Document ID: chunk:federal_register_of_legislation:F2006B06261:body:0
Version: federal_register_of_legislation:F2006B06261
Segment Type: other
Provision Reference: 
Character Range: 0–1076

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

 Transavia PL 12 Series Aeroplanes

 AD/PL 12/15
 Amdt 1

 Landing Gear Lower Pivot Lug 2/89

 Applicability: PL 12 and PL 12U:-
            For Para 1 - S/Nos G350 to G465. For Para 2 - All S/Nos prior to G466.

             Requirement: 1. Visually inspect the outer faces of the landing gear lower pivot lug in the vicinity of the weld joining the reinforcing washer to the lug.

             2.    Inspect the landing gear lower pivot lug in accordance with Transavia SB No. 20.

3.    Reinforce each lower pivot lug in accordance with Transavia SB No. 25 or a scheme approved by the Authority.

 Compliance: For Para. 1 - Daily, until modified.

            For Para. 2 - At intervals not exceeding 75 hours time in service until modified. For Para. 3 - Before 1 September 1974.
            Background: This Amendment changes the "Applicability" to reflect design and manufacturing improvements to later model aircraft.