Commonwealth legislation

Airworthiness Directives 2004 - Revocation and Remaking - Mitsubishi MU-2 Series Aeroplanes

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This instrument cancels a long list of existing Airworthiness Directives (ADs) for Mitsubishi MU‑2 aeroplanes and reissues each AD as a separate, identical instrument. It affects aircraft owners, operators and maintenance organisations who must continue to meet the inspections, modifications and other requirements in those ADs. The change is made by a CASA delegate under subregulation 39.001(1); mechanically it is an administrative re‑issuance that preserves existing obligations while requiring parties to track the newly issued instruments for compliance and record‑keeping.

JSON API Aviation / CASA instruments

Deep dive

Want the full deep dive?

Zoe can write the in-depth analysis on top of the summary above: how it works, who it affects and what each part actually does.

Current sections

Direct links to the current provisions in Airworthiness Directives 2004 - Revocation and Remaking - Mitsubishi MU-2 Series Aeroplanes.

Airworthiness Directives 2004 - Revocation and Remaking - Mitsubishi MU-2 Series Aeroplanes

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.

View image in the official source

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

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.

1 Airworthiness Directives 2004 - Revocation and Remaking - Mitsubishi MU-2 Series Aeroplanes