Document ID: chunk:federal_register_of_legislation:F2006B07363:body:0
Version: federal_register_of_legislation:F2006B07363
Segment Type: other
Provision Reference: 
Character Range: 0–793

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 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.