instructions for continued airworthiness document

16
Table of Contents This document is produced on behalf of 365 Aerospace Limited, UK. 365 Aerospace own the copyright of the format of this document, which is supplied in confidence. The contents must not be reproduced without permission in writing from 365 Aerospace. Form No 365-117 (Issue 1) INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT In accordance with EASA CS 25.1529/FAR 25.1529, Appendix H For 365 Aerospace Modification: MOD-0109 – Change for the Introduction of a Bose A20 Headset ICA Document No: ICA-0109-001

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Page 1: INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT

Table of Contents

This document is produced on behalf of 365 Aerospace Limited, UK. 365 Aerospace own the copyright of the format of this document, which is supplied in confidence. The contents must not be reproduced without permission in writing from 365 Aerospace.

Form No 365-117 (Issue 1)

INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT In accordance with EASA CS 25.1529/FAR 25.1529, Appendix H

For 365 Aerospace Modification: MOD-0109 – Change for the Introduction of a Bose A20 Headset ICA Document No: ICA-0109-001

Page 2: INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT

TOC-00

TABLE OF CONTENTS

Front Page FP-00

Table of Contents TOC-00

Document Approval DA-00

Highlights HL-00

Record of Revision RR-00

Introduction INTRO-00

List of Effective Aircraft LEA-00

Change/Modification Listing CML-00

Instructions for Continued Airworthiness

ICA-01 Change for the Introduction of Bose A20 Headsets ICA-01

IPC Illustrated Parts Catalogue IPC

Page 3: INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT

DA-00

DOCUMENT APPROVAL

A. With reference to any change/modification referenced in this document, the technical content of the supplemental information

associated with any listed change/modification is approved under the authority of DOA No. EASA.21J.575. B. With reference to any Owner/Operator/Supplier change or modification, the technical content of the supplemental information

associated with any listed change/modification is approved under the authority of the named Owner/Operator/Supplier of the source documents. The Owner/Operator/Supplier of the source documents has given the compiler the rights to use their information in order to produce this document.

C. The Checking process will include a verification of technical consistency with the associated change/modification and any

compliance documentation which may relate to effectivity, description, effects on airworthiness and environmental protection especially when limitations are changed or affected.

D. The approval process will include ultimate verification of the Instructions for Continued Airworthiness by a 365 Aerospace Ltd

Certification Verification Engineer.

Checked: Print Name:

CVE Approved: Print Name:

Mitchellh
Typewritten Text
M. Hills
Mitchellh
Typewritten Text
D. Jackson
Page 4: INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT

HL-00

HIGHLIGHTS Issue 2 Document Title Change – was ‘B737-300/400 – TNT Fleet’, now ‘For 365 Aerospace Modification: MOD-0109 – Change for the Introduction of a Bose A20 Headset’ Document Number Change – was ‘ICA-737-345-TNT’, now ‘ICA-0109-001’ Addition of IPC Section Issue 3 List of Effective Aircraft Change – addition of MSN 27632 Issue 4 List of Effective Aircraft Change – addition of MSNs 25110, 25111 & 25147 Issue 5 List of Effective Aircraft Change – addition of MSNs 29201, 29202, & 29203 Issue 6 List of Effective Aircraft Change – addition of MSNs 25097, 28886, 28892, 28893, & 29270 Issue 7 List of Effective Aircraft Change – addition of MSN 27143

Page 5: INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT

RR-00

RECORD OF REVISION

Issue Date Issue Date Initial (1) DEC 02/15

2 JAN 01/16 3 JUN 01/16 4 OCT 19/16 5 APR 01/18 6 JUL 01/18 7 JUN 01/20

This document is to be used in conjunction with the related aircraft’s manuals, as prescribed in the Contents Page of this Section 00. The information contained within this manual relates to various customer orientated changes that have been carried out on the associated aircraft. A list of effective customer orientated changes can be found in the Change/Modification List section of this document. These changes/modifications are in addition to the initial design of the aircraft and are therefore detailed within this manual using appropriate and related convention.

Page 6: INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT

INTRO-00

INTRODUCTION

1. Scope The purpose of this document is to provide Instructions for Continued Airworthiness in accordance with EASA CS 25.1529/FAR

25.1529. Appendix H 2. Information about sections of this document

2.1 Instructions for Continued Airworthiness – ICA-XX

(1) This section lists and prescribes continuing airworthiness information for an individual change/modification. Its convention is informative so that it obligates the aircraft operator to include certain information provided by this document into relevant operational manuals, including, but not exclusive to, the operators aircraft scheduled maintenance program.

2.2 Instructions for Continued Airworthiness – WDM, AWM, IPC, AMM, etc. (if applicable)

(1) These sections were prepared by 365 Aerospace Ltd and are 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 that are in addition to the associated airplane’s type design.

NOTE: THIS SUPPLEMENTAL INFORMATION PREPARED SPECIFICALLY TO COVER THE AIRPLANE(S)

LISTED IN THE "LIST OF EFFECTIVE AIRCRAFT" SECTION.

THIS MANUAL IS NOT SUITABLE FOR USE, INCLUDING WITHOUT LIMITATION, GENERAL INSTRUCTIONS OR TRAINING, FOR ANY AIRPLANES NOT LISTED HEREIN.

(2) The convention for the use of these sections is in the same convention (ATA 100) as the associated OEM

manuals. Therefore, this publication is deemed as SUPPLEMENTAL to the associated OEM manuals, and instructions on how to use the data is the same.

Page 7: INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT

LEA-00

LIST OF EFFECTIVE AIRCRAFT

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

B737-476SF 061 PW541 PA431 2324 24440 OE-IAJ

B737-4Q8SF 811 PW241 PA612 2505 25105 OE-IAE B737-4Q8F 665 PW245 PA668 2561 25109 OE-IBW B737-4Q8F 104 150 PW094 PA317 2210 25168 OE-IAG

B737-4Y0F 650 790 PW050 PA334 2227 25184 OE-IAF

B737-45DSF 401 PV281 2458 27131 OO-TNN

B737-45BDSF 2589 27256 OO-TNP

B737-49RSF 2833 28881 OO-TNO

B737-34SBDSF 325 PR091 PC121 2983 29108 OE-IBZ

B737-34SBDSF 326 PR092 PC139 3001 29109 OO-TNL

B737-4M0F 423 PW445 PC194 3056 29205 OO-TNQ

B737-4M0F 424 PW446 PC196 3058 29206 OE-IAP

B737-4M0F 425 PW447 PC216 3078 29207 OE-IAQ

B737-4M0SF 426 PW448 PC219 3081 29208 OE-IAR

B737-4M0F 427 PW449 PC225 3087 29209 OE-IAS

B737-4M0F 428 500 PW450 PC229 3091 29210 OE-IAT

B737-48E 2857 27632 OE-IAX

B737-4Q8 2299 25097 OE-IAK

B737-4Q8 2586 25110 OE-IAY

B737-4Q8 2605 25111 OE-IAZ

B737-4Z9 2043 25147 OE-IAB

B737-4M0 3018 29201 OE-IAU

B737-4M0 0325 29202 OE-IAC

B737-4M0 3049 29203 OE-IAD

B737-490 2902 28886 OE-IAM

B737-490 3036 28892 OE-IBI

B737-490 3039 28893 OE-IBL

B737-490 3038 29270 OE-IBO

B737-42JSF 27143 OE-IWP

Page 8: INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT

CML-00

CHANGE/MODIFICATION LISTING DOA Mod/STC information

Mod/STC Ref: Title:

MOD-0109 Change for the Introduction of Bose A20 Headsets

Owner/Operator/Supplier Mod/STC Information

Owner / Operator/

Supplier Mod/STC Ref: DOA Mod/STC Ref

(If applicable): Title: Supplier:

Page 9: INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT

ICA-01 Page 1 JUN 01/20

INSTRUCTIONS FOR CONTINUED AIRWORTHINESS ICA-01 Change for the Introduction of Bose A20 Headsets 1.1 General (1) This section relates to 365 Aerospace Ltd’s Modification No. MOD-0109

(2) Modification of the associated aircraft and aircraft type, for which the above modification relates, obligates the aircraft operator to include pertinent maintenance information provided by this document into the operators aircraft scheduled maintenance program.

(3) In the event of conflicting or contradictory instruction between any aircraft manual data and this document, 365 Aerospace

should be consulted before implementing the use of the instructions. 1.2 Airworthiness Limitations

(1) The Airworthiness Limitations section is approved and variations must also be approved.

(2) Those limitations and procedures previously approved by National Authorities, OEMs, etc., and not contained in this document are unchanged.

(3) In relation to the above 365 Aerospace Modification, certain operational approvals require that the aircraft and/or systems

comply with specified design requirements. Where this modification records compliance with those design requirements this will not be taken as acceptance by the Agency of compliance with the relevant operational requirements, for which further justification may be required.

(4) In relation to the above 365 Aerospace Modification, the aircraft operator is required to review the performance of the new

headset within the operational surroundings with reference to FAA Special Airworthiness Information Bulletin (SAIB) CE-16-08 and Information for Operators, InFO-07001.

1.3 Maintenance Schedule Changes

(1) If the Noise Cancellation of the Bose A20 headsets is to be powered through a battery supply rather than the aircraft power supply, then it is recommended that operators ensure that necessary means of power are available for the headsets in the form of a weekly check of the condition and charge of the headset batteries and ensure that separate battery back-up is available for each headset on any active service. This is not required for headsets that are powered through the aircraft systems.

(2) All maintenance of the Bose A20 Headsets should be in accordance with Bose A20 Aviation Headset Owners Guide. 1.4 Additional EWIS Tasks None.

Page 10: INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT

ILLUSTRATED

PARTS

CATALOGUE

Contents

Page 11: INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT

IPC-CONTENTS Page 1

Chapter 11 PLACARD & MARKINGS

Chapter 21 AIR CONDITIONING

Chapter 22 AUTO FLIGHT

Chapter 23 COMMUNICATIONS

23-50-01-99Z – HEADPHONE ASSY - ELECTRICAL

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

Page 12: INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT

IPC-CONTENTS Page 2

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 13: INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT

IPC-LEF Page 1

LIST OF EFFECTIVE PAGES

Description Page No. Date Description Page No. Date

IPC Front Page IPC Contents 1 IPC Contents 2 IPC-LEF 1 Chapter 23 Front Page 23-50-01-99Z 0 JAN 01/16 23-50-01-99Z 1 JAN 01/16

Page 14: INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT

CHAPTER

23 COMMUNICATIONS

Page 15: INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT

B737-300/400/500 ILLUSTRATED PARTS CATALOGUE

23-50-01-99Z 23-50-01 MOD-0109 Fig 99Z JAN 01/16 Page 0

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

HEADPHONE ASSY - ELECTRICAL FIGURE 99Z

Page 16: INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT

B737-300/400/500 ILLUSTRATED PARTS CATALOGUE

23-50-01-99Z 23-50-01 MOD-0109 Fig 99Z JAN 01/16 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-0109-001 CHANGE FOR THE INTRODUCTION OF A BOSE A20 HEADSET RF

10 324843-2020 • HEADSET – NOISE CANCELLING (MODEL: BOSE A20) 3 (11-08728)

-- ITEMS NOT ILLUSTRATED