Document ID: chunk:federal_register_of_legislation:F2006B11338:body:0
Version: federal_register_of_legislation:F2006B11338
Segment Type: other
Provision Reference: 
Character Range: 0–634

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-2/10
 Amdt 1

 Flap Control System Flexible Shafts - Inspection 12/84

 Applicability: All models MU-2B aircraft referred to in the requirement document. Document: Mitsubishi MU-2 S.B. No. 162 Rev. A.
 Compliance: At intervals not exceeding 100 hours time in service after 28 February 1975.

            Background:  This directive is amended to clarify the aircraft applicability and amend the revision status of the requirement document.