Airworthiness Directives 2004 - Revocation and Remaking - Mitsubishi Mu-2 Series Aeroplanes (Cth)

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