|
Number
|
Issued by
|
Issue date
|
Subject
|
Approval Holder / Type Designation
|
Effective date
|
Attachment |
|
US-89-06-01
|
|
1989-04-03
|
SWITLIK PARACHUTE COMPANY, INC. - CO2 Inflators - Inspection
|
-
APPLIANCES
-
ATA 25 EQUIPMENT / FURNISHINGS
|
1989-04-03
|
|
|
NL-1989-040
|
|
1989-04-03
|
AUDIO CONNECTION DME1 & DME2 CORRECTION
|
|
1989-04-10
|
|
|
NL-1989-039
|
|
1989-04-03
|
AUTOMATIC FLIGHT-IDLE STOPS RELOCATION
|
|
1989-04-10
|
|
|
NL-1989-017-2
|
|
1989-04-03
|
WING ACCESS PANELS REPLACEMENT
|
|
1989-04-10
|
|
|
G-023-04-89
|
|
1989-04-01
|
Electrical Power - Wiring and clipping - Provision of additional clip position in left aft jet pipe area to prevent generator cable chafing on flap track housing.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1989-04-01
|
|
|
G-024-04-89
|
|
1989-04-01
|
Flight Controls - Flap control system - To introduce flap electronic control unit (ECU) 676801007 (or later interchangeable standard) in lieu of 676801003, 676801005 and 676801006
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1989-04-01
|
|
|
ES-01-89
|
|
1989-04-01
|
Flight Controls - Elevator, Rudder and Aileron Trim Control System - Inspection / Modification
|
-
AIRBUS DEFENCE & SPACE S.A.
|
1989-04-01
|
|
|
F-1989-033-019R1
|
|
1989-03-31
|
Pitch trim
|
|
1989-03-31
|
|
|
NL-1989-037
|
|
1989-03-28
|
FUSELAGE CENTRE SECTION FRAMES REINFORCEMENT
|
|
1989-04-04
|
|
|
F-1989-051
|
|
1989-03-22
|
Brake cylinder
|
|
1989-04-01
|
|
|
F-1988-140R2
|
|
1989-03-22
|
Landing Gear - Main Landing Gear Door Emergency Unlocking Mechanism - Functional Test
|
-
DASSAULT AVIATION
-
Mystère-Falcon 50
-
Mystère-Falcon 900
|
1989-03-22
|
|
|
F-1989-023R1
|
|
1989-03-22
|
CANCELLED: Electrical Power System - ARTUS Transfo-Rectifier - Replacement
|
|
1989-03-22
|
|
|
D-1989-019
|
|
1989-03-21
|
Fuel Supply Fittings - Replacement
|
|
1989-03-21
|
|
|
NL-1989-034
|
|
1989-03-10
|
RUDDER & AILERON FLUTTER DAMPER ASSEMBLIES INSPECTION/MODIFICATION
|
|
1989-03-17
|
|
|
NL-1989-031
|
|
1989-03-03
|
FUSELAGE CENTRE SECTION SKIN REINFORCEMENT
|
|
1989-03-10
|
|
|
G-007-03-89
|
|
1989-03-01
|
Cracks under the bearing sleeve on noseleg downtube.
|
|
1989-03-01
|
|
|
G-008-03-89
|
|
1989-03-01
|
Electrical Power - Introduction of auto transfer from centre busbar to starboard busbar of power supply to No. 2 inverter when undervoltage protection system operates.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1989-03-01
|
|
|
G-023-03-89
|
|
1989-03-01
|
CANCELLED: Navigation - To introduce a once-only inspection of certain ASI pipelines to ensure that swaging has taken place.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1989-03-01
|
|
|
G-006-03-89
|
|
1989-03-01
|
SUPERSEDED BY CAA UK AD 003-07-89
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1989-03-01
|
|
|
G-004-03-89
|
|
1989-03-01
|
CANCELLED: Flight Controls - To introduce peening to control column lower pulley guard bolts.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1989-03-01
|
|
