AIRCRAFT MANUAL SUPPLEMENT · 2018-11-22 · The convention for the use of this publication is in the same convention (ATA 100) as the associated manufacturers AMM, WDM, and IPC

AMES - Aerospace and Mechanical Engineering Services Ing. Walter Starzacher GesmbH

The Aircraft Manual Supplement is to be used in conjunction with the related aircraft 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 the applicable certification basis for the alterations/changes/modifications.

AMES Form: 22-21-AMF, Rev. 3 AMS_M352001005_AKI_01062018

Issued(Developed) by: AKI Revision: 0

Date: 11.06.2018 Page 1 of 15

AIRCRAFT MANUAL SUPPLEMENT FOR

B737 Registration Plates This Aircraft Manual Supplement is provided to support the continued airworthiness of the following:

Type Certificate Holder: The Boeing Company Model: Boeing 737 Classic and NG Effectivity: B737-400 MSN 25097, 28886, 28892, 28893, 29270 Applicable Type Certificate: EASA TCDS IM.A.120 Revision: Issue 14 Applicable Agency: EASA EASA Type Certificate/validation: see above Additional Information/Requirement: N/A Foreign Approval Reference: FAA A16WE Rev 62

AIRCRAFT MANUAL SUPPLEMENT


AMES Form: 22-21-AMF, Rev. 3 AMS_M352001005_AKI_01062018 Issued(Developed) by: AKI

Revision: 0 Date: 11.06.2018

Page 2 of 15

Record of Revision

This “Record of Revision” identifies all revisions to this report. When changes to this report are needed, revision will be issued by AMES. This “Record of Revision” shall remain in this document at all times.

Revision Content of/Reason for Revision Revision Date Inserted by Approved by

0 Initial Issue 08.06.2018 JTU DMA

Engineering Bulletin

The following section identifies the Engineering Bulletins for the alterations/changes/modifications which are related to this Aircraft Manual Supplement:

Document Revision

EB_M352001005_AKI_01062018 0

EB_M352001005_AKI_01062018.docx





Page 3 of 15

Introduction

1. General This publication was prepared by AMES – Aerospace and Mechanical Engineering Services GmbH (EASA DOA No. EASA.21J.299) 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 ONLY FOR THE AIRPLANE LISTED ON THE COVER PAGE OF THIS DOCUMENT. THIS MANUAL IS NOT SUITABLE FOR USE, INCLUDING WITHOUT LIMITATION, GENERAL INSTRUCTIONS OR TRAINING, FOR ANY AIRPLANES NOT LISTED HEREIN.

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. For information on the approval of the technical content of this document, please refer to the Change/Mod/Alteration listing. 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

B737-400 25097 OE-IAK

B737-400 28886 OE-IAM

B737-400 28892 OE-IBI

B737-400 28893 OE-IBL

B737-400 29270 OE-IBO

The technical content of this document is approved under the authority of DOA Nr. EASA.21J.299.





Page 4 of 15

TABLE OF CONTENTS

RECORD OF REVISION ........................................................................................................................ 2

ENGINEERING BULLETIN..................................................................................................................... 2

INTRODUCTION .................................................................................................................................. 3

ILLUSTRATED PARTS CATALOG ............................................................................................................ 5 CONTENTS ......................................................................................................................................... 6 11 PLACARDS & MARKINGS ............................................................................................................... 7

11-20-10-02Z-01 COCKPIT LESSOR PLATE INSTALL .................................................................................... 8 11-20-10-02Z-02 AIRFRAME LESSOR PLATE INSTALL ............................................................................... 10 11-20-10-02Z-03 AIRFRAME REG PLATE INSTALL ..................................................................................... 12 11-20-10-08Z-01 ENGINE LESSOR PLATE INSTALL .................................................................................... 14


ILLUSTRATED PARTS CATALOG




Page 5 of 15

ILLUSTRATED

PARTS

CATALOG






Page 6 of 15

CONTENTS

Chapter 11 - PLACARD & MARKINGS

11-20-10-02Z-01 COCKPIT LESSOR PLATE INSTALL

11-20-10-02Z-02 AIRFRAME LESSOR PLATE INSTALL

11-20-10-02Z-03 AIRFRAME REG PLATE INSTALL

11-20-10-08Z-01 ENGINE LESSOR PLATE INSTALL

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

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

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






Page 7 of 15

CHAPTER

11 PLACARDS & MARKINGS



EFFECTIVITY: MSN 25097, 28886, 28892, 28893, 29270

AMS_M352001005_AKI_01062018 Figure: 01

11.06.2018

A T A 1 1 - 2 0 - 0 2 Z REV: 0

PROPERTY OF AMES, CONFIDENTIAL. COPYRIGHT © AMES – ALL RIGHTS RESERVED The technical content of this document is approved under the authority of DOA No.

EASA.21J.299 Page 8 of 15

11-20-10-02Z-01 COCKPIT LESSOR PLATE INSTALL

COCKPIT LESSOR PLATE INSTALL

FIGURE 01 -

10



EFFECTIVITY: MSN 25097, 28886, 28892, 28893, 29270

AMS_M352001005_AKI_01062018 Figure: 01

11.06.2018

A T A 1 1 - 2 0 - 0 2 Z REV: 0



FIG ITEM PART NUMBER 1 2 3 4 5 6 7 NOMENCLATURE/VENDOR EFFECT UNITS PER

ASSY

01 - - COCKPIT LESSOR PLATE INSTALL

10 35220009 . Cockpit Lease Plate - MSN 25097 25097 1 10 35220010 . Cockpit Lease Plate - MSN 28886 28886 1 10 35220011 . Cockpit Lease Plate - MSN 28892 28892 1 10 35220012 . Cockpit Lease Plate - MSN 28893 28893 1 10 35220013 . Cockpit Lease Plate - MSN 29270 29270 1

MISSING ITEM NUMBERS NOT APPLICABLE

- ITEMS NOT ILLUSTRATED



EFFECTIVITY: MSN 25097, 28886, 28892, 28893, 29270

AMS_M352001005_AKI_01062018 Figure: 02

11.06.2018

A T A 1 1 - 2 0 - 0 2 Z REV: 0



11-20-10-02Z-02 AIRFRAME LESSOR PLATE INSTALL

AIRFRAME LESSOR PLATE INSTALL

FIGURE 02

10



EFFECTIVITY: MSN 25097, 28886, 28892, 28893, 29270

AMS_M352001005_AKI_01062018 Figure: 02

11.06.2018

A T A 1 1 - 2 0 - 0 2 Z REV: 0




ASSY

02 - - AIRFRAME LESSOR PLATE INSTALL

10 35220029 . Airframe Lease Plate - MSN 25097 25097 1 10 35220030 . Airframe Lease Plate - MSN 28886 28886 1 10 35220031 . Airframe Lease Plate - MSN 28892 28892 1 10 35220032 . Airframe Lease Plate - MSN 28893 28893 1 10 35220033 . Airframe Lease Plate - MSN 29270 29270 1





EFFECTIVITY: MSN 25097, 28886, 28892, 28893, 29270

AMS_M352001005_AKI_01062018 Figure: 03

11.06.2018

A T A 1 1 - 2 0 - 0 2 Z REV: 0



11-20-10-02Z-03 AIRFRAME REG PLATE INSTALL

AIRFRAME REG PLATE INSTALL FIGURE 03

10



EFFECTIVITY: MSN 25097, 28886, 28892, 28893, 29270

AMS_M352001005_AKI_01062018 Figure: 03

11.06.2018

A T A 1 1 - 2 0 - 0 2 Z REV: 0




ASSY

03 - - AIRFRAME REG PLATE INSTALL

10 35220024 . Airframe Reg Plate - MSN 25097 25097 1 10 35220025 . Airframe Reg Plate - MSN 28886 28886 1 10 35220026 . Airframe Reg Plate - MSN 28892 28892 1 10 35220027 . Airframe Reg Plate - MSN 28893 28893 1 10 35220028 . Airframe Reg Plate - MSN 29270 29270 1





EFFECTIVITY: MSN 25097, 28886, 28892, 28893, 29270

AMS_M352001005_AKI_01062018 Figure: 01

11.06.2018

A T A 1 1 - 2 0 - 0 8 Z REV: 0



11-20-10-08Z-01 ENGINE LESSOR PLATE INSTALL

ENGINE LESSOR PLATE INSTALL FIGURE 01

10



EFFECTIVITY: MSN 25097, 28886, 28892, 28893, 29270

AMS_M352001005_AKI_01062018 Figure: 01

11.06.2018

A T A 1 1 - 2 0 - 0 8 Z REV: 0




ASSY

01 - - ENGINE LESSOR PLATE INSTALL

10 35220014 . Engine Lease Plate (1) - MSN 25097 25097 1 10 35220015 . Engine Lease Plate (2) - MSN 25097 25097 1 10 35220016 . Engine Lease Plate (1) - MSN 28886 28886 1 10 35220017 . Engine Lease Plate (2) - MSN 28886 28886 1 10 35220018 . Engine Lease Plate (1) - MSN 28892 28892 1 10 35220019 . Engine Lease Plate (2) - MSN 28892 28892 1 10 35220020 . Engine Lease Plate (1) - MSN 28893 28893 1 10 35220021 . Engine Lease Plate (2) - MSN 28893 28893 1 10 35220022 . Engine Lease Plate (1) - MSN 29270 29270 1 10 35220023 . Engine Lease Plate (2) - MSN 29270 29270 1



Documents

AIRCRAFT MANUAL SUPPLEMENT · 2018-11-22 · The convention for the use of this publication is in the same convention (ATA 100) as the associated manufacturers AMM, WDM, and IPC