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AIRCRAFT MANUAL SUPPLEMENT
To support Instructions for Continued Airworthiness in accordance with Regulations EASA CS-25.1529/FAR 14 CFR-25.1529, Appendix H.
365 Aerospace Modification MOD-0206 – ‘EGPWS standardization and computer upgrade to -218-218 Document No: AMS-0206-001
Intro Produced on behalf of 365 Aerospace Limited, UK. 365 Aerospace own the copyright of the format of this Manual Supplement, which is supplied in confidence. The contents must not be reproduced without permission In writing from the owner.
Produced on behalf of 365 Aerospace Limited, UK. 365 Aerospace own the copyright of the format of this Manual Supplement, which is supplied in confidence. The contents must not be reproduced without permission In writing from the owner.
HIGHLIGHTS Highlights of future amendments will be listed below
Produced on behalf of 365 Aerospace Limited, UK. 365 Aerospace own the copyright of the format of this Manual Supplement, which is supplied in confidence. The contents must not be reproduced without permission In writing from the owner.
RECORD OF REVISION
Issue Date Issue Date
Initial (1) Dec 05/2016
The Aircraft Manual Supplement (AMS) is to be used in conjunction with the related aircraft’s manuals. The information contained within this manual relates to various alterations/changes/modifications that have been carried out on the associated aircraft. A list of effective alterations/changes/modifications can be found in the Introduction pages to this manual. These alterations/changes/modifications are in addition to the initial design of the aircraft and are therefore detailed within this manual using appropriate and related convention. This manual complies with EASA Regulations CS-25.1529 and CS-25 Appendix H, which in turn mirror the FAA regulation 14 CFR 25.1529.
RRA-00
Page 1
Produced on behalf of 365 Aerospace Limited, UK. 365 Aerospace own the copyright of the format of this Manual Supplement, which is supplied in confidence. The contents must not be reproduced without permission In writing from the owner.
INTRODUCTION
1. General A. This publication was prepared on behalf of 365 Aerospace Ltd and is in accordance with Air Transport Association of America
Specification No. 100, Specification for Manufacturers Technical Data. The data contained within is related to certain changes/modifications/alterations that are in addition to the associated airplane’s type design.
NOTE: THIS MANUAL IS PREPARED SPECIFICALLY TO COVER THE AIRPLANE(S) LISTED IN THE "INTRODUCTION"
SECTION, FOR THE OWNER/OPERATOR NAMED ON THE TITLE PAGE.
THIS MANUAL IS NOT SUITABLE FOR USE, INCLUDING WITHOUT LIMITATION, GENERAL INSTRUCTIONS OR TRAINING, FOR ANY AIRPLANES NOT LISTED HEREIN.
B. The convention for the use of this publication is in the same convention (ATA 100) as the associated manufacturers AMM,
WDM, and IPC. Therefore, this publication is a SUPPLEMENT to the associated AMM, WDM, and IPC, and instructions on how to use this manual are equivalent to the instructions on how to use the manufacturers AMM, WDM and IPC.
C. This Manual Supplement has been raised to give historic design information pertaining to the following related aircraft
manuals:
WDM – Wiring Diagram Manual
IPC – Illustrated Parts Catalogue
AMM – Aircraft Maintenance Manual D. For information on the approval of the technical content of this document, please refer to the Change/Mod/Alteration listing E. Aircraft Effectivity Information:
MODEL/ TYPE
CUST EFFECT CODE
CUST EFFECT CODE
(IPC ONLY)
VARIABLE ENGR
NUMBER
ENGINE SET
NUMBER LINE
NUMBER
MFG SERIAL
NUMBER REGISTRY NUMBER
CUST ASSIGNED AIRPLANE
IDENT
737-4Z9 401 401 PW701 PB899 2043 25147 OE-IAB PW701
INTRO-00
Page 1 Dec 05/16
Produced on behalf of 365 Aerospace Limited, UK. 365 Aerospace own the copyright of the format of this Manual Supplement, which is supplied in confidence. The contents must not be reproduced without permission In writing from the owner.
INTRODUCTION
2. Change/Modification/Alteration Listing
A. DOA Mod/STC information – Table 2.1
Mod/STC Ref: Title:
MOD-0206 EGPWS standardization and computer upgrade to -218-218
B. Owner/Operator/Supplier Mod/STC Information – Table 2.2
Mod/STC Ref: Title: Supplier:
3. Approval
A. With reference to any Mod/STC indicated in Table 2.1 above, the technical content of the supplement information associated
with any listed Mod/STC above is approved under the authority of DOA No. EASA.21J.575. B. With reference to any Mod/STC indicated in Table 2.2 above, the technical content of the supplement information associated
with any listed Mod/STC above is approved under the authority of the named Owner/Operator/Supplier of the document. The Owner/Operator/Supplier of the document has given the compiler of this supplement rights to use their information in order to produce this manual supplement.
C. The Checking process will include a verification of technical consistency with the associated Mod/STC and Compliance
documentation which may relate to effectivity, description, effects on airworthiness and environmental protection especially when limitations are changed or affected.
Checked: Print Name: Olivier Poelmans
Approved: Print Name:
INTRO-00
Page 2 Dec 05/16
WIRING
DIAGRAM
MANUAL
Contents
WDM-CONTENTS
Page 1
Chapter 11 PLACARD & MARKINGS
Chapter 21 AIR CONDITIONING
Chapter 22 AUTO FLIGHT
Chapter 23 COMMUNICATIONS
Chapter 24 ELECTRICAL POWER
Chapter 25 EQUIPMENT/FURNISHINGS
Chapter 26 FIRE PROTECTION
Chapter 27 FLIGHT CONTROLS
Chapter 28 FUEL
Chapter 29 HYDRAULIC POWER
Chapter 30 ICE AND RAIN PROTECTION
Chapter 31 INDICATING/RECORDING SYSTEMS
Chapter 32 LANDING GEAR
Chapter 33 LIGHTS
Chapter 34 NAVIGATION
34-49-02 –Ground Proximity Warning Signal
Chapter 35 OXYGEN
Chapter 36 PNEUMATIC
Chapter 38 WATER/WASTE
Chapter 49 AIRBORNE AUXILIARY POWER
Chapter 52 DOORS
WDM-CONTENTS
Page 2
Chapter 53 FUSELAGE
Chapter 54 NACELLES / PYLONS
Chapter 55 STABILIZERS
Chapter 56 WINDOWS
Chapter 57 WINGS
Chapter 71 POWER PLANT
Chapter 73 ENGINE FUEL AND CONTROL
Chapter 74 IGNITION
Chapter 75 AIR
Chapter 77 ENGINE INDICATING
Chapter 78 EXHAUST
Chapter 79 OIL
Chapter 80 STARTING
Chapter 91 CHARTS
Chapter 93 PANELS
WDM-LEP
Page 1
LIST OF EFFECTIVE PAGES
Description Page No. Date Description Page No. Date
WDM Front Page WDM Contents 1 WDM Contents 2 WDM-List of Effective Pages 1 Chapter 34 Front Page 34-49-02 1 Dec 05/16
CHAPTER
34
NAVIGATION
B737-300/400/500 WIRING DIAGRAM MANUAL SUPPLEMENT
MSN25147/PW701
GROUND PROXIMITY WARNING SIGNAL
34-49-02 INCORPORATES:
34-49-02 365 AEROSPACE MOD 0206
Page 1 Page 1
DEC 05/16 DEC 05/16
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
ILLUSTRATED
PARTS
CATALOGUE
Contents
IPC-CONTENTS
Page 1
Chapter 11 PLACARD & MARKINGS
Chapter 21 AIR CONDITIONING
Chapter 22 AUTO FLIGHT
Chapter 23 COMMUNICATIONS
Chapter 24 ELECTRICAL POWER
Chapter 25 EQUIPMENT/FURNISHINGS
Chapter 26 FIRE PROTECTION
Chapter 27 FLIGHT CONTROLS
Chapter 28 FUEL
Chapter 29 HYDRAULIC POWER
Chapter 30 ICE AND RAIN PROTECTION
Chapter 31 INDICATING/RECORDING SYSTEMS
Chapter 32 LANDING GEAR
Chapter 33 LIGHTS
Chapter 34 NAVIGATION
34-42-11-99Z – EQUIPMENT INSTL ELECT. RACKS (Ground Proximity Computer only)
Chapter 35 OXYGEN
Chapter 36 PNEUMATIC
Chapter 38 WATER/WASTE
Chapter 49 AIRBORNE AUXILIARY POWER
Chapter 52 DOORS
Chapter 53 FUSELAGE
Chapter 54 NACELLES / PYLONS
Chapter 55 STABILIZERS
Chapter 56 WINDOWS
Chapter 57 WINGS
IPC-CONTENTS
Page 2
Chapter 71 POWER PLANT
Chapter 73 ENGINE FUEL AND CONTROL
Chapter 74 IGNITION
Chapter 75 AIR
Chapter 77 ENGINE INDICATING
Chapter 78 EXHAUST
Chapter 79 OIL
Chapter 80 STARTING
Chapter 91 CHARTS
Chapter 93 PANELS
IPC-LEP
Page 1
LIST OF EFFECTIVE PAGES
Description Page No. Date Description Page No. Date
IPC Front Page IPC Contents 1 IPC Contents 2 IPC-List of Effective Pages 1 Chapter 34 Front Page 34-42-11-99Z 0 Dec 05/16 34-42-11-99Z 0A Dec 05/16 34-42-11-99Z 1 Dec 05/16
CHAPTER
34
NAVIGATION
B737-300/400/500 ILLUSTRATED PARTS CATALOGUE SUPPLEMENT
34-42-11-99Z 34-42-11 MOD-0206
Fig 99Z DEC 05/16 Page 0
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
EQUIPMENT INSTL-ELECT. RACKS (GROUND PROXIMITY COMPUTER ONLY) FIGURE 99Z (SHEET 1)
B737-300/400/500 ILLUSTRATED PARTS CATALOGUE SUPPLEMENT
34-42-11-99Z 34-42-11 MOD-0206
Fig 99Z DEC 05/16 Page 0A
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
EQUIPMENT INSTL-ELECT. RACKS (GROUND PROXIMITY COMPUTER ONLY) FIGURE 99Z (SHEET 2)
B737-300/400/500 ILLUSTRATED PARTS CATALOGUE SUPPLEMENT
34-42-11-99Z 34-42-11 MOD-0206
Fig 99Z DEC 05/16 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
FIG ITEM
PART NUMBER NOMENCLATURE EFF
CODE
UNITS PER
ASSY 1234567
99Z --1 EO-0206-001 EGPWS STANDARDIZATION AND COMPUTER UPGRADE TO -218-218
PW701 RF
40 965-0976-060-218-218 • COMPUTER ASSY – ENHANCED GROUND PROXIMITY WARNING
ELECTRICAL EQUIP NUMBER: M00652 POST SERVICE BULLETIN 34-1789 AND 365 AEROSPACE MOD 0206
1
-- ITEMS NOT ILLUSTRATED
AIRCRAFT
MAINTENANCE
MANUAL
Contents
AMM-CONTENTS
Page 1
Chapter 11 PLACARD & MARKINGS
Chapter 21 AIR CONDITIONING
Chapter 22 AUTO FLIGHT
Chapter 23 COMMUNICATIONS
Chapter 24 ELECTRICAL POWER
Chapter 25 EQUIPMENT/FURNISHINGS
Chapter 26 FIRE PROTECTION
Chapter 27 FLIGHT CONTROLS
Chapter 28 FUEL
Chapter 29 HYDRAULIC POWER
Chapter 30 ICE AND RAIN PROTECTION
Chapter 31 INDICATING/RECORDING SYSTEMS
Chapter 32 LANDING GEAR
Chapter 33 LIGHTS
Chapter 34 NAVIGATION
34-42-03 – Ground Proximity Warning System
Chapter 35 OXYGEN
Chapter 36 PNEUMATIC
Chapter 38 WATER/WASTE
Chapter 49 AIRBORNE AUXILIARY POWER
Chapter 52 DOORS
Chapter 53 FUSELAGE
Chapter 54 NACELLES / PYLONS
Chapter 55 STABILIZERS
Chapter 56 WINDOWS
Chapter 57 WINGS
AMM-CONTENTS
Page 2
Chapter 71 POWER PLANT
Chapter 73 ENGINE FUEL AND CONTROL
Chapter 74 IGNITION
Chapter 75 AIR
Chapter 77 ENGINE INDICATING
Chapter 78 EXHAUST
Chapter 79 OIL
Chapter 80 STARTING
Chapter 91 CHARTS
Chapter 93 PANELS
AMM-LEP
Page 1
LIST OF EFFECTIVE PAGES
Description Page No. Date Description Page No. Date
AMM Front Page AMM Contents 1 AMM Contents 2 AMM-List of Effective Pages 1 Chapter 34 Front Page 34-42-03 501 DEC 05/16
CHAPTER
34
NAVIGATION
B737-300/400/500 AIRCRAFT MAINTENANCE MANUAL SUPPLEMENT
EFFECTIVITY
34-42-03 PW701 post SB 737-34-1789 and MOD-0206
Page 501
DEC 05/16
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
GROUND PROXIMITY WARNING SYSTEM – ADJUSTMENT TEST
1. General
A. The 365 Aerospace modification MOD-0206 changes the mode 6 callouts to menu 91, changes the mode 6 callouts to the default volume and activates the windshear caution option. It also updates the EGPWC to application software version 218 and configuration database 218 in accordance with Honeywell SB 965-0976/1690-34-76 in order to avoid nuisance EGPWS mode 2A alerts.
B. The operational test must be carried out in accordance with Boeing AMM 34-42-03.
Below tables provide the correct test results after incorporation of MOD-0206. 2. GPWS – Operational Test
E. Procedure
Table 502/34-42-03-993-816
AURAL WARN LIGHTS Minimums Off
1000 Off 500 Off 100 Off 50 Off 40 Off 30 Off 20 Off 10 Off
G. Program pin test
SUBTASK 34-42-03-745-243
(3) (a) 1) PART NUMBER 965-0976-060-218-218 2) MOD STATUS XXXX 3) SERIAL NUMBER XXXXXX 4) APPLICATION SOFTWARE VERSION 218.X 5) CONFIGURATION SOFTWARE VERSION 218.X 6) TERRAIN DATABASE VERSION XXX 7) ENVELOPE MODULATION DATABASE VERSION BXX 8) BOOT CODE VERSION BXXX.X 9) AIRCRAFT TYPE ONE NINE THREE 10) AUDIO MENU ZERO 11) ALTITUDE CALLOUT MENU NINE ONE 12) PEAKS ENABLED 13) OPTIONAL INPUTS SELECTED 14) SINGLE GPS SELECTED 15) DUAL ILS SELECTED 16) DUAL RADIO ALTIMETER SELECTED 17) BANK ANGLE SELECTED 18) OBSTACLE AWARENESS ENABLED