PLANNING GUIDELEGACY BJ - MAINTENANCEMPG-1483TR 8-1Oct 26/121 of 2

mpg1483EMBRAER S.A.AV. BRIGADEIRO FARIA LIMA, 2.170 - CAIXAPOSTAL 8050 - TELEFONE (55) 12 3927-7517FAX (55) 12 3927-7546 CEP. 12.227-901 - SÃOJOSÉ DOS CAMPOS - SÃO PAULO - BRASILe-mail: distrib@embraer.com.br - http://www.embraer.comTO:HOLDERS OF PUBLICATION No. MPG-1483 - “MAINTENANCE PLANNING GUIDE”, APPLICABLE TO EMB-135BJAIRCRAFT.TEMPORARY REVISION No. 8-1 DATED OCTOBER 26/2012HIGHLIGHTSThis 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. ContentsThis issue encompasses Temporary Revision 8-1 – MPG-1483 dated October 26, 2012.2.Outline of changesAn outline of all changes is presented below.PLANNING GUIDELEGACY BJ - MAINTENANCEMPG-1483TR 8-1Oct 26/122 of 2

mpg1483SECTION 3 – SYSTEMS & POWERPLANT INSPECTION REQUIREMENTSUpdated item 3.11 SYSTEMS AND POWERPLANT TASKS, as indicated below.APPENDIX 2 – AIRWORTHINESS LIMITATION REQUIREMENTSUpdated 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 CHANGE20-00-00-220-006-A00TASK REVISED. Task description was editorially updated.REFERENCE NUMBER DESCRIPTION OF CHANGE28-50-01-220-001-A02NEW TASK. New task created.28-50-01-720-001-A00NEW TASK. New task created.28-50-08-212-001-A00NEW TASK. New task created.28-50-09-212-001-A00NEW TASK. New task created.28-50-10-212-001-A00NEW TASK. New task created.PLANNING GUIDELEGACY BJ - MAINTENANCEMPG-1483Oct 26/12

mpg1483RECORD OF TEMPORARY REVISIONST.R.No.DATEISSUEDDATEREMOVEDINCORPORATEDBYT.R.No.DATEISSUEDDATEREMOVEDINCORPORATEDBY0-1 Feb 06/02 Nov 26/02 Revision 10-2 May 29/02 Nov 26/02 Revision 10-3 Jun 13/02 Nov 26/02 Revision 10-4 Sep 16/02 Nov 26/02 Revision 11-1 Dec 06/02Jul 31/03Revision 22-1 Sep 16/03 Apr 01/04 Revision 32-2 Nov 21/03 Apr 01/04 Revision 33-1 Jun 24/04 Oct 14/05 Revision 43-2 Sep 03/04 Oct 14/05 Revision 43-3 Oct 19/04 Oct 14/05 Revision 43-4 Jun 22/05 Oct 14/05 Revision 44-1 Dec 20/05 Mar 22/07 Revision 56-1 Oct 02/09 Aug 12/10 Revision 77-1 Oct 13/10 Apr 27/12 Revision 87-2 Feb 22/11 Apr 27/12 Revision 87-3 Feb 24/11 Apr 27/12 Revision 87-4 May 12/11 Apr 27/12 Revision 88-1 Oct 26/12AGÊNCIA NACIONAL DE AVIAÇÃO CIVIL - ANACLEGACY BJ - MPG(MPG-1483)TRANSMITTAL LETTER FOR TEMPORARY REVISION No. 8-1SUBMITTED FOR APPROVALON: 26th OCTOBER 2012This transmittal letter presents LEGACY BJ - MPG TemporaryRevision 8-1 with the sanction ofAgência Nacional de Aviação Civil- ANAC.Reasons:The MPG-1483 revision 8 SECTION 3 - SYSTEMS &POWERPLANT INSPECTION REQUIREMENT is being reviseddue to editorial correction and APPENDIX 2 - AIRWORTHINESSLIMITATION REQUIREMENTS, is being revised based on the DCA0145-028-00020-2011 revision E (FAA/ANAC) and revision D(EASA) to incorporate technical changes due to fuel systemlimitation.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 TemporaryRevisions. Retain this transmittal letter and file it at the front of thereport.Signed by:MARIO LEHMERT RENAUDAgência Nacional de Aviação Civil - ANACMRB ChairmanDate:PLANNING GUIDELEGACY BJ - MAINTENANCEMPG-1483TR 8-1Oct 26/121 of 6

mpg1483MPG - TEMPORARY REVISION No. 8-1TO: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 TOLERANCE20-00-00-220-006-A00 DETInspect (Detailed Inspection) Ventral Fuel Tank -EWIS Components Of Ventral Tank Unit Harness(Zone: 196).NOTE:EWIS48 MOL650 ± 30 DaysREFERENCE NUMBER TYPE DESCRIPTION INT EFFECT TOLERANCE20-00-00-220-006-A00 DETInspect (Detailed Inspection) Ventral Fuel Tank -EWIS Components Of Ventral Tank Unit Harness(Zone: 1972).NOTE:EWIS48 MOL650 ± 30 DaysPLANNING GUIDELEGACY BJ - MAINTENANCEMPG-1483TR 8-1Oct 26/122 of 6

mpg1483MPG - TEMPORARY REVISION No. 8-1TO: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 DCA0145-028-00020-2011 revision E (FAA/ANAC) and revision D (EASA) to incorporate technical changes due to fuel systemlimitation.FILING INSTRUCTIONS:Insert this in Appendix 2 - AirworthinessLimitation Requirements, facing on page A2-66.On page A2-66, update CDCCL item 8, as indicated below.From:To:8) Wires inside the pumpsThe type, length and supporting ofwires used inside the fuel pumps are such that provide enough clearance from any internal surface ofthe pump, what prevents from chafing and arcing. This configuration is a CDCCL item andmust be retained if any maintenance task thatrequires the pump to be disassembled is performed. The pumps CMM provide warnings aboutthe critical configuration of the wiresin thepumps. This is applicablefor all fuel pumps ofall tanks of the aircraft.NOTE:Applicable to aircraft Equipped with Ventral Fuel Tank andAE3007A2 Engines, commercially called Legacy 650 and identifiedin the MPG as L650.8) Wires inside the pumpsThe type, length and supporting ofwires used inside the fuel pumps are such that provide enough clearance from any internal surface ofthe pump, what prevents from chafing and arcing. This configuration is a CDCCL item andmust be retained if any maintenance task thatrequires the pump to be disassembled is performed. The pumps CMM provide warnings aboutthe critical configuration of the wiresin thepumps. This is applicable forall fuel pumps of all tanks of the aircraft,including the pumps equipped with the CHA.NOTE:Applicable to aircraft Equipped with Ventral Fuel Tank andAE3007A2 Engines, commercially called Legacy 650 and identifiedin the MPG as L650.PLANNING GUIDELEGACY BJ - MAINTENANCEMPG-1483TR 8-1Oct 26/123 of 6

mpg1483MPG - TEMPORARY REVISION No. 8-1TO: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 DCA0145-028-00020-2011 revision E (FAA/ANAC) and revision D (EASA) to incorporate technical changes due to fuel systemlimitation.FILING INSTRUCTIONS:Insert this in Appendix 2 - AirworthinessLimitation 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 WallFuel pumps of main wing tanks and auxiliarytanks having PTFE interface fitting, which are installed on the tanks wall. This fitting ishighlighted as CDCCL in the appropriate AMM procedures, to check proper installation, leakproofness, during periodic inspections orwhenever pump is changed.NOTE:Applicable to aircraft Equipped with Ventral Fuel Tank andAE3007A2 Engines, commercially called Legacy 650 and identifiedin the MPG as L650.PLANNING GUIDELEGACY BJ - MAINTENANCEMPG-1483TR 8-1Oct 26/124 of 6

mpg1483MPG - TEMPORARY REVISION No. 8-1TO: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 DCA0145-028-00020-2011 revision E (FAA/ANAC) and revision D (EASA) to incorporate technical changes due to fuel systemlimitation.FILING INSTRUCTIONS:Insert this in Appendix 2 - AirworthinessLimitation Requirements, facing on page A2-71.On page A2-71:Insert the new tasks 28-50-01-220-001-A02 and28-50-01-720-001-A00, as indicated below.REFERENCE NUMBER TYPE DESCRIPTION ZONE INT EFFECT TOLERANCE28-50-01-220-001-A02 DET Inspect (Detailed Inspection) Fuel Pump ElectricalHarness CHA (Cable Harness Assembly) endfitting.NOTE:Applicable to aircraft with fuel pump harness with corrugated conduit.155/156157/197271/272197210,000 FHor 48 MOL650 Not Applicable28-50-01-720-001-A00 FNC Functionally Check Fuel Pump Electrical Harnessfor Leakage.NOTE:Applicable to aircraft with fuel pump harness with corrugated conduit.155/156157/197271/272197220,000 FHor 96 MOL650 Not ApplicablePLANNING GUIDELEGACY BJ - MAINTENANCEMPG-1483TR 8-1Oct 26/125 of 6

mpg1483MPG - TEMPORARY REVISION No. 8-1TO: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 DCA0145-028-00020-2011 revision E (FAA/ANAC) and revision D (EASA) to incorporate technical changes due to fuel systemlimitation.FILING INSTRUCTIONS:Insert this in Appendix 2 - AirworthinessLimitation 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 TOLERANCE28-50-08-212-001-A00 GVI Inspect (GeneralVisual) Ventral Fuel Tank ExternalHarness1972 10,000 FHor 48 MOL650 Not Applicable28-50-09-212-001-A00 GVI Inspect (General Visual) FWD Fuel Tank ExternalHarness191/197 10,000 FHor 48 MOL650 Not Applicable28-50-10-212-001-A00 GVI Inspect (GeneralVisual) Aft Fuel Tank ExternalHarness271/272 10,000 FHor 48 MOL650 Not ApplicablePLANNING GUIDELEGACY BJ - MAINTENANCEMPG-1483TR 8-1Oct 26/126 of 6

mpg1483MPG - TEMPORARY REVISION No. 8-1TO: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 DCA0145-028-00020-2011 revision E (FAA/ANAC) and revision D (EASA) to incorporate technical changes due to fuel systemlimitation.FILING INSTRUCTIONS:Insert this in Appendix 2 - AirworthinessLimitation Requirements, facing on page A2-72.On page A2-72:Delete the statement indicated below:In addition to the Fuel System Limitation requirements, the followinglimitation is being added to EMB-135BJ with Ventral Fuel Tank andAE3007A2 engines installed (Legacy650) under FAA certification:The EMB-135BJ (Legacy 650) shall not be operated pastSeptember 30th, 2013 unlessthe owner or operator hasincorporated a major type design change that complies withprovisions of 14CFR Part 25.981(a)(3), amendment 102 or later.Changes to this limitation can be accomplished by FAA approval ofmajor type design change required in accordance with §21.97.