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