Commonwealth legislation

AD/PA-22/13 Amdt 1 - Fuselage Fabric in Area of Windshield Top Attachment Channel - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This AD requires owners/operators of Piper PA‑22 (Tri‑Pacer and Colt) aeroplanes not incorporating SL 362 to inspect the fuselage fabric at the windshield top attachment channel. Inspections must recur every 100 hours TIS or 6 months and follow the procedure in Piper SB No. 174 or FAA AD 61‑6‑6. It creates recurring maintenance cost and downtime, or the alternative of installing SL 362 to remove the aircraft from the AD’s applicability.

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AD/PA-22/13 Amdt 1 - Fuselage Fabric in Area of Windshield Top Attachment Channel - 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 Piper PA-22 (Tri-Pacer and Colt) Series Aeroplanes

AD/PA-22/13

Amdt 1

Fuselage Fabric in Area of Windshield Top Attachment Channel - Inspection

5/69

Applicability: All models not incorporating SL 362. Document: 1. Piper SB No. 174; or

FAA AD 61-6-6.

Compliance: At intervals not exceeding 100 hours time in service or 6 months whichever occurs first.

Source text

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