Commonwealth legislation

AD/PA-38/24 - Elevator Control Travel - Modification

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

Owners/operators of Piper PA-38-112 aeroplanes (serials 38-78A0001 through 38-82A0122) must have the elevator control modification in Piper Service Bulletin No. 800 carried out. The AD mandates this work within 100 hours TIS after 28 Feb 1985 or at the next scheduled inspection to fix a reported restriction in moving the yoke out of full‑aft.

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AD/PA-38/24 - Elevator Control Travel - 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-38/24 Elevator Control Travel - Modification 2/85

Applicability: All model PA-38-112 with S/Nos. 38-78A0001 to 38-82A0122. Requirement: Piper SB No. 800.

Compliance: Within 100 hours time in service after 28 February 1985 or at the next scheduled inspection for maintenance release issue after 28 February 1985, which ever is the later.

Background: It has been reported that when either control wheel is full AFT and an upward-and- forward pressure is applied, the potential exists that the pilot may be unable to move the control yoke out of the full AFT position.

Source text

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