Commonwealth legislation

AD/TB20/31 - Main Landing Gear

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This AD requires owners/operators of Socata TB20/TB21 aircraft — but only those where the LH or RH attachment-bearing ring was removed and replaced — to carry out the inspection and corrective work specified in Socata Service Bulletin TB SB10.091.57. Work must be done within 50 hours TIS after 31 May 1995 or by 31 July 1995. Owners bear the cost; the rule ensures rings were correctly installed to maintain airworthiness.

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AD/TB20/31 - Main Landing Gear

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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 Aerospatiale (Socata) TB20 (Trinidad) Series Aeroplanes

AD/TB20/31 Main Landing Gear 8/95 DM

Applicability: TB20 and TB21 aircraft, on which the ring on the attachment bearing of the LH or RH main landing gear has been removed and replaced during maintenance.

Requirement: Action in accordance with Socata TB Service Bulletin SB10.091.57.

Note: DGAC AD 95-084(A) refers.

Compliance: Within 50 hours time in service after 31 May 1995, or prior to 31 July 1995, whichever occurs first.

Background: This Directive is issued to ensure that the rings, when replaced, have been correctly installed on the attachment bearing of the hinged strut.

Source text

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