# Technical Disposition Ref.: TD/K4/S1/27583/2009

Issue: E Date: 26 Aug 2009 1 of 25 A/C: MSN: ALL refer RAS last page



## Rudder inspection on external surface
Changes for Issue E: Page 1 and 10 revised; page 2 5 added 

## The external surface of the rudder has to be inspec ted in defined areas for debonding. Inspect the individual Rudder with the ELCH inspect ion method given on page 2 to 4 in the areas as defined in table 1 on pages 8 and 9. This table is sorted by operator and MSN, it define s the required inspection per panel on LH and/or RH side. The letter in the inspection locati on box defines the TD page with the dimensions of the individual inspection area. These dimensions are given on page 11 and subsequent ones.
Rudders which are affected in areas with thicker sk ins need a specific inspection method. The rudders to be inspected with the Vacuum Loss In spection method are listed on page 10. For the final Vacuum Loss Inspection at Locations D and F to N the Inspection Instruction as per Appendix A is required. In case of findings the inspection results have to be reported to Airbus before next flight to get further instructions. If there are no findings report to Airbus within 10 days. For the reporting use the reporting sheet from page s 5 to 7, use one reporting sheet for each inspection area.

Send the inspection report with a referenced mail t o:

AIRTAC (Airbus Technical AOG Center) Customer Services AIRBUS Central Entity Phone: +33 (0)5 61 93 3400 (24 hour) Fax: +33 (0)5 61 93 3500 Mailto: airtac@airbus.com Page: G. Stemmer Approved:

Copyright Airbus S.A.S. 2009. All rights reserved. This document contains Airbus S.A.S. (Societe par A ctions Simplifiee) proprietary information and shal l at all times remain the property of Airbus S.A.S.

. No intellectual property right or license is grante d by Airbus S.A.S. in connection with any informati on contained in it. It shall be treated as confiden tial, shall not be disclosed in whole or in part to any third party and shall not be duplicated in a ny manner, without Airbus S.A.S. prior written cons ent. This Technical Disposition (TD) only covers de sign aspects and excludes workmanship aspects. It has been prepared for a spe cific aircraft or components, based on the original Airbus Type Certificate, and solely on the basis o f the information supplied to Airbus.

This TD is not to be used for any other aircraft or component or any other purposes than for which it was supplied without the written approval of Airbus

.

# Technical Disposition Ref.: TD/K4/S1/27583/2009

Issue: E Date: 26 Aug 2009 2 of 25 A/C: MSN: ALL refer RAS last page



## Job preparation:

WARNING: MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN POSITION BEFORE YOU START A TASK ON OR NEAR THE HORIZONTAL AND VERTICAL STABILIZERS (REFER TO A310 or A300-600 AMM 55-40-00 ).
NOTE: 

## To achieve a full picture of the structural conditi on in the inspection area it is required to check in advance the aircraft documentation for any repairs performed by the operator in that area. If repairs are present in the inspection area document them together with the inspection results on the reporting sheets at page 5 to 7.

- The aircraft must be in a Hangar or Dock providing accessibility to the complete rudder external surface.

- Make sure that the aircraft is electrically grounde d (Refer to A310 or A300-600 

## AMM 24-00-00 PB301).

- Make the horizontal and vertical stabilizer safe (Refer to A310 or A300-600 

## AMM 55-00-00 PB301).

- Conditions and supplies needed for inspection: - Compressed air supply for ELCH test

- Get access to the rudder (if required by a platform or Cherry Picker)

- Get access to the rudder front spar by opening the relevant trailing edge panel, verify and record Rudder S/N and P/N (the identification plate is located on the rudder front spar, see next page). If the actual S/N does not match with the S/N from table 1 (pages 8 and 9) or the identification plate is missing report to Airbus to get new instructions for this rudder.

- Record FC and FH of the rudder.

- Close trailing edge panels. Page:

Copyright Airbus S.A.S. 2009. All rights reserved. This document contains Airbus S.A.S. (Societe par A ctions Simplifiee) proprietary information and shal l at all times remain the property of Airbus S.A.S.

. No intellectual property right or license is grante d by Airbus S.A.S. in connection with any informati on contained in it. It shall be treated as confiden tial, shall not be disclosed in whole or in part to any third party and shall not be duplicated in a ny manner, without Airbus S.A.S. prior written cons ent. This Technical Disposition (TD) only covers de sign aspects and excludes workmanship aspects. It has been prepared for a spe cific aircraft or components, based on the original Airbus Type Certificate, and solely on the basis o f the information supplied to Airbus.

This TD is not to be used for any other aircraft or component or any other purposes than for which it was supplied without the written approval of Airbus

.

# Technical Disposition Ref.: TD/K4/S1/27583/2009

Issue: E Date: 26 Aug 2009 3 of 25 A/C: MSN: ALL refer RAS last page Page:

Copyright Airbus S.A.S. 2009. All rights reserved. This document contains Airbus S.A.S. (Societe par A ctions Simplifiee) proprietary information and shal l at all times remain the property of Airbus S.A.S.

. No intellectual property right or license is grante d by Airbus S.A.S. in connection with any informati on contained in it. It shall be treated as confiden tial, shall not be disclosed in whole or in part to any third party and shall not be duplicated in a ny manner, without Airbus S.A.S. prior written cons ent. This Technical Disposition (TD) only covers de sign aspects and excludes workmanship aspects. It has been prepared for a spe cific aircraft or components, based on the original Airbus Type Certificate, and solely on the basis o f the information supplied to Airbus.

This TD is not to be used for any other aircraft or component or any other purposes than for which it was supplied without the written approval of Airbus

.

# Technical Disposition Ref.: TD/K4/S1/27583/2009

Issue: E Date: 26 Aug 2009 4 of 25 A/C: MSN: ALL refer RAS last page



## Perform the Inspe c tion as follows: Inspect the external surface by the methods:

 Mark and clean the inspection Area (with Solvent Ge neral Purpose (Mat No. 11-026) and lint free Cotton Cloth (Mat. No. 19-003)).
 Perform ELCH Inspection as per NTM 51-10-26 Part 7. For Locations D, E, F, H, L, N and P: Apply the ins pection grid and maintain a distance to any edge or fastener as per sketch at the bottom of this page. For Locations B, C, C2, G, J, K and M: Apply an ins pection grid of 75x75mm and maintain a distance to any edge or fastener of 75mm

. For calibration use only Method 1 and apply the thr eshold values for: the area between trailing edge screws and trailing edge: (1) Yellow value: 0.3mm and (2) Red value: 0.4mm all other areas: (1) Yellow value: 0.25mm and (2) Red value: 0.35mm

 In case of findings determine the complete debonded area even if it extends outside the defined inspection area.
 In case of findings re-examine by tap test from out side as per NTM 51-10-19 Part 5 whether an outer or inner skin disbond is present.
 Document the inspection results using the reporting sheets on pages 5 to 7. In case of findings mark the inspection results wit h dimensions on the rudder surface and document by a photo and if operator performed r epairs are present in the inspection area include these in the damage report with r elevant dimensions. Job close up:

- Make sure that the work areas are clean and clear o f tools and other items of equipment.

- Remove the control safety locks and warning notices , as necessary.

- 

## Put the horizontal and vertical stabilizers back to operating condition (Refer to A310 or A300-600 AMM 55-00-00 PB301).

- 

## Remove the access platforms, if used. Inspection grid for ELCH inspection Page:

Copyright Airbus S.A.S. 2009. All rights reserved. This document contains Airbus S.A.S. (Societe par A ctions Simplifiee) proprietary information and shal l at all times remain the property of Airbus S.A.S.

. No intellectual property right or license is grante d by Airbus S.A.S. in connection with any informati on contained in it. It shall be treated as confiden tial, shall not be disclosed in whole or in part to any third party and shall not be duplicated in a ny manner, without Airbus S.A.S. prior written cons ent. This Technical Disposition (TD) only covers de sign aspects and excludes workmanship aspects. It has been prepared for a spe cific aircraft or components, based on the original Airbus Type Certificate, and solely on the basis o f the information supplied to Airbus.

This TD is not to be used for any other aircraft or component or any other purposes than for which it was supplied without the written approval of Airbus

.

# Technical Disposition Ref.: TD/K4/S1/27583/2009

Issue: E Date: 26 Aug 2009 5 of 25 A/C: MSN: ALL refer RAS last page



## Inspection Report



# Rudder Surface Inspection as per TD in area:

Aircraft type: Inspection date: MSN: Operator: Rudder S/N: FC: Rudder P/N: FH:

Inspection method ELCH Inspection No findings Findings as detailed (loc ation, size and inner or outer skin) by sketch* and photos

No repairs Operator performed repairs

as per sketch* and photos

* use the sketches from next pages Page:

Copyright Airbus S.A.S. 2009. All rights reserved. This document contains Airbus S.A.S. (Societe par A ctions Simplifiee) proprietary information and shal l at all times remain the property of Airbus S.A.S.

. No intellectual property right or license is grante d by Airbus S.A.S. in connection with any informati on contained in it. It shall be treated as confiden tial, shall not be disclosed in whole or in part to any third party and shall not be duplicated in a ny manner, without Airbus S.A.S. prior written cons ent. This Technical Disposition (TD) only covers de sign aspects and excludes workmanship aspects. It has been prepared for a spe cific aircraft or components, based on the original Airbus Type Certificate, and solely on the basis o f the information supplied to Airbus.

This TD is not to be used for any other aircraft or component or any other purposes than for which it was supplied without the written approval of Airbus

.

# Technical Disposition Ref.: TD/K4/S1/27583/2009

Issue: E Date: 26 Aug 2009 6 of 25 A/C: MSN: ALL refer RAS last page



## Inspection Report

for rudders with S/N in the HF-1xxx range Page:

Copyright Airbus S.A.S. 2009. All rights reserved. This document contains Airbus S.A.S. (Societe par A ctions Simplifiee) proprietary information and shal l at all times remain the property of Airbus S.A.S.

. No intellectual property right or license is grante d by Airbus S.A.S. in connection with any informati on contained in it. It shall be treated as confiden tial, shall not be disclosed in whole or in part to any third party and shall not be duplicated in a ny manner, without Airbus S.A.S. prior written cons ent. This Technical Disposition (TD) only covers de sign aspects and excludes workmanship aspects. It has been prepared for a spe cific aircraft or components, based on the original Airbus Type Certificate, and solely on the basis o f the information supplied to Airbus.

This TD is not to be used for any other aircraft or component or any other purposes than for which it was supplied without the written approval of Airbus

.

# Technical Disposition Ref.: TD/K4/S1/27583/2009

Issue: E Date: 26 Aug 2009 7 of 25 A/C: MSN: ALL refer RAS last page



## Inspection Report

for rudders with S/N in the TS-2xxx range Page:

Copyright Airbus S.A.S. 2009. All rights reserved. This document contains Airbus S.A.S. (Societe par A ctions Simplifiee) proprietary information and shal l at all times remain the property of Airbus S.A.S.

. No intellectual property right or license is grante d by Airbus S.A.S. in connection with any informati on contained in it. It shall be treated as confiden tial, shall not be disclosed in whole or in part to any third party and shall not be duplicated in a ny manner, without Airbus S.A.S. prior written cons ent. This Technical Disposition (TD) only covers de sign aspects and excludes workmanship aspects. It has been prepared for a spe cific aircraft or components, based on the original Airbus Type Certificate, and solely on the basis o f the information supplied to Airbus.

This TD is not to be used for any other aircraft or component or any other purposes than for which it was supplied without the written approval of Airbus

.

# Technical Disposition Ref.: TD/K4/S1/27583/2009

Issue: E Date: 26 Aug 2009 8 of 25 A/C: MSN: ALL refer RAS last page



### Table 1

Rudder Serial Number MSN AIRLINETrailingEdgeLowerRibUpperEdgeLeadingEdgeReinforcedareasOtherLocationTrailingEdgeLowerRibUpperEdgeLeadingEdgeReinforcedareasOtherLocation24kg core

HF-1189 470 AAL F X HF-1203 506 AAL D D X TS-2029 695 AIC C TS-2026 743 AMU C C TS-2058 700 BBC C D TS-2009 725 CES D A L TS-2017 732 CES D C2 A TS-2025 741 CES C2 A C TS-2031 746 CES C A TS-2050 763 CES E A TS-2018 733 CSN C2 D A TS-2020 734 CSN C2 A TS-2022 739 CSN C D A TS-2041 750 CSN A TS-2044 756 CSN A C TS-2046 762 CSN C TS-2016 693 DEC D A D A TS-1405 701 DLH K TS-2056 773 DLH D N HF-1064 321 F2I B HF-1017 260 FDX G X HF-1020 313 FDX B HF-1059 355 FDX B HF-1087 369 FDX B H X HF-1061 500 FDX B B TS-2065 702 IYE D A TS-2066 704 IYE C2 HF-1119 419 JAB J X



### The letter in the inspection location box defines t he TD page with the dimensions of the individual inspection area Inspection location LH Inspection location RH Page:

Copyright Airbus S.A.S. 2009. All rights reserved. This document contains Airbus S.A.S. (Societe par A ctions Simplifiee) proprietary information and shal l at all times remain the property of Airbus S.A.S.

. No intellectual property right or license is grante d by Airbus S.A.S. in connection with any informati on contained in it. It shall be treated as confiden tial, shall not be disclosed in whole or in part to any third party and shall not be duplicated in a ny manner, without Airbus S.A.S. prior written cons ent. This Technical Disposition (TD) only covers de sign aspects and excludes workmanship aspects. It has been prepared for a spe cific aircraft or components, based on the original Airbus Type Certificate, and solely on the basis o f the information supplied to Airbus.

This TD is not to be used for any other aircraft or component or any other purposes than for which it was supplied without the written approval of Airbus

.

# Technical Disposition Ref.: TD/K4/S1/27583/2009

Issue: E Date: 26 Aug 2009 9 of 25 A/C: MSN: ALL refer RAS last page



### Table 1 continued

Rudder Serial Number MSN AIRLINETrailingEdgeLowerRibUpperEdgeLeadingEdgeReinforcedareasOtherLocationTrailingEdgeLowerRibUpperEdgeLeadingEdgeReinforcedareasOtherLocation24kg core

TS-2007 724 JAL A TS-2012 729 JAL A TS-2013 730 JAL A A TS-2021 737 JAL A A TS-2024 740 JAL D A TS-2040 753 JAL A TS-2060 770 JAL A TS-2075 783 JAL C TS-2001 719 KAC D TS-2004 722 KAL C TS-2014 731 KAL A A TS-2062 767 MXU C2 A TS-2028 744 OHY C TS-2032 747 OHY E M TS-2035 749 OHY P A C TS-2011 691 PIA E D A A HF-1266 563 TAR B X TS-2076 784 THA C A TS-2079 786 THA D TS-2074 787 THA C C



### The letter in the inspection location box defines t he TD page with the dimensions of the individual inspection area Inspection location LH Inspection location RH Page:

Copyright Airbus S.A.S. 2009. All rights reserved. This document contains Airbus S.A.S. (Societe par A ctions Simplifiee) proprietary information and shal l at all times remain the property of Airbus S.A.S.

. No intellectual property right or license is grante d by Airbus S.A.S. in connection with any informati on contained in it. It shall be treated as confiden tial, shall not be disclosed in whole or in part to any third party and shall not be duplicated in a ny manner, without Airbus S.A.S. prior written cons ent. This Technical Disposition (TD) only covers de sign aspects and excludes workmanship aspects. It has been prepared for a spe cific aircraft or components, based on the original Airbus Type Certificate, and solely on the basis o f the information supplied to Airbus.

This TD is not to be used for any other aircraft or component or any other purposes than for which it was supplied without the written approval of Airbus

.

# Technical Disposition Ref.: TD/K4/S1/27583/2009

Issue: E Date: 26 Aug 2009 10 of 25 A/C: MSN: ALL refer RAS last page



## Specific Inspection at various areas - Location A

Rudder Serial Number MSN AIRLINE Specific Inspection as per:

TS-2009 725 CES TD/K4/S1/27658/2009/D TS-2017 732 CES TD/K4/S1/27659/2009/D TS-2025 741 CES TD/K4/S1/27660/2009/D TS-2031 746 CES TD/K4/S1/27661/2009/D TS-2050 763 CES TD/K4/S1/27662/2009/D TS-2018 733 CSN TD/K4/S1/27668/2009/D TS-2020 734 CSN TD/K4/S1/27669/2009/D TS-2022 739 CSN TD/K4/S1/27671/2009/D TS-2041 750 CSN TD/K4/S1/27674/2009/D TS-2044 756 CSN TD/K4/S1/27675/2009/E TS-2016 693 DEC TD/K4/S1/27680/2009/E TS-2065 702 IYE TD/K4/S1/27731/2009/D TS-2007 724 JAL TD/K4/S1/27601/2009/D TS-2012 729 JAL TD/K4/S1/27665/2009/D TS-2013 730 JAL TD/K4/S1/27666/2009/D TS-2021 737 JAL TD/K4/S1/27670/2009/D TS-2024 740 JAL TD/K4/S1/27672/2009/D TS-2040 753 JAL TD/K4/S1/27673/2009/D TS-2060 770 JAL TD/K4/S1/27677/2009/D TS-2014 731 KAL TD/K4/S1/27667/2009/D TS-2062 767 MXU TD/K4/S1/27664/2009/E TS-2035 749 OHY TD/K4/S1/27663/2009/D TS-2011 691 PIA TD/K4/S1/27679/2009/D TS-2076 784 THA TD/K4/S1/27678/2009/D


## To obtain these documents send a mail to:
Jean-Luc BOITEUX Customer Services AIRBUS Central Entity Phone: + 33 (0)5 61 93 18 69 Fax: + 33 (0)5 61 93 48 28 Mailto:jean-luc.j.boiteux@airbus.com Page:

Copyright Airbus S.A.S. 2009. All rights reserved. This document contains Airbus S.A.S. (Societe par A ctions Simplifiee) proprietary information and shal l at all times remain the property of Airbus S.A.S.

. No intellectual property right or license is grante d by Airbus S.A.S. in connection with any informati on contained in it. It shall be treated as confiden tial, shall not be disclosed in whole or in part to any third party and shall not be duplicated in a ny manner, without Airbus S.A.S. prior written cons ent. This Technical Disposition (TD) only covers de sign aspects and excludes workmanship aspects. It has been prepared for a spe cific aircraft or components, based on the original Airbus Type Certificate, and solely on the basis o f the information supplied to Airbus.

This TD is not to be used for any other aircraft or component or any other purposes than for which it was supplied without the written approval of Airbus

.

# Technical Disposition Ref.: TD/K4/S1/27583/2009

Issue: E Date: 26 Aug 2009 11 of 25 A/C: MSN: ALL refer RAS last page



## Dimensions of Inspection area Trailing Edge – Locat ion B

LH shown, RH symmetrical Page:

Copyright Airbus S.A.S. 2009. All rights reserved. This document contains Airbus S.A.S. (Societe par A ctions Simplifiee) proprietary information and shal l at all times remain the property of Airbus S.A.S.

. No intellectual property right or license is grante d by Airbus S.A.S. in connection with any informati on contained in it. It shall be treated as confiden tial, shall not be disclosed in whole or in part to any third party and shall not be duplicated in a ny manner, without Airbus S.A.S. prior written cons ent. This Technical Disposition (TD) only covers de sign aspects and excludes workmanship aspects. It has been prepared for a spe cific aircraft or components, based on the original Airbus Type Certificate, and solely on the basis o f the information supplied to Airbus.

This TD is not to be used for any other aircraft or component or any other purposes than for which it was supplied without the written approval of Airbus

.

# Technical Disposition Ref.: TD/K4/S1/27583/2009

Issue: E Date: 26 Aug 2009 12 of 25 A/C: MSN: ALL refer RAS last page



## Dimensions of Inspection area Trailing Edge – Locat ion C

LH shown, RH symmetrical Page:

Copyright Airbus S.A.S. 2009. All rights reserved. This document contains Airbus S.A.S. (Societe par A ctions Simplifiee) proprietary information and shal l at all times remain the property of Airbus S.A.S.

. No intellectual property right or license is grante d by Airbus S.A.S. in connection with any informati on contained in it. It shall be treated as confiden tial, shall not be disclosed in whole or in part to any third party and shall not be duplicated in a ny manner, without Airbus S.A.S. prior written cons ent. This Technical Disposition (TD) only covers de sign aspects and excludes workmanship aspects. It has been prepared for a spe cific aircraft or components, based on the original Airbus Type Certificate, and solely on the basis o f the information supplied to Airbus.

This TD is not to be used for any other aircraft or component or any other purposes than for which it was supplied without the written approval of Airbus

.

# Technical Disposition Ref.: TD/K4/S1/27583/2009

Issue: E Date: 26 Aug 2009 13 of 25 A/C: MSN: ALL refer RAS last page



## Dimensions of Inspection area Trailing Edge – Locat ion C2

LH shown, RH symmetrical Page:

Copyright Airbus S.A.S. 2009. All rights reserved. This document contains Airbus S.A.S. (Societe par A ctions Simplifiee) proprietary information and shal l at all times remain the property of Airbus S.A.S.

. No intellectual property right or license is grante d by Airbus S.A.S. in connection with any informati on contained in it. It shall be treated as confiden tial, shall not be disclosed in whole or in part to any third party and shall not be duplicated in a ny manner, without Airbus S.A.S. prior written cons ent. This Technical Disposition (TD) only covers de sign aspects and excludes workmanship aspects. It has been prepared for a spe cific aircraft or components, based on the original Airbus Type Certificate, and solely on the basis o f the information supplied to Airbus.

This TD is not to be used for any other aircraft or component or any other purposes than for which it was supplied without the written approval of Airbus

.

# Technical Disposition Ref.: TD/K4/S1/27583/2009

Issue: E Date: 26 Aug 2009 14 of 25 A/C: MSN: ALL refer RAS last page



## Dimensions of Inspection area Lower Rib – Location D

LH shown, RH symmetrical Page:

Copyright Airbus S.A.S. 2009. All rights reserved. This document contains Airbus S.A.S. (Societe par A ctions Simplifiee) proprietary information and shal l at all times remain the property of Airbus S.A.S.

. No intellectual property right or license is grante d by Airbus S.A.S. in connection with any informati on contained in it. It shall be treated as confiden tial, shall not be disclosed in whole or in part to any third party and shall not be duplicated in a ny manner, without Airbus S.A.S. prior written cons ent. This Technical Disposition (TD) only covers de sign aspects and excludes workmanship aspects. It has been prepared for a spe cific aircraft or components, based on the original Airbus Type Certificate, and solely on the basis o f the information supplied to Airbus.

This TD is not to be used for any other aircraft or component or any other purposes than for which it was supplied without the written approval of Airbus

.

# Technical Disposition Ref.: TD/K4/S1/27583/2009

Issue: E Date: 26 Aug 2009 15 of 25 A/C: MSN: ALL refer RAS last page



## Dimensions of Inspection area Trailing Edge – Locat ion E

LH shown, RH symmetrical Page:

Copyright Airbus S.A.S. 2009. All rights reserved. This document contains Airbus S.A.S. (Societe par A ctions Simplifiee) proprietary information and shal l at all times remain the property of Airbus S.A.S.

. No intellectual property right or license is grante d by Airbus S.A.S. in connection with any informati on contained in it. It shall be treated as confiden tial, shall not be disclosed in whole or in part to any third party and shall not be duplicated in a ny manner, without Airbus S.A.S. prior written cons ent. This Technical Disposition (TD) only covers de sign aspects and excludes workmanship aspects. It has been prepared for a spe cific aircraft or components, based on the original Airbus Type Certificate, and solely on the basis o f the information supplied to Airbus.

This TD is not to be used for any other aircraft or component or any other purposes than for which it was supplied without the written approval of Airbus

.

# Technical Disposition Ref.: TD/K4/S1/27583/2009

Issue: E Date: 26 Aug 2009 16 of 25 A/C: MSN: ALL refer RAS last page



## Dimensions of Inspection area Leading Edge – Locati on F

LH shown, RH symmetrical Page:

Copyright Airbus S.A.S. 2009. All rights reserved. This document contains Airbus S.A.S. (Societe par A ctions Simplifiee) proprietary information and shal l at all times remain the property of Airbus S.A.S.

. No intellectual property right or license is grante d by Airbus S.A.S. in connection with any informati on contained in it. It shall be treated as confiden tial, shall not be disclosed in whole or in part to any third party and shall not be duplicated in a ny manner, without Airbus S.A.S. prior written cons ent. This Technical Disposition (TD) only covers de sign aspects and excludes workmanship aspects. It has been prepared for a spe cific aircraft or components, based on the original Airbus Type Certificate, and solely on the basis o f the information supplied to Airbus.

This TD is not to be used for any other aircraft or component or any other purposes than for which it was supplied without the written approval of Airbus

.

# Technical Disposition Ref.: TD/K4/S1/27583/2009

Issue: E Date: 26 Aug 2009 17 of 25 A/C: MSN: ALL refer RAS last page



## Dimensions of Inspection area – Location G Only valid for S/N HF-1017 RH panel Page:

Copyright Airbus S.A.S. 2009. All rights reserved. This document contains Airbus S.A.S. (Societe par A ctions Simplifiee) proprietary information and shal l at all times remain the property of Airbus S.A.S.

. No intellectual property right or license is grante d by Airbus S.A.S. in connection with any informati on contained in it. It shall be treated as confiden tial, shall not be disclosed in whole or in part to any third party and shall not be duplicated in a ny manner, without Airbus S.A.S. prior written cons ent. This Technical Disposition (TD) only covers de sign aspects and excludes workmanship aspects. It has been prepared for a spe cific aircraft or components, based on the original Airbus Type Certificate, and solely on the basis o f the information supplied to Airbus.

This TD is not to be used for any other aircraft or component or any other purposes than for which it was supplied without the written approval of Airbus

.

# Technical Disposition Ref.: TD/K4/S1/27583/2009

Issue: E Date: 26 Aug 2009 18 of 25 A/C: MSN: ALL refer RAS last page



## Dimensions of Inspection area – Location H Only valid for S/N HF-1087 RH panel Page:

Copyright Airbus S.A.S. 2009. All rights reserved. This document contains Airbus S.A.S. (Societe par A ctions Simplifiee) proprietary information and shal l at all times remain the property of Airbus S.A.S.

. No intellectual property right or license is grante d by Airbus S.A.S. in connection with any informati on contained in it. It shall be treated as confiden tial, shall not be disclosed in whole or in part to any third party and shall not be duplicated in a ny manner, without Airbus S.A.S. prior written cons ent. This Technical Disposition (TD) only covers de sign aspects and excludes workmanship aspects. It has been prepared for a spe cific aircraft or components, based on the original Airbus Type Certificate, and solely on the basis o f the information supplied to Airbus.

This TD is not to be used for any other aircraft or component or any other purposes than for which it was supplied without the written approval of Airbus

.

# Technical Disposition Ref.: TD/K4/S1/27583/2009

Issue: E Date: 26 Aug 2009 19 of 25 A/C: MSN: ALL refer RAS last page



## Dimensions of Inspection area – Location J Only valid for S/N TS-1119 RH panel Page:

Copyright Airbus S.A.S. 2009. All rights reserved. This document contains Airbus S.A.S. (Societe par A ctions Simplifiee) proprietary information and shal l at all times remain the property of Airbus S.A.S.

. No intellectual property right or license is grante d by Airbus S.A.S. in connection with any informati on contained in it. It shall be treated as confiden tial, shall not be disclosed in whole or in part to any third party and shall not be duplicated in a ny manner, without Airbus S.A.S. prior written cons ent. This Technical Disposition (TD) only covers de sign aspects and excludes workmanship aspects. It has been prepared for a spe cific aircraft or components, based on the original Airbus Type Certificate, and solely on the basis o f the information supplied to Airbus.

This TD is not to be used for any other aircraft or component or any other purposes than for which it was supplied without the written approval of Airbus

.

# Technical Disposition Ref.: TD/K4/S1/27583/2009

Issue: E Date: 26 Aug 2009 20 of 25 A/C: MSN: ALL refer RAS last page



## Dimensions of Inspection area – Location K Only valid for S/N TS-1405 LH panel Page:

Copyright Airbus S.A.S. 2009. All rights reserved. This document contains Airbus S.A.S. (Societe par A ctions Simplifiee) proprietary information and shal l at all times remain the property of Airbus S.A.S.

. No intellectual property right or license is grante d by Airbus S.A.S. in connection with any informati on contained in it. It shall be treated as confiden tial, shall not be disclosed in whole or in part to any third party and shall not be duplicated in a ny manner, without Airbus S.A.S. prior written cons ent. This Technical Disposition (TD) only covers de sign aspects and excludes workmanship aspects. It has been prepared for a spe cific aircraft or components, based on the original Airbus Type Certificate, and solely on the basis o f the information supplied to Airbus.

This TD is not to be used for any other aircraft or component or any other purposes than for which it was supplied without the written approval of Airbus

.

# Technical Disposition Ref.: TD/K4/S1/27583/2009

Issue: E Date: 26 Aug 2009 21 of 25 A/C: MSN: ALL refer RAS last page



## Dimensions of Inspection area – Location L Only valid for S/N TS-2009 RH panel Page:

Copyright Airbus S.A.S. 2009. All rights reserved. This document contains Airbus S.A.S. (Societe par A ctions Simplifiee) proprietary information and shal l at all times remain the property of Airbus S.A.S.

. No intellectual property right or license is grante d by Airbus S.A.S. in connection with any informati on contained in it. It shall be treated as confiden tial, shall not be disclosed in whole or in part to any third party and shall not be duplicated in a ny manner, without Airbus S.A.S. prior written cons ent. This Technical Disposition (TD) only covers de sign aspects and excludes workmanship aspects. It has been prepared for a spe cific aircraft or components, based on the original Airbus Type Certificate, and solely on the basis o f the information supplied to Airbus.

This TD is not to be used for any other aircraft or component or any other purposes than for which it was supplied without the written approval of Airbus

.

# Technical Disposition Ref.: TD/K4/S1/27583/2009

Issue: E Date: 26 Aug 2009 22 of 25 A/C: MSN: ALL refer RAS last page



## Dimensions of Inspection area – Location M Only valid for S/N TS-2032 RH panel Page:

Copyright Airbus S.A.S. 2009. All rights reserved. This document contains Airbus S.A.S. (Societe par A ctions Simplifiee) proprietary information and shal l at all times remain the property of Airbus S.A.S.

. No intellectual property right or license is grante d by Airbus S.A.S. in connection with any informati on contained in it. It shall be treated as confiden tial, shall not be disclosed in whole or in part to any third party and shall not be duplicated in a ny manner, without Airbus S.A.S. prior written cons ent. This Technical Disposition (TD) only covers de sign aspects and excludes workmanship aspects. It has been prepared for a spe cific aircraft or components, based on the original Airbus Type Certificate, and solely on the basis o f the information supplied to Airbus.

This TD is not to be used for any other aircraft or component or any other purposes than for which it was supplied without the written approval of Airbus

.

# Technical Disposition Ref.: TD/K4/S1/27583/2009

Issue: E Date: 26 Aug 2009 23 of 25 A/C: MSN: ALL refer RAS last page



## Dimensions of Inspection area – Location N Only valid for S/N TS-2056 LH panel Page:

Copyright Airbus S.A.S. 2009. All rights reserved. This document contains Airbus S.A.S. (Societe par A ctions Simplifiee) proprietary information and shal l at all times remain the property of Airbus S.A.S.

. No intellectual property right or license is grante d by Airbus S.A.S. in connection with any informati on contained in it. It shall be treated as confiden tial, shall not be disclosed in whole or in part to any third party and shall not be duplicated in a ny manner, without Airbus S.A.S. prior written cons ent. This Technical Disposition (TD) only covers de sign aspects and excludes workmanship aspects. It has been prepared for a spe cific aircraft or components, based on the original Airbus Type Certificate, and solely on the basis o f the information supplied to Airbus.

This TD is not to be used for any other aircraft or component or any other purposes than for which it was supplied without the written approval of Airbus

.

# Technical Disposition Ref.: TD/K4/S1/27583/2009

Issue: E Date: 26 Aug 2009 24 of 25 A/C: MSN: ALL refer RAS last page



## Dimensions of Inspection area – Location P Only valid for S/N TS-2035 LH panel Page:

Copyright Airbus S.A.S. 2009. All rights reserved. This document contains Airbus S.A.S. (Societe par A ctions Simplifiee) proprietary information and shal l at all times remain the property of Airbus S.A.S.

. No intellectual property right or license is grante d by Airbus S.A.S. in connection with any informati on contained in it. It shall be treated as confiden tial, shall not be disclosed in whole or in part to any third party and shall not be duplicated in a ny manner, without Airbus S.A.S. prior written cons ent. This Technical Disposition (TD) only covers de sign aspects and excludes workmanship aspects. It has been prepared for a spe cific aircraft or components, based on the original Airbus Type Certificate, and solely on the basis o f the information supplied to Airbus.

This TD is not to be used for any other aircraft or component or any other purposes than for which it was supplied without the written approval of Airbus

.

# Technical Disposition Ref.: TD/K4/S1/27583/2009

Issue: E Date: 26 Aug 2009 25 of 25 A/C: MSN: ALL refer RAS last page



## Appendix A

Final Vacuum Loss Inspection at Locations D and F t o N

Rudder S/N MSN AIRLINE Final Inspection as per: HF-1189 470 AAL TD/K4/S1/28535/2009/A HF-1203 506 AAL TD/K4/S1/28536/2009/A TS-2058 700 BBC TD/K4/S1/28475/2009/B TS-2009 725 CES TD/K4/S1/28531/2009/A TS-2017 732 CES TD/K4/S1/28540/2009/A TS-2018 733 CSN TD/K4/S1/28542/2009/A TS-2022 739 CSN TD/K4/S1/28545/2009/A TS-2016 693 DEC TD/K4/S1/28538/2009/A TS-1405 701 DLH TD/K4/S1/28560/2009/A TS-2056 773 DLH TD/K4/S1/28563/2009/A HF-1017 260 FDX TD/K4/S1/28559/2009/B TS-2065 702 IYE TD/K4/S1/28519/2009/A HF-1119 419 JAB TD/K4/S1/28567/2009/A TS-2024 740 JAL TD/K4/S1/28267/2009/C TS-2001 719 KAC TD/K4/S1/28524/2009/A TS-2032 747 OHY TD/K4/S1/28571/2009/A TS-2011 691 PIA TD/K4/S1/28537/2009/A TS-2079 786 THA TD/K4/S1/28429/2009/A



## To obtain these documents send a mail to:
Jean-Luc BOITEUX Customer Services AIRBUS Central Entity Phone: + 33 (0)5 61 93 18 69 Fax: + 33 (0)5 61 93 48 28 Mailto:jean-luc.j.boiteux@airbus.com Page:

Copyright Airbus S.A.S. 2009. All rights reserved. This document contains Airbus S.A.S. (Societe par A ctions Simplifiee) proprietary information and shal l at all times remain the property of Airbus S.A.S.

. No intellectual property right or license is grante d by Airbus S.A.S. in connection with any informati on contained in it. It shall be treated as confiden tial, shall not be disclosed in whole or in part to any third party and shall not be duplicated in a ny manner, without Airbus S.A.S. prior written cons ent. This Technical Disposition (TD) only covers de sign aspects and excludes workmanship aspects. It has been prepared for a spe cific aircraft or components, based on the original Airbus Type Certificate, and solely on the basis o f the information supplied to Airbus.

This TD is not to be used for any other aircraft or component or any other purposes than for which it was supplied without the written approval of Airbus

.