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  • Page 1 of 5 DOA017/28.04.2011

    EASA Approval: EASA.21J.312

    Continued Airworthiness Instructions

    CAI No: CAI-757-2320-52 Revision: I

    Title: Communications - Data Transmission & Automatic Calling - DLink+ ACARS / CPDLC Installation

    Applicable Aircraft: Boeing 757-200/300

    Applicable Registrations/Variable Nos: All aircraft listed in CRA-757-2320-52 Rev J or later revision

    Affected Airworthiness Documents: Aircraft Flight Manual

    Maintenance Manual Illustrated Parts Catalog Wiring Diagram Manual Maintenance Program Electrical Load Analysis MEL Operations Manual Weight and Balance Other

    Document References: Boeing 757-200/300 Aircraft Flight Manual. Note AFM-757-2320-52 Rev D or later will be issued as separate document. Boeing 757-200/300 Aircraft Maintenance Manual Boeing 757-200/300 Illustrated Parts Catalog Boeing 757-200/300 Wiring Diagram Manual

    The operator is responsible for amending affected manuals with the continued airworthiness instructions contained herein. The technical content of this document is approved under the authority of Icelandair Technical Services Part 21 Subpart J DOA No. EASA.21J.312 - EASA STC: 10044500 Prepared by / Signature / Date:

    Approved by Signature / Date: Structures Avionic

  • EASA Approval: EASA.21J.312

    Continued Airworthiness Instructions

    CAI No: CAI-757-2320-52 Revision: I

    Page 2 of 5 DOA017/28.04.2011

    REVISION RECORD SHEET

    REVISION REVISION REASON DATE

    I/R

    N/A

    19/10/2012

    A Rev A issued to show relocation of the annunciator Panel from P5 overhead panel to P9 forward electronic control panel. Also, to correct revision status on documents.

    11/02/2013

    B Rev B issued to add reference to DDP-757-2320-52 I/R or later for equipment approval.

    25.03.2013

    C Rev C issued to add aircraft to effective list and applicable supplements

    8.10.2013

    D Rev C issued to add NRW/IKARS aircraft to effective list and applicable supplements

    12.11.2013

    E

    Rev E issued to add updated WDM drawings. 02.01.2014

    F

    Rev F issued to add updated WDM drawings. 01.04.2014

    G Rev G issued to add updated WDM drawings and adding new annunciator panels to IPC supplement.

    26.06.2014

    H Rev H issued to add updated WDM drawings, WDM supplement divided into A and B sections. AMM supplement updated for annunciator panel instructions.

    13.10.2014

    I Rev I issued to add aircraft ND037 (TF-ISY) 20.01.2015

  • EASA Approval: EASA.21J.312

    Continued Airworthiness Instructions

    CAI No: CAI-757-2320-52 Revision: I

    Page 3 of 5 DOA017/28.04.2011

    Table of Contents

    Item Content Page No 1 Description 4 2 Control and Operation 4 3 System Line Replaceable Units (LRU’s) 4 4 Equipment Locations 4 5 Certification Considerations 4 6 Equipment Approvals 5 7 Servicing Information 5 8 Maintenance Instructions 5 9 Troubleshooting Instructions 5 10 Removal and Replacement Information 5 11 Wiring Diagrams Supplements 5 12 Special Inspection Requirements 5 13 Application of Protective Treatments 5 14 Data 5 15 List of Special Tools 5 16 Recommended Overhaul Period 5 17 Airworthiness Limitations 5 18 Assistance 6 APPENDIX I Illustrated Parts Catalogue Supplement APPENDIX II-A Wiring Diagram Manual Supplement (Icelandair) APPENDIX II-B Wiring Diagram Manual Supplement

    (Nordwind/Ikar)

    APPENDIX III Aircraft Maintenance Manual Supplement

  • EASA Approval: EASA.21J.312

    Continued Airworthiness Instructions

    CAI No: CAI-757-2320-52 Revision: I

    Page 4 of 5 DOA017/28.04.2011

    1. Description: This change installs and activates a Spectralux Dlink+ system which provides Aircraft Communications Addressing and Reporting System (ACARS) / Controller Pilot Data Link Communications (CPDLC) system on the Boeing 757-200/-300 series aircraft. The system provides flight crews with the ability to send and receive messages over Very-High Frequency Digital Link (VDL) Mode A/2 networks.

    2. Control and Operation:

    Introduced in AMM supplement Appendix III

    3. System Line Replaceable Units (LRU’s): Equipment Part Number Description Reference

    M9000 14114-1-02 Dlink+ w/ CPDLC ACARS, Brown See Note

    M10386 8055515-4502 PTA-45B Data Printer See Note

    M9001 12854 Personality Module See Note

    M99001 ITS-757-2320-52-007-01 Annunciator Panel Assembly See Note

    M99002 PED523252-04-01 Annunciator Panel Assembly See Note

    M99003 PED523252-04-02 Annunciator Panel Assembly See Note Note: See Aircraft Maintenance Manual Supplement – Appendix III

    4. Equipment Locations: Equipment Location Dlink+ w/ CPDLC ACARS P8 Aft Control Stand Data Printer P8 Aft Control Stand Personality Module P8 Aft Control Stand Annunciator Panel Assembly P9 Forward Electronic Panel or P10 Control Stand.

    5. Certification Considerations: The Dlink+ w/CPDLC ACARS and the personality module unit have been approved fit for this installation by DDP-757-2320-52 I/R or later. A functional hazard analysis and system safety assessment was carried out by per document SSA-757-2320-52Rev B or later. Furthermore, the equipment are FAA TSO approved per FAA TSO-C160 and TSO-C113. The annunciator panel is a part of this design change and will be built by an approved production organisation.

  • EASA Approval: EASA.21J.312

    Continued Airworthiness Instructions

    CAI No: CAI-757-2320-52 Revision: I

    Page 5 of 5 DOA017/28.04.2011

    6. Equipment Approvals: Description Part Number Approval Dlink+ w/ CPDLC ACARS, Brown 14114-1-02 DDP-757-2320-52 I/R Data Printer, Brown 8055515-4502 PMA Personality Module 12854 DDP-757-2320-52 I/R Annunciator Panel Assembly ITS-757-2320-52-007-01 EASA Form 1 Release Annunciator Panel Assembly PED523252-04-01 EASA Form 1 Release Annunciator Panel Assembly PED523252-04-02 EASA Form 1 Release

    7. Servicing Information: The equipment are considered on-condition items

    8. Maintenance Instructions: Introduced in AMM supplement Appendix III

    9. Troubleshooting Instructions Introduced in AMM supplement Appendix III

    10. Removal and Replacement Information: Introduced in AMM supplement Appendix III

    11. Wiring Diagrams: Introduced in WDM supplement Appendix II

    12. Special Inspection Requirements: None

    13. Application of Protective Treatments: None

    14. Data: CRA-757-2320-52 Rev J or later provides reference to all data for this change

    15. List of Special Tools:

    None

    16. Recommended Overhaul Period:

    Introduced in AMM supplement Appendix III

    17. Airworthiness Limitations:

    N/A. There are no airworthiness limitations or any EWIS component that must be replaced at regular intervals due to this modification.

    18. Assistance: No special support is needed to carry out the continued airworthiness.

  • EASA Approval: EASA.21J.312

    APPENDIX I Illustrated Parts Catalog

    Supplement

    CAI No: CAI-757-2320-52 Revision: I

    APPENDIX I

    Illustrated Parts Catalog Supplement

  • EASA Approval: EASA.21J.312

    APPENDIX I Illustrated Parts Catalog

    Supplement

    CAI No: CAI-757-2320-52 Revision: I

    Title: Communications - Data Transmission & Automatic Calling - DLink+ ACARS / CPDLC Installation

    Applicable Aircraft/Components: Boeing 757-200/300

    Applicable Registrations/Variable Nos/Component Serial Numbers: All aircraft listed in CRA-757-2320-52 Rev J or later revision

    Affected Documentation

    Boeing 757-200/300 Illustrated Parts Catalog Front Matter

    1.1 Scope

    This document provides information related to the change incorporated by CRA-757-2320-52 Rev J or later

    1.2 Purpose

    Information herein supplements information provided in the existing aircraft IPC with information specific to CRA-757-2320-52 Rev J or later

    1.3 Definitions

    This document contains no words, terms, expressions, etc. that have varying interpretation throughout the industry.

    1.4 Referenced information

    Boeing 757, Illustrated Parts Catalog

    1.5 Distribution

    This documentation is to be distributed to each aircraft that has incorporated change specified in CRA-757-2320-52 Rev J or later as applicable above.

  • MANUAL SUPPLEMENT TO: Approval Doc:

    Boeing B757-200/300 IPC

    PAGE 1

    Figure 1

    Date 20.10.2015

    CRA-757-2320-52

    Figure 1 - DLINK LOCATION

    23-22-06-01The technical content of this document is approved under the authority of Icelandair Technical Services Part 21 Subpart J DOA Nr. EASA.21J.312

  • MANUAL SUPPLEMENT TO: Approval Doc:

    Boeing B757-200/300 IPC

    PAGE 2

    Figure 2

    Date 20.10.2015

    Figure 2 -DLINK

    The technical content of this document is approved under the authority of Icelandair Technical Services Part 21 Subpart J DOA Nr. EASA.21J.312

    23-22-06-01

    CRA-757-2320-52

    5

  • MANUAL SUPPLEMENT TO: Approval Doc:Boeing B757-200/300 IPC

    FIGITEM Part Number Nomenclature

    EffectFrom To

    UnitsPer

    Assy

    2 ALL

    5 14114-1-02 Dlink+ w/ CPDLC ACARS, Brown 1 - Mod 2 incorpurate

    V4PUZ9 ELECTRICL EQUIPMENT NUMBER: M9000

    -10 12854-4 UNIT - PERSONALITY MODULE 1 SUPPLIER CODE: V4PUZ9 ELECTRICL EQUIPMENT NUMBER: M9001

    PAGE 3

    Figure 2

    Date 20.10.2015

    The technical content of this document is approved under the authority of Icelandair Technical Services Part 21 Subpart J DOA Nr. EASA.21J.312

    23-22-06-01

    CRA-757-2320-52

  • MANUAL SUPPLEMENT TO: Approval Doc:

    Boeing B757-200/300 IPC

    PAGE 4

    Figure 3

    Date 20.10.2015

    The technical content of this document is approved under the authority of Icelandair Technical Services Part 21 Subpart J DOA Nr. EASA.21J.312

    23-22-06-01

    CRA-757-2320-52

    Figure 3 - Annunciation Panel Assembly - Config 1

    5

    A

  • MANUAL SUPPLEMENT TO: Approval Doc:Boeing B757-200/300 IPC

    FIGITEM Part Number Nomenclature

    EffectFrom To

    UnitsPer

    Assy

    3

    5 ITS-757-2320-52-007-01 .Annunciator Panel Assembly 1 ELECTRICL EQUIPMENT NUMBER: M99001 - Mod A incorpurated

    Note: For aircraft post EO-757-2320-60 satLINK MAX installation P/N PED523260-06-01 is installed.

    PAGE 5

    Figure 3

    Date 20.10.201523-22-06-01

    CRA-757-2320-52

    The technical content of this document is approved under the authority of Icelandair Technical Services Part 21 Subpart J DOA Nr. EASA.21J.312

    NT287 ND177 ND037 ND038 ND039

    ND164 NT915 NT914 NB079

    ND246 ND247 ND201 ND202

    ND203 NT861 NT862 NN001

    NN002 ND244 ND245 NC971

    NB139 NT913 NT916 NL141

  • MANUAL SUPPLEMENT TO: Approval Doc:

    Boeing B757-200/300 IPC

    PAGE 5Figure 4Date 20.10.2015

    CRA-757-2320-52

    Figure 4 - Annunciation Panel Assembly - Config 2

    The technical content of this document is approved under the authority of Icelandair Technical Services Part 21 Subpart J DOA Nr. EASA.21J.312

    23-22-06-01

    D

    10 5

  • MANUAL SUPPLEMENT TO: Approval Doc:Boeing B757-200/300 IPC

    FIGITEM Part Number Nomenclature

    EffectFrom To

    UnitsPer

    Assy4

    5 PED523252-04-01 .Annunciator Panel Assembly (Left-hand) 1 ELECTRICL EQUIPMENT NUMBER: M99002

    10 PED523252-04-02 .Annunciator Panel Assembly (Right-hand) 1 ELECTRICL EQUIPMENT NUMBER: M99003

    PAGE 6Figure 4Date 20.10.2015

    CRA-757-2320-52

    The technical content of this document is approved under the authority of Icelandair Technical Services Part 21 Subpart J DOA Nr. EASA.21J.312

    23-22-06-01

    NC073 NC072 NT377 NT376 NT378 NE301 NT346

    NT358

    NC073 NC072 NT377 NT376 NT378 NE301 NT346

    NT358

  • MANUAL SUPPLEMENT TO: Approval Doc:

    Boeing B757-200/300 IPC

    PAGE 1

    Figure 1

    Date 22.10.2014

    CRA-757-2320-52

    Figure 1 - PRINTER LOCATION

    The technical content of this document is approved under the authority of Icelandair Technical Services Part 21 Subpart J DOA Nr. EASA.21J.312

    31-33-01-01

  • MANUAL SUPPLEMENT TO: Approval Doc:Boeing B757-200/300 IPC

    PAGE 2

    Figure 2

    Date 22.10.2014

    CRA-757-2320-52Figure 2 - PRINTER

    The technical content of this document is approved under the authority of Icelandair Technical Services Part 21 Subpart J DOA Nr. EASA.21J.312

    31-33-01-01

  • MANUAL SUPPLEMENT TO: Approval Doc:Boeing B757-200/300 IPC

    FIGITEM Part Number Nomenclature

    EffectFrom To

    UnitsPer

    Assy

    2 ALL

    5 8055515-4502 .PRINTER - DATA (PTA-45B) 1 SUPPLIER CODE: V97896 ELECTRICL EQUIPMENT NUMBER: M10386 OPTIONAL PART: 8055515-4503 8055515-4506 8055515-4507

    -10 8050917-0006 ..PAPER ROLL - DATA PRINTER 1 SUPPLIER CODE: V97896

    PAGE 3

    Figure 2

    Date 22.10.2014

    CRA-757-2320-52

    The technical content of this document is approved under the authority of Icelandair Technical Services Part 21 Subpart J DOA Nr. EASA.21J.312

    31-33-01-01

  • EASA Approval: EASA.21J.312

    APPENDIX II-A Wiring Diagram Manual

    Supplement

    CAI No: CAI-757-2320-52 Revision: I

    APPENDIX II-A

    Wiring Diagram Manual Supplement Icelandair

  • EASA Approval: EASA.21J.312

    APPENDIX II-A Wiring Diagram Manual

    Supplement

    CAI No: CAI-757-2320-52 Revision: I

    Title: Communications - Data Transmission & Automatic Calling - DLink+ ACARS / CPDLC Installation

    Applicable Aircraft/Components: Boeing 757-200/300

    Applicable Registrations/Variable Nos/Component Serial Numbers: Aircraft listed in CRA-757-2320-52 Rev J or later (Groups 1-3)

    Affected Documentation

    Boeing 757-200/300 Wiring Diagram Manual Front Matter

    1.1 Scope

    This document provides information related to the change incorporated by CRA-757-2320-52 Rev J or later

    1.2 Purpose

    Information herein supplements information provided in the existing aircraft WDM with information specific to CRA-757-2320-52 Rev J or later

    1.3 Definitions

    This document contains no words, terms, expressions, etc. that have varying interpretation throughout the industry.

    1.4 Referenced information

    Boeing 757, Wiring Diagram Manual 1.5 Distribution

    This documentation is to be distributed to each aircraft that has incorporated change specified in CRA-757-2320-52 Rev J or later as applicable above.

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    EFFECTIVITY

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    The technical content of this docum

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    Subpart J D

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    OA N

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    Page 4.B

    EFFECTIVITY

    ND

    164

    The technical content of this docum

    ent is approved under

    the authority of Icelandair Technical Services Part 21

    Subpart J D

    OA N

    o. EASA.21J.312

    75

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    Page 4.C

    EFFECTIVITY

    NB079

    The technical content of this docum

    ent is approved under

    the authority of Icelandair Technical Services Part 21

    Subpart J D

    OA N

    o. EASA.21J.312

    75

    7-2

    00

    W

    IR

    IN

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    Page 4.D

    EFFECTIVITY

    NT287

    The technical content of this docum

    ent is approved under

    the authority of Icelandair Technical Services Part 21

    Subpart J D

    OA N

    o. EASA.21J.312

    75

    7-2

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    W

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    Page 5

    EFFECTIVITY

    ALL

    The technical content of this docum

    ent is approved under

    the authority of Icelandair Technical Services Part 21

    Subpart J D

    OA N

    o. EASA.21J.312

    75

    7-2

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    W

    IR

    IN

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    1

    23

    -2

    0-0

    0

    Page 6.A

    EFFECTIVITY

    ND

    177, N

    D164, N

    T914, N

    T915, N

    D246, N

    D247, N

    T287

    The technical content of this docum

    ent is approved under

    the authority of Icelandair Technical Services Part 21

    Subpart J D

    OA N

    o. EASA.21J.312

    75

    7-2

    00

    W

    IR

    IN

    G D

    IA

    GR

    AM

    M

    AN

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    REV. N

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    D164, N

    T914, N

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    D246, N

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    T287

    10

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    Page 6.B

    EFFECTIVITY

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    EFFECTIVITY

    ALL

    The technical content of this docum

    ent is approved under

    the authority of Icelandair Technical Services Part 21

    Subpart J D

    OA N

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    23

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    EFFECTIVITY

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    The technical content of this docum

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    the authority of Icelandair Technical Services Part 21

    Subpart J D

    OA N

    o. EASA.21J.312

    75

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    EFFECTIVITY

    NT914, N

    T915

    The technical content of this docum

    ent is approved under

    the authority of Icelandair Technical Services Part 21

    Subpart J D

    OA N

    o. EASA.21J.312

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    W

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    1

    23

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    0-0

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    EFFECTIVITY

    ND

    037, N

    D038, N

    D039, N

    D164, N

    D177, N

    D246, N

    D247

    The technical content of this docum

    ent is approved under

    the authority of Icelandair Technical Services Part 21

    Subpart J D

    OA N

    o. EASA.21J.312

    75

    7-2

    00

    W

    IR

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    EFFECTIVITY

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    EFFECTIVITY

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    EFFECTIVITY

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    ent is approved under

    the authority of Icelandair Technical Services Part 21

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    EFFECTIVITY

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