AIRWORTHINESS DIRECTIVE

 

CAA-AD-2-044/98R1

 

Replaces CAA-AD-2-044/98

 

Date of issue: April 02, 2002

 

AIRCRAFT - FUEL TANK (ATA 28) - INSPECTION

 

Applicability:

- AIRBUS A300 and A300-600 aircraft all certified models and all serial numbers except aircraft on which AIRBUS INDUSTRIE modification 11848 has been embodied in production or AIRBUS INDUSTRIE Service Bulletin (SB) A300-28-0073 or A300-28-6058 in service.

 

- AIRBUS A310 aircraft all certified models and all serial numbers except aircraft on which AIRBUS INDUSTRIE modification 11847 has been embodied in production or SB A310-28-2130 in service.

 

Effective date: May 16, 2002

 

Compliance: Required as indicated in DGAC AD 1998-174-248(B) R1.

 

Remarks: The compliance of this AD must be recorded in Aircraft Logbook, where applicable the requirements of this AD must be integrated into Aircraft Technical Documentation. Address inquiries concerning this AD to: Civil Aviation Authority, Airworthiness Division, Ruzyne Airport, 160 08 Prague 6, Czech Republic, tel.: 420 2 33320922, fax: 420 2 20562270.

 

Ing. Pavel MATOUŠEK

Director of Airworthiness Division

CAA CZ

 

 

DGAC AD No.: 1998-174-248(B) R1

 

AIRBUS

A300, A310 and A300-600 aircraft

Fuel Tanks - Bonding Leads (ATA 28)

 

APPLICABILITY:

 

- AIRBUS A300 and A300-600 aircraft all certified models and all serial numbers except aircraft on which AIRBUS INDUSTRIE modification 11848 has been embodied in production or AIRBUS INDUSTRIE Service Bulletin (SB) A300-28-0073 or A300-28-6058 in service.

 

- AIRBUS A310 aircraft all certified models and all serial numbers except aircraft on which AIRBUS INDUSTRIE modification 11847 has been embodied in production or SB A310-28-2130 in service.

 

REASONS:

 

During a scheduled maintenance check, an inspection of the inner fuel tanks revealed the damage of the bonding leads (corrosion, rupture or degraded electrical contact at the endings) which could be the origin of electrical arcing.

 

The purposes of Revision 1 of this Airworthiness Directive (AD) is:

 

- to cancel the paragraph ACTIONS 1 of the original issue of this AD (preliminary inspection prior to the embodiment of the modification),

 

- to reduce the APPLICABILITY of this AD.

 

ACTIONS:

 

[...]

 

Before March 31, 2003, modify the fuel pipe couplings in accordance with the instructions of the applicable SB A300-28-0073 or A300-28-6058 or A310-28-2130.

 

[...]

 

REF.:

[...]

AIRBUS INDUSTRIE Service Bulletin A300-28-0073

[...]

AIRBUS INDUSTRIE Service Bulletin A300-28-6058

[...]

AIRBUS INDUSTRIE Service Bulletin A310-28-2130

(Any later approved revision of these SB's is acceptable).

 

This Revision 1 replaces original AD 98-174-248(B) dated April 22, 1998.

 

EFFECTIVE DATES:

 

Original AD: MAY 02,1998

Revision 1: MARCH 30, 2002