AD/DHC-2/15 Amdt 1 - Main Undercarriage Lower Forward Bolt Attachment - Inspection
1AD/DHC-2/15 Amdt 1 - Main Undercarriage Lower Forward Bolt Attachment - Inspection
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text DHC-2 (Beaver) Series Aeroplanes
AD/DHC-2/15
Amdt 1
Applicability: All models.
Main Undercarriage Lower Forward Bolt Attachment - Inspection
8/84
Requirement: Inspect the main undercarriage lower forward attachment bolts for cracking as follows:
- P/N C2U-487ND (part of bolt assembly No. C2U-185A) : magnetic particle inspect in accordance with ANO 108.8 or fluorescent penetrant inspect in accordance with ANO 108.10.
2. P/N 02-B-16 (hard chrome plated bolts): fluorescent penetrant inspect in accordance with ANO 108.10.
Compliance: At intervals not exceeding 100 hours time in service for aircraft engaged in agricultural operations, and 500 hours time in service for other aircraft.