Commonwealth legislation

AD/F28/51 - Main Landing Gear Bay Cracking

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This directive requires owners/operators of specific Fokker F28s (S/Ns 11003–11091, 11094–11135, 11991–11992) to carry out the actions in Fokker Service Bulletin F28/57-76 to address a reported crack near Station 2635 and the rear spar. Compliance is mandatory by 31 March 1986; the AD delegates inspection/repair detail to the manufacturer’s bulletin and does not state cost, enforcement, or payment arrangements.

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AD/F28/51 - Main Landing Gear Bay Cracking

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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 Fokker F28 Series Aeroplanes

AD/F28/51 Main Landing Gear Bay Cracking 2/86

Applicability: All model F28 with S/Nos 11003 to 11091, 11094 to 11135, 11991 and 11992. Requirement: Action in accordance with Fokker SB F28/57-76.

Note: RLD AD 85-87 refers.

Compliance: Prior to 31 March 1986.

The manufacturer reports an instance of a crack in the area of Station 2635 and the rear spar.

Source text

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