Document ID: chunk:federal_register_of_legislation:F2006B11367:body:0
Version: federal_register_of_legislation:F2006B11367
Segment Type: other
Provision Reference: 
Character Range: 0–803

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-2/37 Flap Flexible Shaft Sealing and Torque Check 12/85

            Applicability: All models MU-2B/-10/-15/-20/-25/-26 with S/Nos. 008 to 347 except S/Nos. 313 and 321. All models MU-2B-30/-35/- 36 with S/Nos.501 to 696 except S/Nos. 652
            and 661.

 Requirement: Action in accordance with Mitsubishi SB No. 198.

            Note: JCAB AD No. TCD-2451-85 refers.

            Compliance: At the next scheduled inspection for Maintenance Release issue after 31 December 1985.

            Background: The manufacturer reports failures of the flexible drive shaft attributable to ingress of moisture.