Commonwealth legislation

AD/CESSNA 210/15 Amdt 1 - Aileron Mass Balance Weight Attachment Rivets - Inspection

In ForceCTH

Jurisdiction

Commonwealth

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legislative instrument

Plain English Summary

3/10 complexity

This airworthiness directive applies to Cessna 210 aeroplanes serials 21057841–21058220 and requires recurring inspections of the rivets attaching the lower aileron skin to the balance weight for corrosion, using a specified light sideways screwdriver blow to test rivet heads; any damaged or corroded rivets must be replaced.

Owners/operators must ensure inspections every 100 hours TIS and bear inspection, parts and downtime costs; maintenance personnel make the judgement calls and perform replacements.

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AD/CESSNA 210/15 Amdt 1 - Aileron Mass Balance Weight Attachment Rivets - 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 Cessna 210 Series Aeroplanes

AD/CESSNA 210/15

Amdt 1

Aileron Mass Balance Weight Attachment Rivets - Inspection

10/74

Applicability: All models with S/Nos. 21057841 to 21058220.

Requirement: Inspect the rivets attaching the lower aileron skin to the balance weight for corrosion.

Where corrosion is suspected under the rivet heads attempts should be made to remove the rivet heads by a light sharp sideways blow with a screwdriver. All damaged or corroded rivets must be replaced.

Compliance: Within 100 hours time in service after 29 September 1972 and there- after at intervals not exceeding 100 hours time in service.

Source text

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