|
Number
|
Issued by
|
Issue date
|
Subject
|
Approval Holder / Type Designation
|
Effective date
|
Attachment |
|
D-1998-105
|
|
1998-01-30
|
Engine Controls - Lubrication of Power and Condition Control cables
|
|
1998-01-30
|
|
|
D-1998-046
|
|
1998-01-29
|
Flight Controls - Relief Restrictor Valve - Replacement
|
|
1998-01-29
|
|
|
D-1998-042
|
|
1998-01-29
|
Flight Controls - Exchange of roll-spoiler control rod
|
|
1998-01-29
|
|
|
US-98-02-08
|
|
1998-01-28
|
Engine - Crankshaft - Inspection
|
-
LYCOMING ENGINES
-
AEIO-320
-
AEIO-360
-
AIO-320
-
AIO-360
-
IO-320
-
IO-360
-
LIO-320
-
LIO-360
-
LO-360
-
LTO-360
-
O-320
-
O-360
-
TIO-360
-
TO-360
|
1998-03-30
|
|
|
F-1998-021
|
|
1998-01-28
|
SUPERSEDED BY DGAC FRANCE AD 1999-508
|
|
1998-02-07
|
|
|
F-1998-020-005
|
|
1998-01-28
|
Fuel transfer
|
|
1998-02-07
|
|
|
F-1998-029
|
|
1998-01-28
|
Wings – Front and Rear Spar Lower Boom at Rib 9 – Inspection
|
|
1998-02-07
|
|
|
F-1998-028-242
|
|
1998-01-28
|
SUPERSEDED BY EASA AD 2021-0288
|
|
1998-02-07
|
|
|
F-1997-063-214R1
|
|
1998-01-24
|
Fuselage - Forward canted frames
|
|
1998-01-24
|
|
|
G-009-01-98
|
|
1998-01-16
|
Engine - Combustion section - Improved phase 2 combustion liner with strengthened head and improved heatshields.
|
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
|
1998-01-16
|
|
|
D-1998-020
|
|
1998-01-15
|
Wings - Inspection of outer wing for fuel leakage
|
|
1998-01-15
|
|
|
D-1997-321-2
|
|
1998-01-15
|
Flight Controls - Inspection of double shuttle valve
|
|
1998-01-15
|
|
|
F-1996-135R1
|
|
1998-01-14
|
Fuselage - Aft Door Frames - Stress corrosion
|
-
AIRBUS S.A.S.
-
A300
-
A300-600
-
A300-600ST (Beluga)
-
A310
|
1998-01-24
|
|
|
SE-1-121
|
|
1998-01-09
|
Ice and Rain Protection - Prop De-Ice Harness-Inspection on Chafing on Electrical Harness and Hydraulic Pipe
|
|
1998-01-09
|
|
|
G-006-01-98
|
|
1998-01-01
|
Mainplanes – To introduce new nuts at the wing to fuselage main-spar attachment
|
|
1998-01-01
|
|
|
G-005-01-98
|
|
1998-01-01
|
Fuselage – To introduce inspections at the main-spar. Applicable to all B.121 aircraft.
|
|
1998-01-01
|
|
|
G-008-01-98
|
|
1998-01-01
|
Main Landing Gear - Forward door mechanism - Inspection of the spring strut for looseness of the fork end.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1998-01-01
|
|
|
G-007-01-98
|
|
1998-01-01
|
Ice and Rain Protection - Engine de-icing - Inspection/test of engine nacelles for cable chafing and oil/moisture contamination.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1998-01-01
|
|
|
G-004-01-98
|
|
1998-01-01
|
Windows - Inspection and lubrication of ATP right hand side cockpit sliding window external release handle mechanism.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1998-01-01
|
|
|
F-1997-383-240
|
|
1997-12-27
|
Doubler angle at the fuselage-wing lower surface junction (ATA 53)
|
-
AIRBUS S.A.S.
-
A300-600
-
A300-600ST (Beluga)
|
1997-12-27
|
|