Commonwealth legislation

AD/F27/127 - Fuselage Bracket Attachment Fasteners

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Commonwealth

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legislative instrument

Plain English Summary

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This airworthiness directive requires owners/operators of the listed Fokker F27 serial numbers to comply with the Technical Requirements of RLD AD 91‑112 (related to fuselage bracket attachment fasteners) after reports of loose bolts and hi‑shear pins.

The Civil Aviation Safety Authority issues the AD, sets a revised compliance date of 12 December 1991 for Australian‑registered aircraft, and compliance costs and implementation fall to the aircraft owners/operators.

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AD/F27/127 - Fuselage Bracket Attachment Fasteners

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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 F27 Series Aeroplanes

AD/F27/127 Fuselage Bracket Attachment Fasteners 12/91

Applicability: Model F27 S/No’s 10102 thru 10433, 10435 thru 10443, & 10446 thru 10450. Requirement: Action in accordance with the Technical Requirements of RLD AD 91-112.

Note: Fokker SB F27/57-23 Revision 6 refers.

Compliance: As specified in the Requirement Document with a revised effective date of 12 December 1991 for Australian registered aircraft.

Background: Reports of loose bolts and hi-shear pins in the brackets on the front and rear spars. The effective date required by the RLD is extended by approximately two months.

Source text

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