Commonwealth legislation

AD/CESSNA 336/9 - Flap Actuator - Inspection and Modification

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This AD applies to Cessna 336 airframes S/N 336‑0001 to 336‑0195 and mandates recurring inspection and relubrication of the flap actuator jack screw (per Cessna SL SE60‑16) until a one‑off modification (per Cessna SL ME72‑19) is installed. The modification must be completed by 1 June 1973.

It affects owners/operators and maintenance organisations, who bear the costs and scheduling; completing the retrofit eliminates the repeated 100‑hour inspections.

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AD/CESSNA 336/9 - Flap Actuator - 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 Cessna 336 Series Aeroplanes

AD/CESSNA 336/9 Flap Actuator - Inspection and Modification 2/73

Applicability: All models with S/Nos. 336-0001 to 336-0195.

Requirement: PART 1 - Inspect actuator jack screw and clean and relubricate in accordance with Cessna SL SE60-16.

PART 2 - Modify the aircraft in accordance with Cessna SL ME72-19.

Compliance: For Part 1 : At intervals not exceeding 100 hours time in service after 28 February 1973 until modified.

For Part 2 : Before 1st June 1973.

Source text

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