aircraft manual supplementb737-42chgw pw051 24231 b737-448hgw pw595 25052 b737-4q8 pw233 25097...

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 MDL-0377 Document No: AMS-0377-001

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.

HL-00 Page 1 MAR 01/18

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

RR-00 Page 1 MAR 01/18


RECORD OF REVISION

Issue Date Issue Date Initial (1) MAR 01/18

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.

INTRO-00 Page 1 MAR 01/18


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 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

B737-42CHGW PW051 24231 B737-448HGW PW595 25052

B737-4Q8 PW233 25097 B737-4Y0HGW PW046 25177 B737-429HGW PW761 25729

B737-4Z9 PW702 27094 B373-43Q PW272 28490

PW276 28494 B737-490 PJ601 28885

PJ602 28886 PJ608 28892 PJ610 28893

B737-4M0 PW441 29201 PW442 29202 PW443 29203

B737-490 PJ609 29270

INTRO-00 Page 2 MAR 01/18


INTRODUCTION

2. Change/Modification/Alteration Listing

A. DOA Mod/STC information – Table 2.1

Mod/STC Ref: Title:

MDL-0337 Installation of DeVore Wing Position Lights

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:

Approved: Print Name:

Mitchellh

Typewritten Text

Mitchell Hills

Mitchellh

Typewritten Text

Daniel Jackson

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

33-43-01 – POSITION LIGHTS

Chapter 34 NAVIGATION

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 33 Front Page 33-43-01 1 MAR 01/18 33-43-01 2 MAR 01/18

CHAPTER

33 LIGHTS

B737-300/400/500 WIRING DIAGRAM MANUAL

PJ601, PJ602, PJ608, PJ609, PJ610, PW233, PW272, PW276, PW441, PW442, PW443, PW595, PW702, PW761

POSITION LIGHTS 33-43-01 INCORPORATES: 33-43-01 365 AEROSPACE MOD 0377

Page 1 Page 1

MAR 01/18 MAR 01/18 Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.

B737-300/400/500 WIRING DIAGRAM MANUAL

PW046, PW051

POSITION LIGHTS 33-43-01 INCORPORATES: 33-43-01 365 AEROSPACE MOD 0377

Page 2 Page 2

MAR 01/18 MAR 01/18 Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.

ILLUSTRATED

PARTS

CATALOGUE

Contents

IPC-CONTENTS Page 1






24-50-13-99Z – PANEL ASSY – P18-3 CB (ELECTRICAL POWER ONLY)




Chapter 28 FUEL





Chapter 33 LIGHTS

33-43-11-99Z – LIGHT INSTL – WING TIP (STEADY POSITION NAVIGATION LIGHTS ONLY)


Chapter 35 OXYGEN




Chapter 52 DOORS

Chapter 53 FUSELAGE



Chapter 56 WINDOWS

IPC-CONTENTS Page 2

Chapter 57 WINGS



Chapter 74 IGNITION

Chapter 75 AIR


Chapter 78 EXHAUST

Chapter 79 OIL

Chapter 80 STARTING

Chapter 91 CHARTS

Chapter 93 PANELS

IPC-LEP Page 1



IPC Front Page IPC Contents 1 IPC Contents 2 IPC-List of Effective Pages 1 Chapter 24 Front Page 24-50-13-99Z 0 MAR 01/18 24-50-13-99Z 1 MAR 01/18 Chapter 33 Front Page 33-43-11-99Z 0 MAR 01/18 33-43-11-99Z 1 MAR 01/18

CHAPTER

24 ELECTRICAL

POWER

B737-300/400/500 ILLUSTRATED PARTS CATALOGUE

24-50-13-99Z 24-50-13 MDL-0377 Fig 99Z MAR 01/17 Page 0

Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.

PANEL ASSY – P18-3 CB (ELECTRICAL POWER ONLY) FIGURE 99Z




FIG ITEM PART NUMBER NOMENCLATURE EFF

CODE UNITS PER

ASSY 1234567

99Z --1 EO-0377-001 INSTALLATION OF DEVORE WING POSITION LIGHTS RF --1 73733016 WING FWD POSITION LIGHT INSTL (DEVORE DRAWING) RF

10 MS3320-15 • CIRCUIT BREAKER (15 AMP) 2 ALTERNATE PART: 4310-002-15 (V76374)

-- ITEMS NOT ILLUSTRATED

CHAPTER

33 LIGHTS




LIGHT INSTL – WING TIP (STEADY POSITION NAVIGATION LIGHTS ONLY) FIGURE 99Z




FIG ITEM PART NUMBER NOMENCLATURE EFF

CODE UNITS PER

ASSY 1234567

99Z --1 EO-0377-001 INSTALLATION OF DEVORE WING POSITION LIGHTS RF --1 73733016 WING FWD POSITION LIGHT INSTL (DEVORE DRAWING) RF

10 73733014-1 • POSITION LIGHT 2 20 73733017-1 • BRACKET – RESISTOR (LH WINGTIP) 1 20 73733017-2 • BRACKET – RESISTOR (RH WINGTIP) 1 30 00003091 • REFLECTOR 2 40 CM1982SP • LAMP 2

--50 25-0325-21 • LENS – RED – L/H (EXISTING PART) 1 --60 25-0325-22L • LENS – GREEN – R/H (EXISTING PART) 1 --70 31-0881-1 • LENS RETAINER (EXISTING PART) 2 --80 73733013-13 • LENS RETAINER GASKET 2 --90 73733013-11 • GASKET 2 --100 MS27039-0809 • SCREW 8 --110 NAS1149DN832K • WASHER 10 --120 MS21042L08 • NUT 2

-- ITEMS NOT ILLUSTRATED

AIRCRAFT

MAINTENANCE

MANUAL

Contents

AMM-CONTENTS Page 1









Chapter 28 FUEL





Chapter 33 LIGHTS

33-43-11 – STEADY POSITION (NAVIGATION) LIGHTS

PAGE BLOCK 201 – MAINTENANCE PRACTICES

PAGE BLOCK 401 – REMOVAL AND INSTALLATION


Chapter 35 OXYGEN




AMM-CONTENTS Page 2

Chapter 52 DOORS

Chapter 53 FUSELAGE



Chapter 56 WINDOWS

Chapter 57 WINGS



Chapter 74 IGNITION

Chapter 75 AIR


Chapter 78 EXHAUST

Chapter 79 OIL

Chapter 80 STARTING

Chapter 91 CHARTS

Chapter 93 PANELS

AMM-LEP Page 1



AMM Front Page AMM Contents 1 AMM Contents 2 AMM-List of Effective Pages 1 Chapter 33 Front Page 33-43-11 201 MAR 01/18 33-43-11 202 MAR 01/18 33-43-11 203 MAR 01/18 33-43-11 401 MAR 01/18 33-43-11 402 MAR 01/18 33-43-11 403 MAR 01/18

CHAPTER

33 LIGHTS

B737-300/400/500 AIRCRAFT MAINTENANCE MANUAL

EFFECTIVITY

33-43-11 AIRPLANES WITH DEVORE POSITION LIGHTS Page 201 MDL-0377 MAR 01/18


STEADY POSITION (NAVIGATION) LIGHTS - MAINTENANCE PRACTICES 1. General

A. This procedure contains these tasks for the steady position light:

(1) The replacement of the lamp in a red or green steady position light (referred to as a colored light).

B. The colored lights are in each wingtip behind a window. The wingtip is sealed to

stop fuel fumes and water.

(1) To replace the lamp in a colored light, you remove the access panel below the wingtip. To replace the lamp in a forward colored light, you also remove the forward and middle fairings. The middle fairing contains the window.

2. Colored Steady Position Light - Lamp Replacement

A. References

Reference Title

20-10-47 P/B 201 SEALS ON OPEN ELECTRICAL TERMINAL IN FLAMMABLE LEAKAGE ZONE - MAINTENANCE PRACTICES

24-22-00 P/B 201 MANUAL CONTROL - MAINTENANCE PRACTICES (APPLY POWER) 57-21-11 P/B 401 REMOVABLE WING TIP - REMOVAL/INSTALLATION

B. Location Zones

Zone Area

301 Left Wing Tip 401 Right Wing Tip

C. Access Panels

Number Name/Location

7176 Wing Tip Access Panel (WBL 564) 7576 Wing Tip Access Panel (WBL 564)

D. Lamp Replacement

(1) Do one of these steps to remove electrical power from the colored steady position light:

(a) Open each applicable circuit breaker and attach the DO-NOT-CLOSE tag:

1) On the load control center panel, P18.

(b) On the overhead panel, P5, set the switch to the off position and attach

the DO-NOT-OPERATE tag.

(2) Get access to the colored light.

(a) Remove the screws that hold the access panel and remove the panel.

(b) For a forward colored light, also remove the forward and middle fairings


EFFECTIVITY



(3) Carefully replace the lamp.

(a) Loosen the captive retaining screws that hold the base of the colored light.

NOTE: Do not remove the retaining screws that hold the lens.

(b) Remove the base.

NOTE: Make sure you do not change the position of the index pin in the

base of the colored light.

(c) Loosen the pressure nut by two turns.

(d) Remove the lamp from the light socket.

(e) Clean the lens with a clean dry soft cloth.

(f) Install the new lamp in the light socket.

NOTE: Make sure the silver part of the lamp will point aft.

(g) Tighten the pressure nut with your fingers.

(h) Hold the base in its position with the index pin in the hole in the lens.

(i) Tighten the base retaining screws.

WARNING: MAKE SURE YOU SEAL THE TERMINALS TO PREVENT AN EXPLOSION OF THE FUEL FUMES. AN EXPLOSION CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.

(j) If it is necessary, do this task for the electrical terminals of the

colored light: SEALS ON OPEN ELECTRICAL TERMINAL IN FLAMMABLE LEAKAGE ZONE – MAINTENANCE PRACTICES, PAGEBLOCK 20-10-47/201.

NOTE: It is optional to seal the electrical connection.

NOTE: The sealant does not have to become tack-free prior to the

completion of this procedure and dispatch of the airplane.

E. Lamp Test

(1) Supply electrical power (PAGEBLOCK 24-22-00/201).

(2) Remove each DO-NOT-CLOSE or DO-NOT-OPERATE tag.

(a) Close each circuit breaker that was opened.

(3) Set the switch to the on position.

(a) Make sure the new lamp comes on correctly.

(4) Set the switch to the off position.

(5) If the fairings were removed, install them (PAGEBLOCK 57-21-11/401).


EFFECTIVITY



(6) Install the access panel with its screws.

(7) Close these access panels:



- - - - - END OF TASK - - - - -


EFFECTIVITY



STEADY POSITION (NAVIGATION) LIGHTS - REMOVAL/INSTALLATION 1. General

A. This procedure contains these tasks for the steady position light:

(1) The removal of a red or green steady position light (referred to as a colored light).

(2) The installation of a colored light.

B. The colored lights are in each wingtip behind a window(Figure 401). The wingtip is

sealed to stop fuel fumes and water. 2. Colored Steady Position Light - Removal

A. References

Reference Title

33-43-11 P/B 201 STEADY POSITION (NAVIGATION) LIGHTS – MAINTENANCE PRACTICES

57-21-11 P/B 401 REMOVABLE WING TIP - REMOVAL/INSTALLATION

B. Location Zones

Zone Area


C. Access Panels



D. Procedure

(1) Open these access panels:



(2) Do one of these steps to remove electrical power from the steady position

light:

(a) Open each applicable circuit breaker and attach the DO-NOT-CLOSE tag:

1) On the load control center panel, P18.

(b) At the overhead panel, P5, set the switch to the off position and attach the DO-NOT-OPERATE tag.


EFFECTIVITY



(3) Get access to the colored light.

(a) Remove the screws that hold the access panel and remove the panel.

(b) For a forward colored light, also remove the forward and middle fairings (PAGEBLOCK 57-21-11/401).

(4) Remove the colored light.

(a) Disconnect the electrical wires from the terminals of the colored light.

(b) Loosen the captive retaining screws that hold the base of the colored

light.

(c) Remove the base.

(d) If it is necessary, remove the lamp (PAGEBLOCK 33-43-11/201).

(e) Remove the lockwire from each lens retaining screw.

(f) Remove the lens retaining screws.

(g) Remove the lens retainer and the lens.

- - - - - END OF TASK - - - - - 3. Colored Steady Position Light - Installation

A. References

Reference Title

20-10-47 P/B 201 SEALS ON OPEN ELECTRICAL TERMINAL IN FLAMMABLE LEAKAGE ZONE - MAINTENANCE PRACTICES

24-22-00 P/B 201 MANUAL CONTROL - MAINTENANCE PRACTICES (APPLY POWER) 33-43-11 P/B 201 STEADY POSITION (NAVIGATION) LIGHTS – MAINTENANCE

PRACTICES 57-21-11 P/B 401 REMOVABLE WING TIP - REMOVAL/INSTALLATION

B. Location Zones

Zone Area


C. Access Panels



D. Light Installation

(1) Install the lens.

(a) Put the lens in its retainer.


EFFECTIVITY



(b) Hold the lens and its retainer in the bracket in the wingtip.

NOTE: For the left wingtip, make sure the index pin hole is on the bottom. For the right wingtip, make sure the index pin hole is on the top.

(c) Install each lens retaining screw and its lockwire.

(2) If it is necessary, replace the lamp (PAGEBLOCK 33-43-11/201).

(a) Hold the light base in its position with the index pin in the hole in the

lens.

(b) Tighten the base retaining screws.

(c) Connect the electrical wires to the terminals.

(d) Do this task: SEALS ON OPEN ELECTRICAL TERMINAL IN FLAMMABLE LEAKAGE ZONE - MAINTENANCE PRACTICES, PAGEBLOCK 20-10-47/201.

NOTE: It is optional to seal the electrical connection.

NOTE: The sealant does not have to become tack-free prior to the

completion of this procedure and dispatch of the airplane.

E. Light Test

(1) Supply electrical power (PAGEBLOCK 24-22-00/201).

(2) Remove each DO-NOT-CLOSE or DO-NOT-OPERATE tag.

(a) Close each circuit breaker that was opened when the colored light was removed.

(3) Set the switch to the on position.

(a) Make sure the light comes on correctly.

(4) Set the switch to the off position.

(5) If the fairings were removed, install them (PAGEBLOCK 57-21-11/401).

(6) Install the access panel with its screws.

(7) Close these access panels:



- - - - - END OF TASK - - - - -

aircraft manual supplementb737-42chgw pw051 24231 b737-448hgw pw595 25052 b737-4q8 pw233 25097...

Documents