Commonwealth legislation

AD/CESSNA 210/22 - Intercostal Bulkhead - Reinforcement

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Jurisdiction

Commonwealth

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legislative instrument

Plain English Summary

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The Civil Aviation Safety Authority directive AD/CESSNA 210/22 mandates a physical reinforcement of the intercostal bulkhead on specific Cessna 210 (S/N 21058819–21059030) and T210 (S/N T210‑0198–T210‑0378) aircraft. Affected owners/operators must complete the Cessna Service Letter SE72‑22 procedure within 100 hours time‑in‑service after 31 August 1972; costs, parts, labour and downtime fall to them. The directive references the manufacturer document for technical steps and does not state penalties.

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AD/CESSNA 210/22 - Intercostal Bulkhead - Reinforcement

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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 210 Series Aeroplanes

AD/CESSNA 210/22 Intercostal Bulkhead - Reinforcement 10/72

Applicability: All models with S/Nos. 21058819 to 21059030 and T210- 0198 to T210-0378. Document: Cessna SL SE72-22.

Compliance: Within 100 hours time in service after 31 August 1972.

Source text

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