1AD/HU 269/18 - Tail Boom - 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 Schweizer (Hughes) 269 Series Helicopters

 

AD/HU 269/18 Tail Boom - Inspection 11/67

Applicability: Models 269A and 269B.

 

Requirement:  Visually inspect the tail boom for cracks originating at the bolts attaching the tail rotor transmission housing to the boom and also the horizontal stabiliser forward mounting bolt.

 

Compliance: At intervals not exceeding 50 hours time in service after 13 May 1966.