Commonwealth legislation

AD/CESSNA 177/23 - Stabilator Trim Actuator Attach Bolt

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Commonwealth

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legislative instrument

Plain English Summary

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This AD makes compliance with Cessna Service Letter SE76‑14 mandatory: owners/operators of specified Cessna 177 and 177RG aeroplanes (serials 17702255–02494 and 177RG0700–0937) must address the stabilator trim actuator attach bolt per that service letter within 25 hours TIS after 18 August 1976. It converts the manufacturer’s guidance into a binding safety requirement, creating immediate scheduling, cost, and parts/maintenance pressures for affected operators.

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AD/CESSNA 177/23 - Stabilator Trim Actuator Attach Bolt

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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 Cessna 177 Series Aeroplanes

AD/CESSNA 177/23 Stabilator Trim Actuator Attach Bolt 9/76

Applicability: All models 177 and 177RG with S/Nos. 17702255 to 02494, and 177RG0700 to 0937.

Requirement: Action in accordance with Cessna SL SE76-14.

Note: FAA AD 76-14-08 AMDT. 39-2671 refers.

Compliance: Within 25 hours time in service after 18 August 1976.

Source text

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