Commonwealth legislation

AD/HU 269/12 - Main Rotor Blade Flapping Hinge - Inspection

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Commonwealth

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legislative instrument

Plain English Summary

3/10 complexity

This directive mandates recurring inspections of the main rotor blade flapping hinge on Hughes/Schweizer Model 269A and 269B helicopters, at intervals not exceeding 400 flight hours measured from the baseline date.

Owners/operators must arrange and pay for inspections, repairs, and follow the referenced Hughes structural inspection notices (SINs) for procedures, creating an ongoing scheduling, administrative and compliance cost while delegating detailed inspection methods to the manufacturer documents.

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AD/HU 269/12 - Main Rotor Blade Flapping Hinge - Inspection

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Schweizer (Hughes) 269 Series Helicopters

AD/HU 269/12 Main Rotor Blade Flapping Hinge - Inspection 12/64

Applicability: Models 269A and 269B.

Document: 1. Hughes SINs 2A-391, 2A-1, -06.1 or 2B-07.1 where applicable; or

Hughes SIN N-47.

Compliance: At intervals not exceeding 400 hours time in service after 9 December 1964.

Source text

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