Commonwealth legislation

AD/CESSNA 188/36 - Vertical Fin Rear Spar

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This instrument mandates owners/operators of specified Cessna 188 (Agwagon) aeroplanes (listed serial numbers) to carry out the inspections/repairs set out in Cessna Service Information Letter No. SE80‑85, to be completed within 100 hours TIS after 31 December 1980. It responds to overseas reports of cracks in the vertical fin rear spar; operators bear the cost and scheduling burden, and must obtain and follow the SIL for technical details.

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AD/CESSNA 188/36 - Vertical Fin Rear Spar

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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 188 (Agwagon) Series Aeroplanes

AD/CESSNA 188/36 Vertical Fin Rear Spar 12/80 Applicability: Model 188 with S/Nos. 18801375 to 18803725 and T18803307T to T18803725T. Requirement: Action in accordance with Cessna SIL No. SE80-85.

Compliance: Within 100 hours time in service after 31 December 1980.

Background: Overseas, cracks have been found in the flanges and web of the spar below the lower rudder hinge.

Source text

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