|
Number
|
Issued by
|
Issue date
|
Subject
|
Approval Holder / Type Designation
|
Effective date
|
Attachment |
|
G-0069-PRE80
|
|
1980-01-01
|
Flight Controls - Rudder and rudder trim circuits - Introduction of rudder neutral point two degrees to port and restriction of the rudder trim tab movement to starboard.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1980-01-01
|
|
|
G-0068-PRE80
|
|
1980-01-01
|
Engine Controls - Introduction of increased auto feather inhibit rev/min from 11,500 to 12,800 rev/min.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1980-01-01
|
|
|
G-0067-PRE80
|
|
1980-01-01
|
Doors - Emergency exit - To reposition connection to atmosphere for barometric lock.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1980-01-01
|
|
|
G-0066-PRE80
|
|
1980-01-01
|
Oxygen - Contaminated hoses - Replacement of all items downstream of the contaminated hoses.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1980-01-01
|
|
|
G-0065-PRE80
|
|
1980-01-01
|
Flight Controls - Elevator - Introduction of restricting bracket on the elevator control lever
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1980-01-01
|
|
|
G-0064-PRE80
|
|
1980-01-01
|
Instruments - Introduction of a turn and slip indicator on second pilot's instrument panel.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1980-01-01
|
|
|
G-0063-PRE80
|
|
1980-01-01
|
Instruments - Introduction of a turn and slip indicator on second pilot's instrument panel.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1980-01-01
|
|
|
G-0062-PRE80
|
|
1980-01-01
|
Wings - Introduction of glass fibre fence to replace light alloy fence located in the bottom of each wing.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1980-01-01
|
|
|
G-0061-PRE80
|
|
1980-01-01
|
Landing Gear - Inspection and rectification of emergency landing gear system.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1980-01-01
|
|
|
G-0060-PRE80
|
|
1980-01-01
|
Fuselage - Introduction of reinforcing plates around navigators window.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1980-01-01
|
|
|
G-0059-PRE80
|
|
1980-01-01
|
Fuselage - Inspection and modification to Former 18F.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1980-01-01
|
|
|
G-0058-PRE80
|
|
1980-01-01
|
Stabilizers - Introduction of extra rivets in tailplane construction joint.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1980-01-01
|
|
|
G-0057-PRE80
|
|
1980-01-01
|
Stabilizers - Introduction of re-designed tailplane construction joint plates.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1980-01-01
|
|
|
G-0056-PRE80
|
|
1980-01-01
|
Wings - Bonding of access panels to wing structure.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1980-01-01
|
|
|
G-0055-PRE80
|
|
1980-01-01
|
Flight Controls - Rudder circuit - To increase the clearance between the rudder spring tab and tail cone.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1980-01-01
|
|
|
G-0054-PRE80
|
|
1980-01-01
|
Landing Gear - Main undercarriage cross beam and radius rod - Introduction of a strengthened retraction jack pin.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1980-01-01
|
|
|
G-0053-PRE80
|
|
1980-01-01
|
Propellers - Introduction of packing washer on propeller control unit plugs.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1980-01-01
|
|
|
G-0052-PRE80
|
|
1980-01-01
|
Flight Controls - Improvements to control surface lock circuit.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1980-01-01
|
|
|
G-0051-PRE80
|
|
1980-01-01
|
Auto-Pilot - Introduction of safety stop on elevator servo motor mounting.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1980-01-01
|
|
|
G-0050-PRE80
|
|
1980-01-01
|
Propellers - Introduction of cable retaining clips to uniterselmet cables at the plugs for the propeller control unit and auto feathering switch.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1980-01-01
|
|
