Document ID: chunk:federal_register_of_legislation:F2006B07926:body:0:p2
Version: federal_register_of_legislation:F2006B07926
Segment Type: other
Provision Reference: 
Character Range: 3000–4740

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