Commonwealth legislation

AD/F27/114 Amdt 1 - Main Landing Gear Torque Links

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This AD mandates that owners/operators of all Fokker F27 series comply with Dowty Rotol SB 32-161B Revision 2 to inspect and, if needed, repair or replace main landing gear torque links identified as incorrectly machined. Work must be done before 1 January 1989; operators bear the cost. Amendment 1 expands the batch numbers covered, increasing affected aircraft.

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AD/F27/114 Amdt 1 - Main Landing Gear Torque Links

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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/F27/114

Amdt 1

Applicability: All models.

Main Landing Gear Torque Links 11/87

Requirement: Action in accordance with Dowty Rotol SB 32-161B R2. Compliance: Prior to 1 January 1989.

Background: The manufacturer reports a number of torque links have been incorrectly machined during manufacture. Amendment 1 of this Directive references Revision 2 of the Requirement Document which extends the batch numbers identified as being incorrectly machined.

Source text

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