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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”, APPLICA

AIRCRAFT.

TEMPORARY REVISION No. 8-3 DATED APRIL 08/2013

HIGHLIGHTS

This highlights presents MPG Temporary Revision 8-3.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 8-3 – MPG-1483 dated APRIL 08, 2013.2.Outline of changesAn outline of all changes is presented below.
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SECTION 4 – STRUCTURAL INSPECTION REQUIREMENTSUpdated item 4.10 STRUCTURAL TASKS, as indicated below.APPENDIX 2 – AIRWORTHINESS LIMITATION REQUIREMENTSCreated nine (9) new INSPECTION INTERVAL LIMITS for SSI 53-10-20.

REFERENCE NUMBER DESCRIPTION OF CHANGE

53-12-00-250-805-L00 NEW TASK. New task created.

53-12-00-250-806-L00 NEW TASK. New task created.

53-12-00-250-807-L00 NEW TASK. New task created.

53-12-00-250-808-L00 NEW TASK. New task created.

53-12-00-250-809-L00 NEW TASK. New task created.

53-12-00-250-810-L00 NEW TASK. New task created.
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RECORD OF TEMPORARY REVISIONS

T.R.

No.

DATE

ISSUED

DATE

REMOVED

INCORPORATED

BY

T.R.

No.

DATE

ISSUED

DATE

REMOVED

0-1 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 06/02 Jul 31/03 Revision 2

2-1 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 Jan 22/138-3 Apr 08/13
AGÊNCIA NACIONAL DE AVIAÇÃO CIVIL - ANAC

LEGACY BJ - MPG

(MPG-1483)

TRANSMITTAL LETTER FOR TEMPORARY REVISION No. 8-3

SUBMITTED FOR APPROVAL ON: 08th APRIL 2013

This transmittal letter presents LEGACY BJ - MPG TemporaryRevision 8-3 with the sanction of Agência Nacional de Aviação Civil- ANAC.Reasons:The MPG-1483 revision 8 SECTION 4 - STRUCTURALINSPECTION REQUIREMENTS and APPENDIX 2 -AIRWORTHINESS LIMITATION REQUIREMENTS, is beingrevised based on the DCA 0145-053-00042-2012 revision A toincorporate technical changes.Actions:Please, refer to the highlights of this TR for more details.Insert the pages referred to below as indicated:Page 1, 2 and 3 of 5 – Update on page 4-25.Page 4 and 5 of 5 – Update on page A2-18.

Record the incorporation of the revision oRevisions. Retain this transmittal letter areport.Signed by:

MARIO LEHMERT RENAUDAgência Nacional de Aviação Civil - ANAMRB ChairmanDate: 
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MPG - TEMPORARY REVISION No. 8-3

TO: HOLDERS OF PUBLICATION No. MPG-1483 - "MAINTENANCE PLANNING GUIDE", APPLICABLE TO EMB-1

REASON: The MPG-1483 revision 8 SECTION 4 - STRUCTURAL INSPECTION REQUIREMENTS, is being revised b

053-00042-2012 revision A to incorporate technical changes.

FILING INSTRUCTIONS: Insert this in Section 4 - Structural Inspection Requirements, facing on page 4-25.

On page 4-25:Insert the new tasks 53-12-00-250-805-L00, 53-12-00-250-806-L00, 53-12-250-807-L00, 53-12-250-808-L00, 53-12-253-12-250-810-L00, as indicated below.

REFERENCE NUMBER TYPE DESCRIPTION THRESHOLD INT ZONE E

53-12-00-250-805-L00 SDE Externally inspect the FUSELAGE component by

using Eddy Current Inspection Method:

• Windshield lateral post and its attachment (SSI

53-10-20).

NOTE: Applicable to aircraft Pre-Mod.

S.B.145LEG-00-0007 and Pre-Mod.S.B. 145LEG-53-0030.

7000 FC 10000 FC 223, 224 
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MPG - TEMPORARY REVISION No. 8-3

REFERENCE NUMBER TYPE DESCRIPTION THRESHOLD INT ZONE E

53-12-00-250-806-L00 SDE Externally inspect the FUSELAGE component by

using Eddy Current Inspection Method:

• Windshield lateral post and its attachment

(SSI 53-10-20).NOTE: Applicable to aircraft Post-Mod.S.B.145LEG-00-0007 or with an equivalent modification factory-incorporated and Pre-Mod.S.B.145LEG-53-0030.

6000 FC 6212 FC 223, 224 

53-12-00-250-807-L00 SDE Internally inspect the FUSELAGE component by

using Eddy Current Inspection Method:

• Windshield lateral post and its attachment

(SSI 53-10-20).NOTE: Applicable to aircraft Pre-Mod.S.B.145LEG-00-0007 and Pre-Mod.S.B.145LEG-53-0030.

7000 FC 3151 FC 223, 224 

53-12-00-250-808-L00 SDE Internally Inspect the FUSELAGE component by

using Eddy Current Inspection Method:

• Windshield lateral post and its attachment

(SSI 53-10-20).NOTE: Applicable to aircraft Post-Mod.S.B.145LEG-00-0007 ow with an equivalentmodification factory-incorporated and Pre-Mod.S.B.145LEG-53-0030.

6000 FC 1969 FC 223, 224 
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REFERENCE NUMBER TYPE DESCRIPTION THRESHOLD INT ZONE E

53-12-00-250-809-L00 SDE Externally inspect the FUSELAGE component by

using Eddy Current Inspection Method:

• Windshield lateral post and its attachment

(SSI 53-10-20).NOTE: Applicable to aircraft Pre-Mod.S.B.145LEG-00-0007 and Post-Mod.S.B.145LEG-53-0030 or with an equivalent modification factory-incorporated.

6915 FC 3247 FC 223, 224 

53-12-00-250-810-L00 SDE Externally inspect the FUSELAGE component by

using Eddy Current Inspection Method:

• Windshield lateral post and its attachment

(SSI 53-10-20).NOTE: Applicable to aircraft Post-Mod.

S.B.145LEG-00-0007 or with an equivalentmodification factory-incorporated and PostMod. S.B.145LEG-53-0030 or with n equivalent modification factory-incorporated.

4170 FC 2011 FC 223, 224 
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MPG - TEMPORARY REVISION No. 8-3

TO: HOLDERS OF PUBLICATION No. MPG-1483 - "MAINTENANCE PLANNING GUIDE", APPLICABLE TO EMB-1

REASON: The MPG-1483 revision 8 APPENDIX 2 - AIRWORTHINESS LIMITATION REQUIREMENTS, is being rev

0145-053-00042-2012 revision A to incorporate technical changes.

FILING INSTRUCTIONS: Insert this in Appendix 2 - AIRWORTHINESS LIMITATION REQUIREMENTS, facing on pa

On page A2-18, include the ALI items below:

SSI ZONE TYPE SIDE TASK EFFECT

Pre-Mod SB

145LEG-00-0007

1

Fatigue 

Threshold 

Limit 

(Flight Cycles)

Inspection 

Interval Limit

(Flight Cycles)

Thres

Interval 

(Flight C

53-10-20 

PRE-MOD SB 

145LEG-53-0030

223/224 SDE EXT 53-12-00-250-805-L00 L600 7000 10000 - 

53-10-20 

PRE-MOD SB 

145LEG-53-0030

223/224 SDE EXT 53-12-00-250-806-L00 L600 - - 600

53-10-20 

PRE-MOD SB 

145LEG-53-0030

223/224 SDE INT 53-12-00-250-807-L00 L600 7000 3151 - 
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SSI ZONE TYPE SIDE TASK EFFECT

Pre-Mod SB

145LEG-00-0007

1

Fatigue 

Threshold 

Limit 

(Flight Cycles)

Inspection 

Interval Limit

(Flight Cycles)

Thres

Interval 

(Flight C

53-10-20 

PRE-MOD SB 

145LEG-53-0030

223/224 SDE INT 53-12-00-250-808-L00 L600 - - 600

53-10-20 

PRE-MOD SB 

145LEG-53-0030

223/224 SDE EXT 53-12-00-250-806-L00 L650 - - 600

53-10-20 

PRE-MOD SB 

145LEG-53-0030

223/224 SDE INT 53-12-00-250-808-L00 L650 - - 600

53-10-20 

PRE-MOD SB 

145LEG-53-0030

223/224 SDE EXT 53-12-00-250-809-L00 L600 6915 3247 

53-10-20 

PRE-MOD SB 

145LEG-53-0030

223/224 SDE EXT 53-12-00-250-810-L00 L600 - - 417

53-10-20 

PRE-MOD SB 

145LEG-53-0030

223/224 SDE EXT 53-12-00-250-810-L00 L650 - - 417