AD/CESSNA 310/39 - Main Landing Gear Attachment - Inspection
1AD/CESSNA 310/39 - Main Landing Gear Attachment - Inspection
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
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Cessna 310 Series Aeroplanes
AD/CESSNA 310/39 Main Landing Gear Attachment - Inspection 9/75
Applicability: All models 310 to 310K inclusive. Requirement: With aeroplane on jacks:
Remove Main Landing Gear Attaching “U” Bolts and Shafts.
2. Visually inspect the “U” Bolts, with the aid of a 10X glass, in the area of the thread root ends for cracks.
3. Visually inspect the Attaching Shafts, with the aid of a 10X glass, in the area of the roll pin hole for cracks.
Compliance: 1. For MLG attachment shafts and “U” bolts which have achieved 2500 hours time in service at 12 August 1975; within 100 hours time in service and thereafter at intervals not exceeding 200 hours time in service.
- All other MLG attachment shafts and “U” bolts; before achieving 2500 hours time in service and thereafter at intervals not exceeding 200 hours time in service.