|
Number
|
Issued by
|
Issue date
|
Subject
|
Approval Holder / Type Designation
|
Effective date
|
Attachment |
|
G-011-09-85
|
|
1985-09-01
|
Doors - Overwing escape hatch - Introduction of steel operating shaft - Modified secondary locking cam, secondary lock indicator flag and warning decal.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1985-09-01
|
|
|
G-010-09-85
|
|
1985-09-01
|
Servicing Procedures - Introduction of the HS 748 mandatory Supplementary Structural Inspection Document.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1985-09-01
|
|
|
G-016-09-85
|
|
1985-09-01
|
Electrical Power - To ensure adequate clearance between one installed main DC flexible busbar and adjacent circuit breakers.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1985-09-01
|
|
|
G-015-09-85
|
|
1985-09-01
|
Fuselage - To introduce an inspection for cracks of the nose equipment bay spine member.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1985-09-01
|
|
|
G-014-09-85
|
|
1985-09-01
|
Lights - To introduce an illuminated warning sign above the main entrance door and label at toilet door.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1985-09-01
|
|
|
G-013-09-85
|
|
1985-09-01
|
Power Plant - Replacement of insufficiently heat treated engine mounting structure attachment bolts.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1985-09-01
|
|
|
G-012-09-85
|
|
1985-09-01
|
Wings - Feather edges at holes used to secure under wing fuel tank access panels.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1985-09-01
|
|
|
G-006-09-85
|
|
1985-09-01
|
Autoflight - Autopilot - To introduce extended pitch runaway protection for aircraft pre-mod HCM 45018A.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1985-09-01
|
|
|
G-005-09-85
|
|
1985-09-01
|
Flight Controls - Elevator control system - To introduce lighter -G- weight and delete balance spring.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1985-09-01
|
|
|
F-1975-163-024
|
|
1985-08-22
|
Amortisseurs hydrauliques 3130 S.13.60.000 mont鳠sur moyeu rotor principal - Modifications
|
|
1985-08-22
|
|
|
SE-1-008-Rev-A
|
|
1985-08-15
|
FLIGHT CONTROLS - ELEVATOR TRIM TAB SYSTEM, MOCIFICATION OF PITCH TRIM SYSTEM
|
|
1985-08-15
|
|
|
SE-1-009
|
|
1985-08-15
|
ENGINE CONTROLS - REPLACEMENT OF O-RING SEAL FITTING AND SEALING OF ENGINE CONTROL CABLES AT WING TO FUSELAGE INTERFACE
|
|
1985-08-15
|
|
|
G-006-08-85
|
|
1985-08-01
|
Flight Controls - Introduction of guards in way of elevator and rudder control levers.
|
|
1985-08-01
|
|
|
G-005-08-85
|
|
1985-08-01
|
Fuselage - Introduction of reinforcing strap on fuselage top skin.
|
|
1985-08-01
|
|
|
F-1985-140-018
|
|
1985-07-31
|
Main gear box - Accessory gearbox
|
|
1985-07-31
|
|
|
F-1985-135-042
|
|
1985-07-31
|
Fuel filter and main gear box oil filter
|
|
1985-07-31
|
|
|
F-1985-112-041
|
|
1985-07-03
|
Fuel system - Fuel filter drain pipe
|
|
1985-07-10
|
|
|
G-008-07-85
|
|
1985-07-01
|
Engine - Combustion outer casing - on wing crack inspection at the HP6 offtake soleplate.
|
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
|
1985-07-01
|
|
|
NL-1985-044
|
|
1985-06-26
|
WING AUXILIARY STRUCTURE BUTT STRAPS RESEALING
|
|
1985-06-28
|
|
|
F-1985-095-040
|
|
1985-06-19
|
Main rotor shaft
|
|
1985-06-26
|
|
