|
Number
|
Issued by
|
Issue date
|
Subject
|
Approval Holder / Type Designation
|
Effective date
|
Attachment |
|
G-018-04-85
|
|
1985-04-01
|
IPECO EUROPE - Equipment/Furnishings – Pilot/Co-Pilot Seat – Height adjustment mechanism – inspection of heightlock pins.
|
-
APPLIANCES
-
ATA 25 EQUIPMENT / FURNISHINGS
|
1985-04-01
|
|
|
G-017-04-85
|
|
1985-04-01
|
IPECO EUROPE - Equipment/Furnishings – Pilot/Co-Pilot Seat – Height adjustment mechanism – inspection of heightlock pins.
|
-
APPLIANCES
-
ATA 25 EQUIPMENT / FURNISHINGS
|
1985-04-01
|
|
|
G-016-04-85
|
|
1985-04-01
|
IPECO EUROPE - Equipment/Furnishings – Pilot/Co-Pilot Seat – Height adjustment mechanism – inspection of heightlock pins.
|
-
APPLIANCES
-
ATA 25 EQUIPMENT / FURNISHINGS
|
1985-04-01
|
|
|
G-011-04-85
|
|
1985-04-01
|
Exhaust - Jet pipe - To introduce an inspection to ensure correct installation of the three retaining plate assemblies which secure the jet pipe to the jet pipe manifold.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1985-04-01
|
|
|
G-010-04-85
|
|
1985-04-01
|
Navigation - To re-route electrical wiring to the standby horizon to enable the battery power supply to be independent of gyro isolation.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1985-04-01
|
|
|
G-009-04-85
|
|
1985-04-01
|
Navigation - Introduction of standby horizon normal/emergency switch with associated battery busbar power supply.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1985-04-01
|
|
|
G-013-04-85
|
|
1985-04-01
|
Wings - Reinforcing the bottom skin at landing gear bay cut-out at wing Stn 115.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1985-04-01
|
|
|
G-012-04-85
|
|
1985-04-01
|
Landing gear - Failure of main landing gear door operating rod eye end, door hinge assembly and hinge brackets.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1985-04-01
|
|
|
G-003-04-85
|
|
1985-04-01
|
Fuel - Centre tank - Possibility of fuel leaking into passenger cabin.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1985-04-01
|
|
|
IT-1985-32
|
|
1985-03-13
|
Flap bellcrank support brackets
|
|
1985-03-13
|
|
|
F-1985-037-010
|
|
1985-03-13
|
Locking of rear sidegate
|
|
1985-03-20
|
|
|
F-1985-030-066
|
|
1985-03-06
|
Main landing gear - Retraction actuator
|
|
1985-03-06
|
|
|
G-011-03-85
|
|
1985-03-01
|
DUNLOP - Ice and Rain Protection – Windscreen Wiper Equipment – Inspection and modification of actuating arm at attachment point.
|
-
APPLIANCES
-
ATA 30 ICE & RAIN PROTECTION
|
1985-03-01
|
|
|
G-010-03-85
|
|
1985-03-01
|
DOWTY ROTOL - Landing Gear – Nose undercarriage – Inspection of main fitting.
|
-
APPLIANCES
-
VIKING AIR LTD
|
1985-03-01
|
|
|
G-013-03-85
|
|
1985-03-01
|
Engine - Fuel Control - FFG - Blanking of the P1 vent orifice in the altitude bias sensor.
|
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
|
1985-03-01
|
|
|
G-012-03-85
|
|
1985-03-01
|
Engine - Fuel and Control - Fuel systems air tubes rerun P1 airline incorporating a relief valve and water drain facility with screwed blanking feature.
|
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
|
1985-03-01
|
|
|
G-007-03-85
|
|
1985-03-01
|
Flight Controls - To improve the integrity of mounting of elevator torque tube.
|
|
1985-03-01
|
|
|
G-006-03-85
|
|
1985-03-01
|
Flight Controls - Inspection of complete elevator control circuit.
|
|
1985-03-01
|
|
|
G-005-03-85
|
|
1985-03-01
|
Flight Controls - To improve the integrity of mounting of elevator torque tube.
|
|
1985-03-01
|
|
|
G-004-03-85
|
|
1985-03-01
|
Flying Controls - To introduce re-designed cable guard for aileron servo cables at fuselage Stn 77.75 and fairlead at fuselage Stn 89.15.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1985-03-01
|
|
