Commonwealth legislation

AD/PA-38/4 Amdt 1 - Pilots Control Wheel Installations - Inspection and Modification

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This Airworthiness Directive requires owners/operators of affected Piper PA‑38 (Tomahawk) aeroplanes to inspect—and, if necessary, modify—the pilot’s control‑wheel installation in accordance with Piper Service Bulletin No. 609A. Work must be completed within 25 hours time‑in‑service after 31 October 1978. Compliance costs and technical steps are those set out in the referenced service bulletin.

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AD/PA-38/4 Amdt 1 - Pilots Control Wheel Installations - 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-38/4

Amdt 1

Pilot’s Control Wheel Installations - Inspection and Modification

9/87

Applicability: As detailed in Piper SB No. 609A. Document: Piper SB No. 609A.

Compliance: Unless already accomplished, in accordance with SB No. 609, within 25 hours time in service after 31 October 1978.

Source text

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