Document ID: chunk:federal_register_of_legislation:F2006B11392:body:0
Version: federal_register_of_legislation:F2006B11392
Segment Type: other
Provision Reference: 
Character Range: 0–1039

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

 Mitsubishi MU-2 Series Aeroplanes

AD/MU-2/62 Landing Gear Actuating Mechanism 2/98

 Applicability: Models MU-2B, MU-2B-10, -15, -20, -25, and -26 aircraft with serial numbers 008
            through 347, except serial numbers 313 and 321; and Models MU-2B-30, -35, and -36
            aircraft with serial numbers 501 through 696, except serial numbers 652 and 661.

            Requirement: Modify the bearing box(es) in the landing gear actuating mechanism in accordance with Mitsubishi MU-2 Service Bulletin 230.

            Note: JCAB AD TCD-4684-97 refers.

 Compliance: Unless already accomplished, within 100 hours time in service after 29 January 1998.

            This airworthiness directive becomes effective on 29 January 1998.

            Background: The JCAB requires modification action in order to prevent the possible inability to completely extend the landing gear.