Commonwealth legislation

AD/HU 269/51 Amdt 1 - Tail Rotor Control System Pedal Installation - Inspection and Modification

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

4/10 complexity

This Airworthiness Directive requires owners/operators of all Schweizer (Hughes) HU 269 series helicopters to inspect—and, if necessary, modify—the tail-rotor control system pedal installation, with compliance to the manufacturer’s Hughes Service Instruction N-121.1.

It matters because the AD imposes a regulatory maintenance obligation that may ground aircraft, incur labour and parts costs, and fall to maintenance organisations to perform per the referenced document.

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AD/HU 269/51 Amdt 1 - Tail Rotor Control System Pedal Installation - Inspection and 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 Schweizer (Hughes) 269 Series Helicopters

AD/HU 269/51

Amdt 1

Tail Rotor Control System Pedal Installation - Inspection and Modification

1/78

Applicability: All models.

Document: Hughes SIN Co. N-121.1. Compliance: As per requirement document.

Source text

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