PLANNING GUIDELEGACY BJ - MAINTENANCEMPG-1483TR 8-2Dec 05/121 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. 8-2 DATED DECEMBER 05/2012HIGHLIGHTSThis 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. ContentsThis issue encompasses Temporary Revision8-2 – MPG-1483 dated December 05, 2012.2.Outline of changesAn outline of all changes is presented below.PLANNING GUIDELEGACY BJ - MAINTENANCEMPG-1483TR 8-2Dec 05/122 of 2

mpg1483SECTION 4 – STRUCTURAL INSPECTION REQUIREMENTSUpdated item 4.10 STRUCTURALTASKS, as indicated below.APPENDIX 2 – AIRWORTHINESS LIMITATION REQUIREMENTSCreated item A2.3.2 - IMPLEMENTATIONOF 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 CHANGE54-50-00-220-808-L00NEW TASK. New task created.54-50-00-220-809-L00NEW TASK. New task created.PLANNING GUIDELEGACY BJ - MAINTENANCEMPG-1483Dec 05/12

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 Nov 12/128-2 Dec 05/12AGÊNCIA NACIONAL DE AVIAÇÃO CIVIL - ANACLEGACY BJ - MPG(MPG-1483)TRANSMITTAL LETTER FOR TEMPORARY REVISION No. 8-2SUBMITTED FOR APPROVALON: 05th DECEMBER 2012This transmittal letter presents LEGACY BJ - MPG TemporaryRevision 8-2 with the sanction ofAgência Nacional de Aviação Civil- ANAC.Reasons:The MPG-1483 revision 8 SECTION 4 - STRUCTURALINSPECTION REQUIREMENTS and APPENDIX 2 -AIRWORTHINESS LIMITATIONREQUIREMENTS, is beingrevised based on the DCA 0145-054-00015-2012 revision B(ANAC) and revision A (FAA/EASA) to incorporate technicalchanges.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 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 8-2Dec 05/121 of 4

mpg1483MPG - TEMPORARY REVISION No. 8-2TO: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-L00and 54-50-00-220-809-L00, as indicated below.REFERENCE NUMBER TYPE DESCRIPTIONTHRESHOLDINT ZONE EFFECT TOLERANCE54-50-00-220-808-L00 DET Internally inspect the PYLON component:•Pylon yokes I and II (SSI 54-50-05) primary element.– 4713 FC 414/424 ALL Not Applicable54-50-00-220-809-L00 DET Internally inspect the PYLON component:•Pylon yokes I and II (SSI 54-50-05) secondaryelement.10000 FC 1130 FC 414/424 ALL Not ApplicablePLANNING GUIDELEGACY BJ - MAINTENANCEMPG-1483TR 8-2Dec 05/122 of 4

mpg1483MPG - TEMPORARY REVISION No. 8-2TO: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 DCA0145-054-00015-2012 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:A2.3.2IMPLEMENTATION OF REVISED AIRWORTHINESSLIMITATIONSThis Section will be used to include the Implementation Plan whenan ALI is included or reduced and when one or more aircraft of thefleet have already reached the ALI value:A2.3.2.1 NEW AIRWORTHINESS LIMITATION INCLUDED FORPYLON LINKAGE FITTINGDue to the Damage Tolerance Analysis reassessment, some newALIs were included. So, in order to allow the aircraft operation withthis new limitation, the followingimplementation plan (see Tablebelow) should be used to bridge these new limitations into operators’maintenance plan.The instructions herein mentioned, should be used for all operatorsto bridge a new Airworthiness Limitation Requirement addressed toSSI 54-50-05, located in zones 414/424, into their Maintenance Planapproved by Local Regulatory Authorities.- SSI 54-50-05 - Zone 414 / 424- MPG Task Number: 54-50-00-220-808-L00NOTEA: Accumulated flight cycles since the beginning of theaircraft operation.NOTEB: If 1st Inspection - FCacc< 400 FC, so 1st Inspection isFCacc + 400 FC.NOTEC: Inspection Interval from task 54-50-00-220-808-L00.AccumulatedFlight Cycles(FCacc) (NoteA)1st Inspection 2nd InspectionNextInspectionsUntil 4713 FC 4713 FC (NoteB)9426 FC Repeat interval(Note C)4713 FC to6284 FCNext 400 FC 9426 FC Repeat interval(Note C)6285 FC to6634 FC6684 FC 9426 FC Repeat interval(Note C)PLANNING GUIDELEGACY BJ - MAINTENANCEMPG-1483TR 8-2Dec 05/123 of 4

mpg1483From:A2.3.2 INSPECTION INTERVAL LIMITTo:A2.3.3 INSPECTION INTERVAL LIMITPLANNING GUIDELEGACY BJ - MAINTENANCEMPG-1483TR 8-2Dec 05/124 of 4

mpg1483MPG - TEMPORARY REVISION No. 8-2TO: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 DCA0145-054-00015-2012 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 EFFECTPre-Mod SB145LEG-00-0007Pos-Mod SB145LEG-00-0007FatigueThresholdLimit(Flight Cycles)InspectionInterval Limit(Flight Cycles)ThresholdInterval Limit(Flight Cycles)InspectionInterval Limit(Flight Cycles)54-50-05 414/424 DET INT 54-50-00-220-808-L00 L600 - 4713 - 471354-50-05 414/424 DET INT 54-50-00-220-809-L00 L600 10000 1130 10000 113054-50-05 414/424 DET INT 54-50-00-220-808-L00 L650 - - - 471354-50-05 414/424 DET INT 54-50-00-220-809-L00 L650 - - 10000 1130