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AGÊNCIA NACIONAL DE AVIAÇÃO CIVIL - ANAC
LEGACY BJ - MPG (MPG-1483) TRANSMITTAL LETTER FOR TEMPORARY REVISION No. 8-1 SUBMITTED FOR APPROVAL ON: 01st NOVEMBER 2012 This transmittal letter presents LEGACY BJ - MPG Temporary Revision 8-1 with the sanction of Agência Nacional de Aviação Civil
- ANAC.
Page 3 of 6 - Update on page A2-67.
Page 4 of 6 - Update on page A2-71.
Pages 5 and 6 of 6 - Update on page A2-72.
Reasons:
The MPG-1483 revision 8 SECTION 3 - SYSTEMS & POWERPLANT INSPECTION REQUIREMENT is being revised due to editorial correction and APPENDIX 2 - AIRWORTHINESS LIMITATION REQUIREMENTS, is being revised based on the DCA 0145-028-00020-2011 revision E (FAA/ANAC) and revision D (EASA) to incorporate technical changes due to fuel system Record the incorporation of the revision on the Record of Temporary Revisions. Retain this transmittal letter and file it at the front of the report.
Signed by:
Actions: Has Spahment berced
MARIO LEHMERT RENAUD Please, refer to the highlights of this TR for more details. Agência Nacional de Aviação Civil - ANAC Insert the pages referred to below as indicated: MRB Chairman 12 november 2012 Page 1 of 6 - Update on page 3-21.
Page 2 of 6 - Update on page A2-66.
PLANNING GUIDE
LEGACY BJ - MAINTENANCE MPG-1483 TR 8-1 Oct 26/12 1 of 2 mpg1483 EMBRAER S.A.
AV. BRIGADEIRO FARIA LIMA, 2.170 - CAIXA POSTAL 8050 - TELEFONE (55) 12 3927-7517 FAX (55) 12 3927-7546 CEP. 12.227-901 - SÃO JOSÉ DOS CAMPOS - SÃO PAULO - BRASIL e-mail: distrib@embraer.com.br - http://www.embraer.com TO: HOLDERS OF PUBLICATION No. MPG-1483 - “MAINTENANCE PLANNING GUIDE”, APPLICABLE TO EMB-135BJ AIRCRAFT.
TEMPORARY REVISION No. 8- 1 DATED OCTOBER 26/2012
HIGHLIGHTS This highlights presents MPG Temporary Revision 8-1.
Please insert in your publication the attached page of the referred to Temporary Revision.
Enter this Temporary Revision in the Record of Temporary Revisions.
Insert this highlights at the front of the latest highlights in the manual.
This highlights must be discarded at the next revision.
Please do not hesitate to contact us for any additional information you may find of your needs.
1. Contents This issue encompasses Temporary Revision 8-1 – MPG-1483 dated October 26, 2012.
2.Outline of changes An outline of all changes is presented below.
PLANNING GUIDE
LEGACY BJ - MAINTENANCE MPG-1483 TR 8-1 Oct 26/12 2 of 2 mpg1483 SECTION 3 – SYSTEMS & POWERPLANT INSPECTION REQUIREMENTS Updated item 3.11 SYSTEMS AND POWER PLANT TASKS, as indicated below.
APPENDIX 2 – AIRWORTHINESS LIMITATION REQUIREMENTS Updated item A2.4 CRITICAL DESIGN CONFIGURATION CONTROL LIMITATION (CDCCL):
CDCCL item 8 was updated and CDCCL item 10 was created.
Updated item A2.5.2 – FUEL SYSTEM LIMITATION ITEMS, as indicated below.
The statement of FAA limitation was deleted.
REFERENCE NUMBER DESCRIPTION OF CHANGE 20-00-00-220-006-A00 TASK REVISED. Task description was editorially updated.
REFERENCE NUMBER DESCRIPTION OF CHANGE 28-50-01-220-001-A02 NEW TASK. New task created.
28-50-01-720-001-A00 NEW TASK. New task created.
28-50-08-212-001-A00 NEW TASK. New task created.
28-50-09-212-001-A00 NEW TASK. New task created.
28-50-10-212-001-A00 NEW TASK. New task created.
PLANNING GUIDE
LEGACY BJ - MAINTENANCE MPG-1483 Oct 26/12 mpg1483
RECORD OF TEMPORARY REVISIONS T.R.
No.
DATE ISSUED DATE
REMOVED
INCORPORATED BY T.R.
No.
DATE ISSUED DATE
REMOVED
INCORPORATED BY 0-1 Feb 06/02 Nov 26/02 Revision 1 0-2 May 29/02 Nov 26/02 Revision 1 0-3 Jun 13/02 Nov 26/02 Revision 1 0-4 Sep 16/02 Nov 26/02 Revision 1 1-1 Dec 06/02 Jul 31/03 Revision 2 2-1 Sep 16/03 Apr 01/04 Revision 3 2-2 Nov 21/03 Apr 01/04 Revision 3 3-1 Jun 24/04 Oct 14/05 Revision 4 3-2 Sep 03/04 Oct 14/05 Revision 4 3-3 Oct 19/04 Oct 14/05 Revision 4 3-4 Jun 22/05 Oct 14/05 Revision 4 4-1 Dec 20/05 Mar 22/07 Revision 5 6-1 Oct 02/09 Aug 12/10 Revision 7 7-1 Oct 13/10 Apr 27/12 Revision 8 7-2 Feb 22/11 Apr 27/12 Revision 8 7-3 Feb 24/11 Apr 27/12 Revision 8 7-4 May 12/11 Apr 27/12 Revision 8 8-1 Oct 26/12
AGÊNCIA NACIONAL DE AVIAÇÃO CIVIL - ANAC
LEGACY BJ - MPG (MPG-1483) TRANSMITTAL LETTER FOR TEMPORARY REVISION No. 8-1 SUBMITTED FOR APPROVAL ON: 26th OCTOBER 2012 This transmittal letter presen ts LEGACY BJ - MPG Temporary Revision 8-1 with the sanction of Agência Nacional de Aviação Civil
- ANAC.
Reasons:
The MPG-1483 revision 8 SECTION 3 - SYSTEMS & POWERPLANT INSPECTION REQUIREMENT is being revised due to editorial correction and APPENDIX 2 - AIRWORTHINESS LIMITATION REQUIREMENTS, is being revised based on the DCA 0145-028-00020-2011 revision E (FAA/ANAC) and revision D (EASA) to incorporate technica l changes due to fuel system limitation.
Actions:
Please, refer to the highlights of this TR for more details.
Insert the pages referred to below as indicated:
Page 1 of 6 – Update on page 3-21.
Page 2 of 6 – Update on page A2-66.
Page 3 of 6 – Update on page A2-67.
Page 4 of 6 – Update on page A2-71.
Pages 5 and 6 of 6 – Update on page A2-72.
Record the incorporation of the revision on the Record of Temporary Revisions. Retain this transmittal lett er and file it at the front of the report.
Signed by:
MARIO LEHMERT RENAUD Agência Nacional de Aviação Civil - ANAC MRB Chairman Date:
PLANNING GUIDE
LEGACY BJ - MAINTENANCE MPG-1483 TR 8-1 Oct 26/12 1 of 6 mpg1483 MPG - TEMPORARY REVISION No. 8-1 TO: HOLDERS OF PUBLICATION No. MPG-1483 - "MAINTENANCE PLANNING GUIDE", APPLICABLE TO EMB-135BJ AIRCRAFT.
REASON: Editorial correction.
FILING INSTRUCTIONS: Insert this in Section 3 - Systems & Powerplant Inspection Requirements, facing on page 3-21.
On page 3-21:
Update the description of task 20-00-00-220-006-A00, as described below.
From:
To:
REFERENCE NUMBER TYPE DESCRIPTION INT EFFECT TOLERANCE 20-00-00-220-006-A00 DET Inspect (Detailed Inspection) Ventral Fuel Tank - EWIS Components Of Ventral Tank Unit Harness (Zone: 196).
NOTE: EWIS 48 MO L650 ± 30 Days
REFERENCE NUMBER TYPE DESCRIPTION INT EFFECT TOLERANCE 20-00-00-220-006-A00 DET Inspect (Detailed Inspection) Ventral Fuel Tank - EWIS Components Of Ventral Tank Unit Harness (Zone: 1972).
NOTE: EWIS 48 MO L650 ± 30 Days
PLANNING GUIDE
LEGACY BJ - MAINTENANCE MPG-1483 TR 8-1 Oct 26/12 2 of 6 mpg1483 MPG - TEMPORARY REVISION No. 8-1 TO: HOLDERS OF PUBLICATION No. MPG-1483 - "MAINTENANCE PLANNING GUIDE", APPLICABLE TO EMB-135BJ AIRCRAFT.
REASON: The MPG-1483 revision 8 APPENDIX 2 - AIRWORTHINESS LIMITATION REQUIREMENTS, is being revised based on the DCA 0145-028-00020-2011 revision E (FAA/ANAC) and revision D (EASA) to incorporate technical changes due to fuel system limitation.
FILING INSTRUCTIONS: Insert this in Appendix 2 - Airworthiness Limitation Requirements, facing on page A2-66.
On page A2-66, update CDCCL item 8, as indicated below.
From:
To:
8) Wires inside the pumps The type, length and supporting of wires used inside the fuel pumps are such that provide enough clearance from any internal surface of the pump, what prevents from chafing and arcing. This configuration is a CDCCL item and must be retained if any maintenance task that requires the pump to be disassembled is performed. The pumps CMM provide warnings about the critical configuration of the wires in the pumps. This is applicable for all fuel pumps of all tanks of the aircraft.
NOTE: Applicable to aircraft Equipped with Ventral Fuel Tank and AE3007A2 Engines, commercially called Legacy 650 and identified in the MPG as L650.
8) Wires inside the pumps The type, length and supporting of wires used inside the fuel pumps are such that provide enough clearance from any internal surface of the pump, what prevents from chafing and arcing. This configuration is a CDCCL item and must be retained if any maintenance task that requires the pump to be disassembled is performed. The pumps CMM provide warnings about the critical configuration of the wires in the pumps. This is applicable for all fuel pumps of all tanks of the aircraft, including the pumps equipped with the CHA.
NOTE: Applicable to aircraft Equipped with Ventral Fuel Tank and AE3007A2 Engines, commercially called Legacy 650 and identified in the MPG as L650.
PLANNING GUIDE
LEGACY BJ - MAINTENANCE MPG-1483 TR 8-1 Oct 26/12 3 of 6 mpg1483 MPG - TEMPORARY REVISION No. 8-1 TO: HOLDERS OF PUBLICATION No. MPG-1483 - "MAINTENANCE PLANNING GUIDE", APPLICABLE TO EMB-135BJ AIRCRAFT.
REASON: The MPG-1483 revision 8 APPENDIX 2 - AIRWORTHINESS LIMITATION REQUIREMENTS, is being revised based on the DCA 0145-028-00020-2011 revision E (FAA/ANAC) and revision D (EASA) to incorporate technical changes due to fuel system limitation.
FILING INSTRUCTIONS: Insert this in Appendix 2 - Airworthiness Limitation Requirements, facing on page A2-67.
On page A2-67, insert the new CDCCL item 10, as indicated below.
10) Fuel Pump PTFE Interface fitting at the Tank Wall Fuel pumps of main wing tanks and auxiliary tanks having PTFE interface fitting, whic h are installed on the tanks wall. This fi tting is highlighted as CDCCL in the appropriate AMM procedures, to chec k proper installation, leakproofness, during periodic inspections or whenever pump is changed.
NOTE: Applicable to aircraft Equipped with Ventral Fuel Tank and AE3007A2 Engines, commercially called Legacy 650 and identified in the MPG as L650.
PLANNING GUIDE
LEGACY BJ - MAINTENANCE MPG-1483 TR 8-1 Oct 26/12 4 of 6 mpg1483 MPG - TEMPORARY REVISION No. 8-1 TO: HOLDERS OF PUBLICATION No. MPG-1483 - "MAINTENANCE PLANNING GUIDE", APPLICABLE TO EMB-135BJ AIRCRAFT.
REASON: The MPG-1483 revision 8 APPENDIX 2 - AIRWORTHINESS LIMITATION REQUIREMENTS, is being revised based on the DCA 0145-028-00020-2011 revision E (FAA/ANAC) and revision D (EASA) to incorporate technical changes due to fuel system limitation.
FILING INSTRUCTIONS: Insert this in Appendix 2 - Airworthiness Limitation Requirements, facing on page A2-71.
On page A2-71:
Insert the new tasks 28-50-01-220-001-A02 and 28-50-01-720-001-A00, as indicated below.
REFERENCE NUMBER TYPE DESCRIPTION ZONE INT EFFECT TOLERANCE 28-50-01-220-001-A02 DET Inspect (Detail ed Inspection) Fuel Pump Electrical Harness CHA (Cable Harness Assembly) end fitting.
NOTE: Applicable to aircraft with fuel pump harness with corrugated conduit.
155/156 157/197 271/272 1972 10,000 FH or 48 MO L650 Not Applicable 28-50-01-720-001-A00 FNC Functionally Chec k Fuel Pump Elec trical Harness for Leakage.
NOTE: Applicable to aircraft with fuel pump harness with corrugated conduit.
155/156 157/197 271/272 1972 20,000 FH or 96 MO L650 Not Applicable
PLANNING GUIDE
LEGACY BJ - MAINTENANCE MPG-1483 TR 8-1 Oct 26/12 5 of 6 mpg1483 MPG - TEMPORARY REVISION No. 8-1 TO: HOLDERS OF PUBLICATION No. MPG-1483 - "MAINTENANCE PLANNING GUIDE", APPLICABLE TO EMB-135BJ AIRCRAFT.
REASON: The MPG-1483 revision 8 APPENDIX 2 - AIRWORTHINESS LIMITATION REQUIREMENTS, is being revised based on the DCA 0145-028-00020-2011 revision E (FAA/ANAC) and revision D (EASA) to incorporate technical changes due to fuel system limitation.
FILING INSTRUCTIONS: Insert this in Appendix 2 - Airworthiness Limitation Requirements, facing on page A2-72.
On page A2-72:
Insert the new tasks 28-50-08-212-001-A00, 28-50-09-212-001-A00 and 28-50-10-212-001-A00, as indicated below.
REFERENCE NUMBER TYPE DESCRIPTION ZONE INT EFFECT TOLERANCE 28-50-08-212-001-A00 GVI Inspect (General Visual) Ventral Fuel Tank External Harness 1972 10,000 FH or 48 MO L650 Not Applicable 28-50-09-212-001-A00 GVI Inspect (General Visual) FWD Fuel Tank External Harness 191/197 10,000 FH or 48 MO L650 Not Applicable 28-50-10-212-001-A00 GVI Inspect (General Visual) Aft Fuel Tank External Harness 271/272 10,000 FH or 48 MO L650 Not Applicable
PLANNING GUIDE
LEGACY BJ - MAINTENANCE MPG-1483 TR 8-1 Oct 26/12 6 of 6 mpg1483 MPG - TEMPORARY REVISION No. 8-1 TO: HOLDERS OF PUBLICATION No. MPG-1483 - "MAINTENANCE PLANNING GUIDE", APPLICABLE TO EMB-135BJ AIRCRAFT.
REASON: The MPG-1483 revision 8 APPENDIX 2 - AIRWORTHINESS LIMITATION REQUIREMENTS, is being revised based on the DCA 0145-028-00020-2011 revision E (FAA/ANAC) and revision D (EASA) to incorporate technical changes due to fuel system limitation.
FILING INSTRUCTIONS: Insert this in Appendix 2 - Airworthiness Limitation Requirements, facing on page A2-72.
On page A2-72:
Delete the statement indicated below:
In addition to the Fuel System Limitation requirements, the following limitation is being added to EMB-135BJ with Ventral Fuel Tank and AE3007A2 engines installed (Legacy 650) under FAA certification:
The EMB-135BJ (Legacy 650) shall not be operated past September 30th, 2013 unless the owner or operator has incorporated a major type design change that complies with provisions of 14CFR Part 25.981(a)(3), amendment 102 or later.
Changes to this limitation can be accomplished by FAA approval of major type design change required in accordance with §21.97.