|
Number
|
Issued by
|
Issue date
|
Subject
|
Approval Holder / Type Designation
|
Effective date
|
Attachment |
|
F-1982-078R5
|
|
1998-04-22
|
SUPERSEDED BY EASA AD 2015-0195
|
|
1998-05-02
|
|
|
F-1998-173
|
|
1998-04-22
|
SUPERSEDED BY EASA AD 2015-0195
|
|
1998-05-02
|
|
|
SE-1-126
|
|
1998-04-20
|
Hydraulic Power-Expansion Chamber Attenuator - New end-piece for IHC Aft ECA
|
|
1998-04-20
|
|
|
F-1998-153-088
|
|
1998-04-18
|
Center landing gear - Gear gland nut
|
|
1998-04-18
|
|
|
F-1998-150-246
|
|
1998-04-18
|
Inspection of aft fuselage section longitudinal joints
|
|
1998-04-18
|
|
|
F-1996-270-209R1
|
|
1998-04-18
|
Engine controls - Replacement of bearing on both throttle control levers
|
-
AIRBUS S.A.S.
-
A300
-
A300-600
-
A300-600ST (Beluga)
-
A310
|
1998-04-18
|
|
|
F-1997-065-055R3
|
|
1998-04-18
|
Override mechanism of trimmable horizontal stabilizer (THS) -Electrical control
|
|
1998-04-18
|
|
|
F-1997-064-044R3
|
|
1998-04-18
|
Override mechanism of trimmable horizontal stabilizer (THS) -Electrical control
|
|
1998-04-18
|
|
|
F-1997-203R1
|
|
1998-04-18
|
Probe Heat Computer Wiring Modification
|
|
1998-04-18
|
|
|
D-1998-217
|
|
1998-04-16
|
Rudder spring tabs - Improper belancing
|
|
1998-04-16
|
|
|
F-1998-152
|
|
1998-04-08
|
Probe Heat Computer Test Procedures
|
|
1998-04-18
|
|
|
IT-1998-126
|
|
1998-04-08
|
Revision of the Limitations Section of the Flight Manual
|
|
1998-05-16
|
|
|
F-1996-245-050R1
|
|
1998-04-08
|
SUPERSEDED BY DGAC FRANCE AD 1999-265-117
|
|
1998-04-08
|
|
|
F-1998-147-075
|
|
1998-04-08
|
External wings - Inner skin surface/rear spar jonction
|
|
1998-04-08
|
|
|
IT-1998-124
|
|
1998-04-07
|
Main Rotor Drive - Gleason Crown of the Main Transmission Assy - Inspection
|
-
LEONARDO S.p.A. HELICOPTERS
|
1998-05-15
|
|
|
SE-1-125
|
|
1998-04-07
|
Landing Gear - Extension and Retraction - Inspection of Relay 15GA and related Socket
|
|
1998-04-07
|
|
|
F-1998-133-087
|
|
1998-04-04
|
Engine fire and overheat detection - Foolproofing connectors
|
|
1998-04-04
|
|
|
G-015-04-98
|
|
1998-04-01
|
SUPERSEDED BY EASA AD 2007-0305
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1998-04-01
|
|
|
G-004-04-98
|
|
1998-04-01
|
Engine - Inspection for I.P. turbine shaft spline wear.
|
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
|
1998-04-01
|
|
|
G-003-04-98
|
|
1998-04-01
|
Engine - Low Pressure Compressor Blades - Inspection / Replacement
|
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
|
1998-04-01
|
|
