Commonwealth legislation

AD/PA-38/10 - Stabiliser/Elevator Leading Edge - Inspection and Modification

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Jurisdiction

Commonwealth

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legislative instrument

Plain English Summary

3/10 complexity

This airworthiness directive requires owners/operators of Piper PA‑38‑112 serials 38‑78A0001 through 38‑78A0400 to inspect and modify the stabiliser/elevator leading edge per Piper Service Bulletin No. 607A Part III or FAA AD 78‑22‑01, unless already done. Compliance was required within 50 hours TIS after 20 Nov 1978; costs, downtime and proof of compliance fall to the aircraft owner/operator, while the AD delegates technical details to the referenced documents.

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AD/PA-38/10 - Stabiliser/Elevator Leading Edge - Inspection and Modification

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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 Piper PA-38 (Tomahawk) Series Aeroplanes

AD/PA-38/10 Stabiliser/Elevator Leading Edge - Inspection

and Modification Applicability: All models PA-38-112 with S/Nos. 38-78A0001 to 38-78A0400. Document: 1. Piper SB No. 607A, Part III; or

FAA AD 78-22-01, amendment 39-3323.

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Compliance: Unless already accomplished, within 50 hours time in service after 20 November 1978.

Source text

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