Commonwealth legislation

AD/PA-30/4 - Auto-Pilot Pitch Servo Motor - Modification

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This AD mandates an immediate modification of the auto‑pilot pitch‑servo motor on Piper PA‑30 and PA‑39 aircraft fitted with the Mitchell Altimatic 2. Affected owners/operators and maintenance organisations must comply "Forthwith" by following the technical instructions in Piper Service Bulletin No. 224 and Mitchell Service Bulletin No. A55. The AD itself delegates all technical detail to those service bulletins.

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AD/PA-30/4 - Auto-Pilot Pitch Servo Motor - 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-30 & 39 (Twin Comanche) Series Aeroplanes

AD/PA-30/4 Auto-Pilot Pitch Servo Motor - Modification 7/65

Applicability: All models fitted with Mitchell Altimatic 2 Auto-Pilot. Document: 1. Piper SB No. 224; and

Mitchell SB No. A55. Compliance: Forthwith.

Source text

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