Commonwealth legislation

AD/PA-38/3 Amdt 1 - Vertical Fin/Rudder Leading Edge - Inspection and Modification

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This airworthiness directive requires owners/operators of specified Piper PA-38-112 (Tomahawk) serial numbers to inspect and modify the vertical fin and rudder leading edge, following Piper Service Bulletin No. 607A (Parts I & II) or FAA AD 78-22-01. Inspections must occur at least every 25 hours TIS, with the modification completed within 50 hours TIS after 20 November 1978. Owners/operators bear the cost and scheduling burden.

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AD/PA-38/3 Amdt 1 - Vertical Fin/Rudder 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-38/3

Amdt 1

Vertical Fin/Rudder Leading Edge - Inspection and Modification

1/79

Applicability: All models PA-38-112 with S/Nos. 38-78A0001 to 38-78A0215 and 38-78A0217 to 38-78A0226.

Document: 1. Piper SB No. 607A, Parts I and II; or

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

Compliance: 1. Inspect at intervals not exceeding 25 hours time in service; and

Modify 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.