Commonwealth legislation

AD/HU 269/104 - Rudder Pedal Bulkhead Gusset

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legislative instrument

Plain English Summary

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This directive from the Civil Aviation Safety Authority requires operators of Schweizer (Hughes) 269 series helicopters (269A, A‑1, B, C) to carry out the corrective work in Schweizer Service Bulletin B‑247 within 100 hours time‑in‑service after 10 November 1994. It responds to missing or cracked tail‑rotor pedal gussets and loose or missing rivets that affect structural safety.

Registered owners/operators must arrange and pay for the inspections, installations or repairs called for by the SB to remain compliant and airworthy.

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AD/HU 269/104 - Rudder Pedal Bulkhead Gusset

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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 269/104 Rudder Pedal Bulkhead Gusset 12/94

Applicability: Models 269A, A-1, B, and C.

Requirement: Action in accordance with Schweizer SB B-247.

Note: FAA AD 94-16-04 refers.

Compliance: Within 100 hours time in service after 10 November 1994.

Background: Tail rotor pedal gussets were not installed on 269A aircraft, and other aircraft have been found with the gussets cracked or with loose or missing rivets.

Source text

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