REFERENCE: TR22 Issue 1.0 AFM ISSUE DATE: 26 NOV 09

A330/A340

TEMPORARY REVISION

TR22 issue 1.0

- TR 4.02.00/40 ISSUE 2 - UNDETECTED

ELEVATOR CONTROL LOSS

IN CASE OF DUAL FAILURE

AIRPLANE FLIGHT MANUAL

The content of this document is the property of Airbus. It is supplied in confidence and commercial

security on its contents must be maintained. It must not be used for any purpose other than that for

which it is supplied, nor may information contained in it be disclosed to unauthorized persons. It must

not be reproduced in whole or in part without permission in writing from the owners of the copyright.

© AIRBUS 2005. All rights reserved.

AIRBUS S.A.S

CUSTOMER SERVICES DIRECTORATE

31707 BLAGNAC CEDEX

FRANCE
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AIRPLANE FLIGHT MANUAL

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APPRO APPROVAL DATA

APPRO-TR TEMPORARY REVISIONS

(TR 4.02.00/40 Issue 2) - Undetected Elevator Control Loss in case of Dual Failure..........................................1/2

ABN ABNORMAL PROCEDURES

ABN-27 FLIGHT CONTROLS

UNDETECTED ELEVATOR CONTROL LOSS IN CASE OF DUAL FAILURE....................................................1/2

ABN-29 HYDRAULIC

UNDETECTED ELEVATOR CONTROL LOSS IN CASE OF DUAL FAILURE....................................................1/2
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AFM 26 NOV 09
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APPROVAL DATA

TEMPORARY REVISIONS

TR22 Issue 1.0 APPRO-TR P 1/2

AFM 26 NOV 09

TR22 Issue 1.0

(TR 4.02.00/40 ISSUE 2) - UNDETECTED ELEVATOR

CONTROL LOSS IN CASE OF DUAL FAILURE

Ident.: TDU / APPRO-TR-00009372.0001001 / 26 NOV 09 EASA APPROVED

Criteria: (340-200 or 340-300) 

Impacted DU: NONE

APPROVAL REFERENCE

APPROVED BY: EASA

Approval date: 26 NOV 09

Approval reference: 10028037

Do not remove this Temporary Revision until instructed to do so.

Reason for issue: This TR is issued in digital format to provide the content of TR 4.02.00/40

Issue 2 approved by the EASA under reference 2004_9191 on September

2nd, 2004.

Applicable to: A340-200 or A340-300 aircraft.

This Temporary Revision is made up of the following Temporary Documentary Units:

APPRO-TR-00009372.0001001/26 NOV 09 ABN-29-00009373.0001001/26 NOV 09

ABN-27-00009371.0001001/26 NOV 09
A330/A340

AIRPLANE FLIGHT MANUAL

APPROVAL DATA

TEMPORARY REVISIONS

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TR22 Issue 1.0 APPRO-TR P 2/2

AFM 26 NOV 09
A330/A340

AIRPLANE FLIGHT MANUAL

ABNORMAL PROCEDURES

FLIGHT CONTROLS

TR22 Issue 1.0 ABN-27 P 1/2

AFM 26 NOV 09

UNDETECTED ELEVATOR CONTROL LOSS IN CASE OF DUAL FAILURE

Ident.: TDU / ABN-27-00009371.0001001 / 26 NOV 09 EASA APPROVED

Criteria: (340-200 or 340-300) 

Impacted DU: NONE

Impacted by TR22 Issue 1.0

On ground, before takeoff until takeoff power thrust setting, apply the following procedure.

 In the case of a F/CTL - PRIM 1 FAULT, or F/CTL - PRIM 1 PITCH FAULT:

Turn off PRIM 1, then back on to perform a FCPC PRIM 1 reset.

 If successful:

Perform the normal pre-flight Flight Control check.

 If unsuccessful:

Return to the gate and require appropriate maintenance actions.

 In the case of a F/CTL - ELEV SERVO FAULT:

Return to the gate and require appropriate maintenance actions.
A330/A340

AIRPLANE FLIGHT MANUAL

ABNORMAL PROCEDURES

FLIGHT CONTROLS

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TR22 Issue 1.0 ABN-27 P 2/2

AFM 26 NOV 09
A330/A340

AIRPLANE FLIGHT MANUAL

ABNORMAL PROCEDURES

HYDRAULIC

TR22 Issue 1.0 ABN-29 P 1/2

AFM 26 NOV 09

UNDETECTED ELEVATOR CONTROL LOSS IN CASE OF DUAL FAILURE

Ident.: TDU / ABN-29-00009373.0001001 / 26 NOV 09 EASA APPROVED

Criteria: (340-200 or 340-300) 

Impacted DU: NONE

Impacted by TR22 Issue 1.0

On ground, before takeoff until takeoff power thrust setting, apply the following procedure.

 In the case of a HYD - G SYS LO PR:

Return to the gate and require appropriate maintenance actions.
A330/A340

AIRPLANE FLIGHT MANUAL

ABNORMAL PROCEDURES

HYDRAULIC

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AFM 26 NOV 09