Commonwealth legislation

AD/F27/126 - Wing Attachment Fitting Bolts

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This AD requires owners/operators of Fokker F27 airframes S/No 10102–10259 in the pre‑SB F27/53‑60 (Part II) configuration to carry out the technical actions specified in RLD AD 91‑067 (with Fokker SB F27/53‑115 referenced). It was issued after reports of loose/sheared bolts at fuselage stations that attach the outboard wing fittings; Australian operators get a revised compliance effective date of 12 December 1991.

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AD/F27/126 - Wing Attachment Fitting Bolts

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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/F27/126 Wing Attachment Fitting Bolts 12/91

Applicability: Model F27 S/No 10102 thru 10259, if in pre-SB F27/53-60 (Part II) - config. Requirement: Action in accordance with the Technical Requirements of RLD AD 91-067.

Note: Fokker SB F27/53-115 refers.

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

Background: Report of loose or sheared bolts and screws which connect fuselage main frame STA 7961 and STA 9439.5 to the outboard wing attachment fittings. The effective date required by the RLD is extended by approximately four months.

Source text

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