Commonwealth legislation

AD/TBM 700/16 - Main Landing Gear Inboard Doors

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Commonwealth

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legislative instrument

Plain English Summary

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Applies to Aerospatiale (Socata) TBM 700s with MOD 70-065-32 or OPT 70-57-001: owners/operators must remove the main landing-gear inboard doors per SOCATA TBM 700 Service Bulletin No. 70-073-32 by 15 March 1996. The interim measure aims to reduce the risk of the main gear remaining locked “up” from corrosion; compliance, scheduling and costs fall to aircraft owners/operators and follow the prescribed service bulletin.

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AD/TBM 700/16 - Main Landing Gear Inboard Doors

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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) TBM 700 Series Aeroplanes

AD/TBM 700/16 Main Landing Gear Inboard Doors 5/96 DM

Applicability: All aircraft with modification No. MOD 70-065-32 embodied or option No.

OPT 70-57-001 installed.

Requirement: Remove the main landing gear inboard doors in accordance with SOCATA TBM 700 SB No. 70-073-32.

Note: DGAC AD 96-037(B) refers.

Compliance: Prior to 15 March 1996.

Background: This Directive is issued to avoid the possibility of the main landing gear remaining locked "up" due to the presence of corrosion products. Inboard door removal is an interim solution.

Source text

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