Commonwealth legislation

AD/PA-31/8 - Wing Leading Edge Stall Strips - Installation

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Commonwealth

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legislative instrument

Plain English Summary

3/10 complexity

This directive requires installation of wing leading edge stall strips on specified Piper PA‑31 aeroplanes (serials 31‑2 to 31‑445, with listed exclusions) following Piper Service Bulletin No. 294, to be completed within 50 hours TIS after 10 June 1969. It affects the registered owners/operators and maintenance organisations, who must schedule, pay for and certify the modification per the SB.

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AD/PA-31/8 - Wing Leading Edge Stall Strips - Installation

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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-31 Series Aeroplanes

AD/PA-31/8 Wing Leading Edge Stall Strips - Installation 7/69

Applicability: All models with S/Nos. 31-2 to 31-445 except the following S/Nos. 31-3, -5, -346, -

358, -367, -374, -379, -385, -407, -423, -424, -425, -429, -432, -435, -438, -440, -

441, -442, and -443.

Document: Piper SB No. 294.

Compliance: Within 50 hours time in service after 10 June 1969.

Source text

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