Commonwealth legislation

AD/AC/17A - Landing Gear Truss Attach Angle - Inspection

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Commonwealth

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legislative instrument

Plain English Summary

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This Airworthiness Directive from CASA mandates recurring inspections of the landing‑gear truss attach angle on Twin Commander aeroplanes S/N 231–892 (except 875), carried out per Aero Commander Service Letter No. 77A at intervals not exceeding 1,000 hours’ time‑in‑service. Owners/operators must arrange and fund the inspections and use approved maintenance personnel or organisations to comply.

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AD/AC/17A - Landing Gear Truss Attach Angle - Inspection

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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 Twin Commander (Gulfstream/Rockwell/ Aerocommander 500, 600 and 700) Series Aeroplanes

AD/AC/17A Landing Gear Truss Attach Angle - Inspection 12/67

Applicability: All models: S/Nos. 231 to 892 except 875. Document: Aero Commander SL No. 77A.

Compliance: At intervals not exceeding 1000 hours’ time in service.

Source text

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