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AGENCIA NACIONAL DE AVIAÇÃO CIVIL - ANAC
LEGACY BJ - MPG (MPG-1483) TRANSMITTAL LETTER FOR TEMPORARY REVISION No. 8-2 SUBMITTED FOR APPROVAL ON: 05th DECEMBER 2012 This transmittal letter presents LEGACY BJ - MPG Temporary Revision 8-2 with the sanction of Agência Nacional de Aviação Civil
- ANAC.
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.
Reasons:
The MPG-1483 revision 8 SECTION 4 - STRUCTURAL INSPECTION REQUIREMENTS and APPENDIX 2 AIRWORTHINESS LIMITATION REQUIREMENTS, is being revised based on the DCA 0145-054-00015-2012 revision B (ANAC) and revision A (FAA/EASA) to incorporate technical changes.
Actions:
Please, refer to the highlights of this TR for more details.
Insert the pages referred to below as indicated:
Page 1 of 4 - Update on page 4-47.
Page 2 and 3 of 4 - Update on page A2-12.
Page 4 of 4 - Update on page A2-34.
Signed by:
MARIO LEHMERT RENAUD Main lehmen denud.
Agência Nacional de Aviação Civil - ANAC MaRe chaima 2 January 2013
PLANNING GUIDE
LEGACY BJ - MAINTENANCE MPG-1483 TR 8-2 Dec 05/12 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. 8-2 DATED DECEMBER 05/2012
HIGHLIGHTS This highlights presents MPG Temporary Revision 8-2.
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 8-2 – MPG-1483 dated December 05, 2012.
2.Outline of changes An outline of all changes is presented below.
PLANNING GUIDE
LEGACY BJ - MAINTENANCE MPG-1483 TR 8-2 Dec 05/12 2 of 2 mpg1483 SECTION 4 – STRUCTURAL INSPECTION REQUIREMENTS Updated item 4.10 STRUCTURAL TASKS, as indicated below.
APPENDIX 2 – AIRWORTHINESS LIMITATION REQUIREMENTS Created item A2.3.2 - IMPLEMENTATION OF REVISED AIRWORTHINESS LIMITATIONS.
Updated numbering of INSPECTION INTERVAL LIMIT from A2.3.2 to A2.3.3.
Created four (4) new INSPECTION INTERVAL LIMITS for SSI 54-50-05.
REFERENCE NUMBER DESCRIPTION OF CHANGE 54-50-00-220-808-L00 NEW TASK. New task created.
54-50-00-220-809-L00 NEW TASK. New task created.
PLANNING GUIDE
LEGACY BJ - MAINTENANCE MPG-1483 Dec 05/12 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 Nov 12/12 8-2 Dec 05/12
AGÊNCIA NACIONAL DE AVIAÇÃO CIVIL - ANAC
LEGACY BJ - MPG (MPG-1483) TRANSMITTAL LETTER FOR TEMPORARY REVISION No. 8-2 SUBMITTED FOR APPROVAL ON: 05th DECEMBER 2012 This transmittal letter presen ts LEGACY BJ - MPG Temporary Revision 8-2 with the sanction of Agência Nacional de Aviação Civil
- ANAC.
Reasons:
The MPG-1483 revision 8 SECTION 4 - STRUCTURAL INSPECTION REQUIREMENTS and APPENDIX 2 - AIRWORTHINESS LIMITATION REQUIREMENTS, is being revised based on the DCA 0145-054-00015-2012 revision B (ANAC) and revision A (FAA/EASA) to incorporate technical changes.
Actions:
Please, refer to the highlights of this TR for more details.
Insert the pages referred to below as indicated:
Page 1 of 4 – Update on page 4-47.
Page 2 and 3 of 4 – Update on page A2-12.
Page 4 of 4 – Update on page A2-34.
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 8-2 Dec 05/12 1 of 4 mpg1483 MPG - TEMPORARY REVISION No. 8-2 TO: HOLDERS OF PUBLICATION No. MPG-1483 - "MAINTENANCE PLANNING GUIDE", APPLICABLE TO EMB-135BJ AIRCRAFT.
REASON: The MPG-1483 revision 8 SECTION 4 - STRUCTURAL INSPECTION REQUIREMENTS, is being revised based on the DCA 0145- 054-00015-2012 revision B (ANAC) and revision A (FAA/EASA) to incorporate technical changes.
FILING INSTRUCTIONS: Insert this in Section 4 - Structural Inspection Requirements, facing on page 4-47.
On page 4-47:
Insert the new tasks 54-50-00-220-808-L00 and 54-50-00-220-809-L00, as indicated below.
REFERENCE NUMBER TYPE DESCRIPTION THRESHOLD INT ZONE EFFECT TOLERANCE 54-50-00-220-808-L00 DET Internally inspect the PYLON component:
• Pylon yokes I and II (SSI 54-50-05) primary element.
– 4713 FC 414/424 ALL Not Applicable 54-50-00-220-809-L00 DET Internally inspect the PYLON component:
• Pylon yokes I and II (SSI 54-50-05) secondary element.
10000 FC 1130 FC 414/424 ALL Not Applicable
PLANNING GUIDE
LEGACY BJ - MAINTENANCE MPG-1483 TR 8-2 Dec 05/12 2 of 4 mpg1483 MPG - TEMPORARY REVISION No. 8-2 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 0145-054-00015-2012 revision B (ANAC) and revision A (FAA/EASA) to incorporate technical changes.
FILING INSTRUCTIONS: Insert this in Appendix 2 - AIRWORTHINESS LIMITATION REQUIREMENTS, facing on page A2-12.
On page A2-12, insert the item below and update the numbering of INSPECTION INTERVAL LIMIT:
A2.3.2 IMPLEMENTATION OF REVISED AIRWORTHINESS
LIMITATIONS This Section will be used to include the Implementation Plan when an ALI is included or reduced and when one or more aircraft of the fleet have already reached the ALI value:
A2.3.2.1 NEW AIRWORTHINESS LIMITATION INCLUDED FOR
PYLON LINKAGE FITTING Due to the Damage Tolerance Analysis reassessment, some new ALIs were included. So, in order to allow the aircraft operation with this new limitation, the following implementation plan (see Table below) should be used to bridge these new limitations into operators’ maintenance plan.
The instructions herein mentioned, should be used for all operators to bridge a new Airworthiness Limitation Requirement addressed to SSI 54-50-05, located in zones 414/424, into their Maintenance Plan approved by Local Regulatory Authorities.
- SSI 54-50-05 - Zone 414 / 424
- MPG Task Number: 54-50-00-220-808-L00 NOTE A: Accumulated flight cycles since the beginning of the aircraft operation.
NOTE B: If 1st Inspection - FCacc < 400 FC, so 1st Inspection is FCacc + 400 FC.
NOTE C: Inspection Interval from task 54-50-00-220-808-L00.
Accumulated Flight Cycles (FCacc) (Note A) 1st Inspection 2nd Inspection Next Inspections Until 4713 FC 4713 FC (Note B) 9426 FC Repeat interval (Note C) 4713 FC to 6284 FC Next 400 FC 9426 FC Repeat interval (Note C) 6285 FC to 6634 FC 6684 FC 9426 FC Repeat interval (Note C)
PLANNING GUIDE
LEGACY BJ - MAINTENANCE MPG-1483 TR 8-2 Dec 05/12 3 of 4 mpg1483 From:
A2.3.2 INSPECTION INTERVAL LIMIT To:
A2.3.3 INSPECTION INTERVAL LIMIT
PLANNING GUIDE
LEGACY BJ - MAINTENANCE MPG-1483 TR 8-2 Dec 05/12 4 of 4 mpg1483 MPG - TEMPORARY REVISION No. 8-2 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 0145-054-00015-2012 revision B (ANAC) and revision A (FAA/EASA) to incorporate technical changes.
FILING INSTRUCTIONS: Insert this in Appendix 2 - AIRWORTHINESS LIMITATION REQUIREMENTS, facing on page A2-34.
On page A2-34, include the ALI items below:
SSI ZONE TYPE SIDE TASK EFFECT Pre-Mod SB 145LEG-00-0007 Pos-Mod SB 145LEG-00-0007 Fatigue Threshold Limit (Flight Cycles) Inspection Interval Limit (Flight Cycles) Threshold Interval Limit (Flight Cycles) Inspection Interval Limit (Flight Cycles) 54-50-05 414/424 DET INT 54-50-00-220-808-L00 L600 - 4713 - 4713 54-50-05 414/424 DET INT 54-50-00-220-809-L00 L600 10000 1130 10000 1130 54-50-05 414/424 DET INT 54-50-00-220-808-L00 L650 - - - 4713 54-50-05 414/424 DET INT 54-50-00-220-809-L00 L650 - - 10000 1130