Commonwealth legislation

AD/HU 269/55 - Lateral Cyclic Trim Control Assembly - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This directive requires owners/operators to have the lateral cyclic trim control assembly inspected on certain Schweizer/Hughes 269 series helicopters (specific serial-number ranges or any 269A/269B/269C fitted with listed part numbers). The inspection must be completed within 25 hours time-in-service after 28 July 1976 and must follow Hughes Service Information Notice N-138 or FAA AD 76-10-02. Costs, scheduling, and technical details fall to the operator and the referenced documents.

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/HU 269/55 - Lateral Cyclic Trim Control Assembly - Inspection.

AD/HU 269/55 - Lateral Cyclic Trim Control Assembly - Inspection

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 Schweizer (Hughes) 269 Series Helicopters

AD/HU 269/55 Lateral Cyclic Trim Control Assembly - Inspection 8/76

Applicability: Model 269C with S/Nos. 0162 to 0455, 0458 to 0463, 0465 to 0469, 0471 to 0475, and any model 269A, 269A-1, 269Bor 269C equipped with a P/N 269A7316-3,-5, -7,

-9 or -11 cyclic trim control assembly: Document: 1. Hughes SIN No. N-138; or

FAA AD 76-10-02.

Compliance: Within 25 hours time in service after 28 July 1976.

Source text

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