Commonwealth legislation

AD/PA-20/7 Amdt 1 - Fuselage Fabric in Area of Wind Shield Top Attachment Channel - Modification

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This AD mandates recurring work on the fuselage fabric at the windshield top attachment channel for Piper PA‑20s that do not incorporate SL 362, to be done per Piper Service Bulletin No. 174 or FAA AD 61‑6‑6. Inspections/modifications are required every 100 flight hours or six months. Owners/operators of affected PA‑20s bear the cost and scheduling impact.

JSON API

Deep dive

Want the full deep dive?

Zoe can write the in-depth analysis on top of the summary above: how it works, who it affects and what each part actually does.

Current sections

Direct links to the current provisions in AD/PA-20/7 Amdt 1 - Fuselage Fabric in Area of Wind Shield Top Attachment Channel - Modification.

AD/PA-20/7 Amdt 1 - Fuselage Fabric in Area of Wind Shield Top Attachment Channel - Modification

meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-generator: Aspose.Words for .NET 22.10.0

?xml version="1.0" encoding="utf-8" standalone="no"?>

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-20 (Pacer) Series Aeroplanes

AD/PA-20/7

Amdt 1

Fuselage Fabric in Area of Wind Shield Top Attachment Channel - Modification

4/69

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.