List of Mandatory Continuing Airworthiness Information
Displaying records 15041 to 15060 out of a total of 15938 publications.
|
Number
|
Issued by
|
Issue date
|
Subject
|
Approval Holder / Type Designation
|
Effective date
|
Attachment |
|
G-0696-PRE80
|
|
1980-01-01
|
Fuselage - To cut away vertical flange of roof head-liner to clear flange of forward engine frame.
|
|
1980-01-01
|
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|
G-0695-PRE80
|
|
1980-01-01
|
SUPERSEDED: Fuselage - Fuselage structure - Chafing of engine mounting frame at Station 778.
|
|
1980-01-01
|
|
|
G-0694-PRE80
|
|
1980-01-01
|
Pneumatic - To revise distribution of air conditioning and anti-icing systems.
|
|
1980-01-01
|
|
|
G-0693-PRE80
|
|
1980-01-01
|
SUPERSEDED: Pneumatic - Integrated air system - Electrical power distribution.
|
|
1980-01-01
|
|
|
G-0692-PRE80
|
|
1980-01-01
|
SUPERSEDED: Flight Controls - Flap secondary transmission shaft joint.
|
|
1980-01-01
|
|
|
G-0691-PRE80
|
|
1980-01-01
|
Landing Gear - To add steel reinforcing strip and cleat on nosewheel accumulator guard to prevent guard melting due to friction loads incurred when the oleo is retracted in a collapsed state with wheels spinning.
|
|
1980-01-01
|
|
|
G-0690-PRE80
|
|
1980-01-01
|
Landing Gear - To revise the test instructions for the nose undercarriage.
|
|
1980-01-01
|
|
|
G-0689-PRE80
|
|
1980-01-01
|
SUPERSEDED: Landing Gear - Nose landing gear - retraction with shock absorber strut not fully extended.
|
|
1980-01-01
|
|
|
G-0688-PRE80
|
|
1980-01-01
|
Landing Gear - To provide strengthened guards left and right sides of nosewheel bay.
|
|
1980-01-01
|
|
|
G-0687-PRE80
|
|
1980-01-01
|
Airborne Auxiliary Power - APU - Fuel leakage at atomiser housing.
|
|
1980-01-01
|
|
|
G-0686-PRE80
|
|
1980-01-01
|
Flight Controls - To introduce rudder jacks giving ±21° rudder movement and to revise torque shaft stops.
|
|
1980-01-01
|
|
|
G-0685-PRE80
|
|
1980-01-01
|
SUPERSEDED: Flight Controls - Rudder - Range of movement and operating jack eye ends.
|
|
1980-01-01
|
|
|
G-0684-PRE80
|
|
1980-01-01
|
Lights - To revise design of freight hold light assemblies.
|
|
1980-01-01
|
|
|
G-0683-PRE80
|
|
1980-01-01
|
Flight Controls - Elevator PCU Centralising Spring Pot - Sticking of spring pot and damage to special nut.
|
|
1980-01-01
|
|
|
G-0682-PRE80
|
|
1980-01-01
|
Navigation - To introduce five second time delay in stall correction system.
|
|
1980-01-01
|
|
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G-0681-PRE80
|
|
1980-01-01
|
Landing Gear - Cracking of main landing gear torque link lugs.
|
|
1980-01-01
|
|
|
G-0680-PRE80
|
|
1980-01-01
|
Communications - To record Collins Radio Service Bulletin No. 17 on 618M Series VHF transceivers.
|
|
1980-01-01
|
|
|
G-0679-PRE80
|
|
1980-01-01
|
Flight Controls - Rudder Feel Simulator Unit - Fatigue limitation.
|
|
1980-01-01
|
|
|
G-0678-PRE80
|
|
1980-01-01
|
Stabilizers - Tailplane - Cracking of lower surface stringers.
|
|
1980-01-01
|
|
|
G-0677-PRE80
|
|
1980-01-01
|
Fuel - To redesign Mark 41 re-fuel valve housing in centre section torque box to change material from Light Alloy to Stainless Steel.
|
|
1980-01-01
|
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