Airworthiness Directives 2004 - Revocation and Remaking - Mitsubishi MU-2 Series Aeroplanes (Cth)
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Airworthiness Directives 2004
I, DAVID ALAN VILLIERS, delegate of the Civil Aviation Safety
Authority, acting under subregulation 39.001 (1) of the Civil
Aviation Safety Regulations 1998:
(a) revoke the Airworthiness Directives mentioned in
Schedule 1; and
(b) make, as separate instruments, each Airworthiness
Directive mentioned in Schedule 1 and attached.
David Villiers
Delegate of the Civil Aviation Safety Authority
20 December 2004
Note: Each attached Airworthiness Directive is being re-made in exactly the
same form as appears in the latest published edition of the Directive.
Schedule 1 Revocation and Remaking of
Airworthiness Directives
Mitsubishi MU-2 Series Aeroplanes
AD Name AD Number
Lagging of Engine Air Bleed Pipes - Modification AD/MU-2/1
Windows - Cabin and Cockpit - Modification AD/MU-2/2
Integral Fuel Vent Check Valve AD/MU-2/3 Amdt 1
Integral Fuel Tank Sealing - Inspection AD/MU-2/4 Amdt 1
Wing Structural Fatigue Limitation AD/MU-2/5 Amdt 3
Nose Landing Gear Actuator and Bracket Bolts - Replacement AD/MU-2/6
Front Seat Restraint Installations - Modification AD/MU-2/7
Front Windshield Outer Pane - Inspection and Windshield De-Fogging Air AD/MU-2/8 Amdt 1
Trim Aileron Bellcrank Bracket Bolt Holes - Inspection AD/MU-2/9
Flap Control System Flexible Shafts - Inspection AD/MU-2/10 Amdt 1
Propeller Pitch Control Lever - Inspection AD/MU-2/11
Nose Landing Gear Shimmy Damper - Inspection AD/MU-2/12
Main Landing Gear Forward Door Emergency Cable - Inspection AD/MU-2/13
Engine Nacelle Upper Door Latches - Inspection AD/MU-2/14
Main Landing Gear Door Mechanism Support - Inspection AD/MU-2/15
Main Landing Gear Drag Strut - Inspection AD/MU-2/16
Elevator Trim Tab Bracket - Inspection and Replacement AD/MU-2/17 Amdt 4
Flap Jack Screw - Inspection: Flap Gearbox - Inspection and Re-adjustment AD/MU-2/18
Engine Nacelle Upper Door Rod Assembly - Removal and Modification AD/MU-2/19
Engine Nacelle Upper Door Latch Link - Replacement AD/MU-2/20
Outer Fuel Tank Switch Wiring - Modification AD/MU-2/21 Amdt 1
Nose Landing Gear Strut Assembly AD/MU-2/22 Amdt 2
Nose Landing Gear Retracting Mechanism - Inspection AD/MU-2/23
Nose Landing Gear L/H Drag Strut Attach Bracket - Inspection and AD/MU-2/24 Amdt 1
Flap Control System Torque Tube Assembly Joint AD/MU-2/25 Amdt 2
Control Cable Turnbuckles - Inspection and Replacement AD/MU-2/26
Engine Control System Cable Pulleys - Replacement AD/MU-2/27
Nose Landing Gear Eccentric BO - Inspection and Replacement AD/MU-2/28
Avionic Equipment Mounting Shelf - Modification AD/MU-2/29
Engine Electrical Harness - Inspection and Replacement of P/No MS25471 AD/MU-2/30
Cockpit Airconditioning Ducts - Inspection and Modification AD/MU-2/31
Replacement of Series Relay and Modification to the Two Battery System AD/MU-2/32
Rudder and Elevator Trim Idler Installation - Modification AD/MU-2/33
Engine Air Intake Bleed Air Tubing Coupling Nut Retorque, Inspection, AD/MU-2/34
Horizontal Stabiliser Leading Edge Skin - Inspection and Modification AD/MU-2/35
Pitot System AD/MU-2/36 Amdt 1
Flap Flexible Shaft Sealing and Torque Check AD/MU-2/37
Landing Gear Aural Warning System AD/MU-2/38
Fitment of Manual Ignition Switches AD/MU-2/39
Placard - Use of Reverse Thrust AD/MU-2/40
Generator Wiring AD/MU-2/41 Amdt 1
Autopilot/Electric Trim Switch Standardisation AD/MU-2/42
Autopilot/Electric Trim Switch Standardisation AD/MU-2/43
Split Radio Bus AD/MU-2/44
Operational Restrictions - CANCELLED AD/MU-2/45 Amdt 3
Anti-Ice and De-Ice Systems AD/MU-2/46
Elevator and Rudder Trim Tab Spar AD/MU-2/47
Rudder Trim Tab AD/MU-2/48
Underwing Pressure Bulkhead Flange AD/MU-2/49 Amdt 1
Hartzell Propeller Blade Pilot Tube Bore - CANCELLED AD/MU-2/50 Amdt 1
Autopilot Engage Switch Guard AD/MU-2/51
Elevator Nose-Down Trim Limit AD/MU-2/52 Amdt 1
Ice Detector System Installation AD/MU-2/53 Amdt 1
Tip Tank Wiring Conduit AD/MU-2/54
Emergency Gear Down Gearbox AD/MU-2/55
Underspeed Governor Minimum Stop AD/MU-2/56
Acrylic Windshield and Side Windows AD/MU-2/57
Wing Tip Tank Attachment AD/MU-2/58
Propeller Feathering Valve and Linkage - CANCELLED AD/MU-2/59
De-Ice System Modification AD/MU-2/60 Amdt 1
Trim In Motion and Automatic Pilot Disconnect System AD/MU-2/61 Amdt 1
Landing Gear Actuating Mechanism AD/MU-2/62
Landing Gear Drive Train AD/MU-2/63
Elevator Trim Indication AD/MU-2/64
Engine Torque Indication System AD/MU-2/65
Flight Test AD/MU-2/66
Fuselage Frame AD/MU-2/67
Wing Tip Fuel Tank Attach Brackets AD/MU-2/68
Flap Drive Torque Tube AD/MU-2/69
Pneumatic Lines AD/MU-2/70
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