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-0228 – ‘EFIS pin programming to TNT standard Document No: AMS-0228-001

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) Jan 09/2017

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 and

WDM. Therefore, this publication is a SUPPLEMENT to the associated AMM and WDM, and instructions on how to use this manual are equivalent to the instructions on how to use the manufacturers AMM and WDM.

C. This Manual Supplement has been raised to give historic design information pertaining to the following related aircraft

manuals:

WDM – Wiring Diagram Manual 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 PW701 PB899 2043 25147 OE-IAB PW701

INTRO-00 Page 1 Jan 09/17

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-0228 EFIS pin programming change to TNT standard

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 Jan 09/17

neilcTypewritten TextNeil Chettleburgh

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

34-22-11 –EFIS POWER/PROGRAM PINS – LEFT

34-22-21 –EFIS POWER/PROGRAM PINS – RIGHT

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 34-22-11 1 Jan 09/17 34-22-21 1 Jan 09/17

CHAPTER

34 NAVIGATION

B737-300/400/500 WIRING DIAGRAM MANUAL SUPPLEMENT

MSN25147/PW701

EFIS POWER/PROGRAM PINS - LEFT

34-22-11 INCORPORATES:

34-22-11 365 AEROSPACE MOD 0228 Page 1 Page 1

JAN 09/17 JAN 09/17

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

B737-300/400/500 WIRING DIAGRAM MANUAL SUPPLEMENT

MSN25147/PW701

EFIS POWER/PROGRAM PINS - RIGHT

34-22-21 INCORPORATES:

34-22-21 365 AEROSPACE MOD 0228 Page 1 Page 1

JAN 09/17 JAN 09/17

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

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

34-22-00 – Electronic Flight Instrument 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 34-22-00 501 JAN 09/17

CHAPTER

34 NAVIGATION

B737-300/400/500 AIRCRAFT MAINTENANCE MANUAL SUPPLEMENT

EFFECTIVITY

34-42-03 PW701 post MOD-0228

Page 501

Jan 09/17

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-0228 changes the EFIS pin programming to the TNT standard. It installs wiring at the Captain's and First Officer's EFIS control Panels to change the display setting from 'Track UP' to 'Heading Up' and it changes the pin programming of the Left and Right EFIS Symbol Generators in order to set below options: - Improve the airspeed trend indication - Display '1 CH' on the EADI to indicate single channel autopilot operation - Display a white 'ALT' height alert on the EADI at 2500 ft upon descent to selected altitude - Display analog 'RUNWAY' tied to localizer bar at 200 ft and below - Display full 360° compass rose - Display blinking 'PITCH' and 'ROLL' attitude comparator message - Display a range ring if the range is less than 160 NM and TCAS is activated

B. The operational test must be carried out in accordance with Boeing AMM 34-22-00.

Below tables provide the correct test results after incorporation of MOD-0228. 2. EFIS – Operational Test

G. EFIS Display Modes Test

Table 501 EFIS hex code lines

OE-IAB/PW701/25147 FA351B0 86BE008 E180000

Front PackageWiring Diagram Manual (WDM)Chapter 34 - NavigationWDM 34-22-11WDM 34-22-21Aircraft Maintenance Manual (AMM)Chapter 34 - NavigationAMM 34-22-00 pageblock 501

2017-01-16T10:52:15+0100Olivier Poelmans

2017-01-16T16:32:22+0000Neil Chettleburgh