|
Number
|
Issued by
|
Issue date
|
Subject
|
Approval Holder / Type Designation
|
Effective date
|
Attachment |
|
SE-1-034
|
|
1989-12-08
|
NACELLE - INSPECTION OF DRAG STRUT BOLTS, LOWER FITTINGS AND ATTACHING FASTENERS
|
|
1989-12-08
|
|
|
US-89-25-10
|
|
1989-12-01
|
Wing Lower Forward Spar Attachment Fittings, Centre Section and Outboard Wing Spar Caps - Inspection / Repair / Replacement
|
-
TEXTRON AVIATION INC.
-
100 (King Air)
-
65 (Queen Air)
-
90 (King Air)
|
1990-01-04
|
|
|
US-89-25-08
|
|
1989-12-01
|
Wing Lower Forward Spar Attachment Fittings, Centre Section and Outboard Wing Spar Caps - Inspection / Repair / Replacement
|
|
1990-01-04
|
|
|
G-004-12-89
|
|
1989-12-01
|
Auto Flight - To introduce a once only inspection to ensure the correct orientation and function of both pitch and roll trim indicators Part No. 20242010-132.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1989-12-01
|
|
|
NL-1989-145
|
|
1989-11-15
|
PASSENGER DOOR HANDLE GEARBOX MODIFICATION
|
|
1989-11-22
|
|
|
IT-1989-272
|
|
1989-11-07
|
Engine - Operating Limitations - Flight Manual Revision
|
-
LEONARDO S.p.A. HELICOPTERS
|
1989-11-07
|
|
|
US-89-03-01R1
|
|
1989-11-06
|
GOODYEAR TIRE & RUBBER COMPANY - Tires - Identification / Removal from Service
|
|
1989-11-13
|
|
|
G-002-11-89
|
|
1989-11-01
|
Flight Controls - To remove the stall warning frame heaters from the essential 28V DC busbars and place them on the non-essential busbars.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1989-11-01
|
|
|
G-007-11-89
|
|
1989-11-01
|
Doors - To provide retention of the shouldered bolt at the upper connection of the passenger/ crew door restraint cable.
|
-
BAE SYSTEMS (OPERATIONS) LTD
-
Jetstream 3100
-
Jetstream 3200
|
1989-11-01
|
|
|
G-001-11-89
|
|
1989-11-01
|
CANCELLED: Flight Controls - Elevator - Inspect elevator control cables between frames 42 and 44 (LH) for possible chafing.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1989-11-01
|
|
|
IT-1989-262
|
|
1989-10-31
|
Aileron Balance Weights Securing System Inspection / Modification
|
|
1989-10-31
|
|
|
F-1989-017-017R2
|
|
1989-10-31
|
Modifications to structure prompted by fatigue test findings
|
|
1989-10-31
|
|
|
US-87-14-01R1
|
|
1989-10-30
|
SUPERSEDED BY FAA AD 2009-24-01
|
|
1989-12-11
|
|
|
NL-1989-130
|
|
1989-10-27
|
EXTERNAL POWER SUPPLY BOX SURROUND STRUCTURE REINFORCEMENT
|
|
1989-11-03
|
|
|
NL-1989-128
|
|
1989-10-27
|
AUTOPILOT & EFIS INTERFACE MODIFICATION
|
|
1989-11-03
|
|
|
D-1989-123-2
|
|
1989-10-25
|
Tandem Hydraulic Units - Valve Body Manifolds
|
-
AIRBUS HELICOPTERS DEUTSCHLAND
|
1989-10-25
|
|
|
F-1989-157-099
|
|
1989-10-18
|
Upper skin and joining part of the tail horizontal surface
|
|
1989-10-18
|
|
|
IT-1989-261
|
|
1989-10-17
|
Main Spar Web Inspection and Reinforcement
|
|
1989-10-17
|
|
|
IT-1989-259
|
|
1989-10-17
|
Main Rotor Drive - Aeroquip 601 hose assemblies - Inspection / Replacement
|
-
LEONARDO S.p.A. HELICOPTERS
|
1989-10-17
|
|
|
IT-1989-258
|
|
1989-10-17
|
Engine Oil - Engine Oil Cooler Inlet Tube Assemblies P/N 269A8327-143 - Inspection / Replacement
|
-
MECAER AVIATION GROUP SpA
|
1989-10-17
|
|