key

(on ECS synoptic page)

C 1 0 May be inoperative.

PLACARDING:





None required.


None required.

MINIMUM EQUIPMENT LIST Falcon 2000 LX Revision #: Original

Date: 15/08/2020 Page No: 21-05-1


1. REPAIR CATEGORY

2. NUMBER INSTALLED




21 AIR CONDITIONING

21-5 Outflow Pressurization Valve

C 2 0 (O) One or more may be inoperative provided the flight is conducted in an unpressurized configuration.

PLACARDING:







None required.


Date: 15/08/2020 Page No: 21-06-1


1. REPAIR CATEGORY

2. NUMBER INSTALLED




21 AIR CONDITIONING

21-6 Environmental Control Unit (ECU)


PLACARDING:





Refer to Appendix A - “Falcon 2000EX-EASy Maintenance and Operating Procedures Manual” 1. Perform OPER 36-0 on section 2-36


None required.


Date: 15/08/2020 Page No: 21-07-1


1. REPAIR CATEGORY

2. NUMBER INSTALLED




21 AIR CONDITIONING

21-7 Cold Conditioning Valves C 2 1 (M#) One cold valve may be inoperative provided:

- Affected cold conditioning valve is secured in closed position,

- Flight level is limited to 41,000 ft or below.

C 2 0 (O)(M#) Both may be inoperative provided:

- Cold conditioning valves are secured in closed position,

- Flight is conducted in an unpressurized configuration.

PLACARDING:





Refer to Appendix A - “Falcon 2000EX-EASy Maintenance and Operating Procedures Manual” 1. Perform the procedure referenced at OPER 36-0 on section 2-36.


CASE 1 / 2: Refer to Appendix A - “Falcon 2000EX-EASy Maintenance and Operating Procedures Manual” 1. Perform the procedure referenced at MAINT 21-7 on section 3-21 2. If Valve must be positioned to the closed position this procedure becomes an (M#) procedure and maintenance

personnel are required to to position the valve before dispatch of the aircraft is possible.


Date: 15/08/2020 Page No: 21-08-1


1. REPAIR CATEGORY

2. NUMBER INSTALLED




21 AIR CONDITIONING

21-8 Hot Conditioning Valves C 2 1 (M#) One hot valve may be inoperative provided:

- Affected hot conditioning valve is secured in closed position,

- Manual air conditioning intercommunication valve is set to OPEN position,

- Flight level is limited to 41,000 ft or below.

C 2 0 (O)(M#) Both may be inoperative provided:

- Hot conditioning valves are secured in closed position,

- Flight is conducted in an unpressurized configuration.

PLACARDING:







CASE 1 / 2: Refer to Appendix A - “Falcon 2000EX-EASy Maintenance and Operating Procedures Manual” 1. Perform the procedure referenced at MAINT 21-7 on section 3-21 2. If Valve must be positioned to the closed position this procedure becomes an (M#) procedure and maintenance

personnel are required to to position the valve before dispatch of the aircraft is possible.


Date: 15/08/2020 Page No: 21-09-1


1. REPAIR CATEGORY

2. NUMBER INSTALLED




21 AIR CONDITIONING

21-9 Cabin Air Recirculation Valve

C 1 0 (O) May be inoperative provided it is secured in closed position.

PLACARDING:







None required.


Date: 15/08/2020 Page No: 21-10-1


1. REPAIR CATEGORY

2. NUMBER INSTALLED




21 AIR CONDITIONING

21-10 Jet Pump Valve C 1 0 (O)(M) May be inoperative provided:

- Jet pump valve is verified in closed position,

- Air conditioning remains OFF on ground and in flight when TAS is below 300 Kt,

- Air conditioning is switched ON in flight only when TAS is above 300 Kt.

PLACARDING:







Refer to Appendix A - “Falcon 2000EX-EASy Maintenance and Operating Procedures Manual” 1. Perform the procedure referenced at MAINT 21-10 on section 3-21


Date: 15/08/2020 Page No: 21-11-1


1. REPAIR CATEGORY

2. NUMBER INSTALLED




21 AIR CONDITIONING

21-11 Temperature Regulation Controller (TCS): AUTO mode

A 2 0 (M) One or more may be inoperative provided:

- MANUAL mode is verified operative,

- Repairs are made within three consecutive calendar days.

1) Engine Throttle Position Functions

A 2 1 One may be inoperative provided:

- TCS fault codes have been considered,

- Engine throttles are operative,


2) Computer Dialog Functions (Cockpit and Cabin)




PLACARDING:





None required.


Refer to Appendix A - “Falcon 2000EX-EASy Maintenance and Operating Procedures Manual” 1. Perform the procedure referenced at MAINT 21-11 on section 3-21


Date: 15/08/2020 Page No: 21-11-2


1. REPAIR CATEGORY

2. NUMBER INSTALLED




21 AIR CONDITIONING

21-11 Temperature Regulation Controller (TCS): AUTO mode (cont`d)

3) Compressor Overheat Sensor Functions (Cockpit and Cabin)




4) CREW and PAX Auto Temperature Potentiometer Functions

A 2 0 One or more may be inoperative provided:



5) Cockpit and Cabin Duct Temperature Sensor Functions




PLACARDING:





None required.


None required.


Date: 15/08/2020 Page No: 21-13-1


1. REPAIR CATEGORY

2. NUMBER INSTALLED




21 AIR CONDITIONING

21-13 Temperature Regulation Controller (TCS): MANUAL mode


1) CREW and PAX Manual Temperature Potentiometer Functions




PLACARDING:







None required.


Date: 15/08/2020 Page No: 21-15-1


1. REPAIR CATEGORY

2. NUMBER INSTALLED




21 AIR CONDITIONING

21-15 REMOTE Soft-key

Control of Temperature (on ECS synoptic page)

C 1 O May be inoperative.

PLACARDING:





None required.


None required.


Date: 15/08/2020 Page No: 21-16-1


1. REPAIR CATEGORY

2. NUMBER INSTALLED




21 AIR CONDITIONING

21-16 CABIN

Temperature Indication (on ECS synoptic page)


PLACARDING:





None required.


None required.


Date: 15/08/2020 Page No: 21-17-1


1. REPAIR CATEGORY

2. NUMBER INSTALLED




21 AIR CONDITIONING

21-17 Cabin Duct Temperature Indication (on ECS synoptic page)


PLACARDING:





None required.


None required.


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