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Rechtsbehelfsbelehrung:
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zur Niederschrift beim Luftfahrt-Bundesamt, Hermann-Blenk-Str. 26, 38108 Braunschweig einzulegen.
LTAs werden auch im Internet unter http://www.lba.de publiziert
* * *
AIRWORTHINESS DIRECTIVE
No F-2005-197
Distribution:
B
Issue date:
December 07, 2005
Page :
1/2
This Airworthiness Directive is published by the DGAC on behalf of
EASA, Airworthiness Authority of the State of Design for the affected
product, part or appliance.
Translation of « Consigne de Navigabilité » of same
number.
In case of difficulty, reference should be made to
the French issue.
Direction
générale
de
l’aviation
civile
France
GSAC
publication
No person may operate an aircraft to which an Airworthiness Directive applies,
except in accordance with the requirements of that Airworthiness Directive,
unless otherwise agreed with the Authority of the State of Registry.
Corresponding foreign Airworthiness Directive(s):
Not applicable
Airworthiness Directive(s) replaced:
None
Person in charge of airworthiness:
AIRBUS SAS
Type certificate(s) No. 72
TCDS No 145
Type(s):
A310 aircraft
ATA chapter:
28
Subject:
Transfer control system - Centre tank - Modification to the non-return
valve
1. EFFECTIVITY:
AIRBUS A310 aircraft, A310-304, A310-308, A310-324 and A310-325 models, all serial numbers, fitted
with one or more auxiliary centre tanks (ACT) or provisioned to receive ACT’s on which AIRBUS Service
Bulletin A310-28-2158 has not been embodied
Note: A310-300 Aircraft series MSN 0636 up to MSN 0706 inclusive, on which AIRBUS modification
No. 8928 has been embodied in production, are not concerned by this Airworthiness Directive (AD).
2. REASONS:
An operator has reported that, during flight, it was not possible to transfer fuel from ACT’s 1 and 2.
No ECAM warnings were triggered.
The investigation of the problem revealed that the static inverter 4XE was faulty and the fuse 3XE was
blown. This could result in the loss of the Fuelling bus Bars 900PP and 901PP leading to failure of the
automatic ACT fuel transfer.
These failures, if combined with a failure of the ACT transfer non return valve (NRV) (PN C23AE0102, FIN
280285 in the Center tank) to close, could result in an unsafe condition by preventing manual ACT fuel
transfer.
The aim of this AD is to mandate the replacement of the existing ACT transfer NRV in the center tank
position with the NRV PN C23AE0103 to improve fuel system reliability.
3. MANDATORY ACTIONS AND COMPLIANCE TIMES:
Within 15,000 flight hours at the latest from the effective date of this AD:
- remove the NRV PN C23AE0102 and replace it by a NRV PN C23AE0103 in accordance with the
instructions of AIRBUS Service Bulletin A310-28-2158.
n/GH
AIRWORTHINESS DIRECTIVE
No F-2005-197
Distribution:
B
Issue date:
December 07, 2005
Page:
2/2
4. REFERENCE PUBLICATION:
AIRBUS Service Bulletin A310-28-2158 original issue
Any later approved revision of this SB is acceptable.
5. EFFECTIVE DATE:
December 17, 2005.
6. REMARK:
For questions concerning the technical content of this AD’s requirements, contact:
AIRBUS SAS - EAW - Office of Airworthiness - Fax: 33 5 61 93 45 80.
7. APPROVAL:
This AD is approved under EASA reference No 2005-6417 dated November 29, 2005.
COPY nr.
MINISTÉRIO DAS OBRAS PÚBLICAS, TRANSPORTES E COMUNICAÇÕES
GABINETE DE PREVENÇÃO E INVESTIGAÇÃO DE ACIDENTES COM AERONAVES
GPIAA
FINAL INCIDENT INVESTIGATION REPORT
MONARCH AIRWAYS
AIRBUS A321-231
G-OZBE
FARO AIRPORT
14TH JUNE 2004
REPORT NR 16/INCID/2004
Technical Report nr 16/INCID/04
DOWNLOAD COPY Page 2 of 23
FOREWORD
This report expresses the technical conclusions determined by
G.P.I.A.A. Investigation Commission about facts and causes
involved in this occurrence.
According to Annex 13 to the International Civil Aviation
Organization Convention (Chicago 1944), to the Council Directive
nr. 94/56/EC (21st November 1994) and to nr. 3, 11th
article of Decree-Law 318/99 (11th August), it is not the object
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