Document ID: chunk:federal_register_of_legislation:F2006B11352:body:0
Version: federal_register_of_legislation:F2006B11352
Segment Type: other
Provision Reference: 
Character Range: 0–983

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-2/23 Nose Landing Gear Retracting Mechanism - Inspection

11/81

            Applicability: All models MU-2B/-10/-15/-20/-25/-26 with S/Nos. 005 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: To prevent the possible failure of the NLG retracting mechanism perform the following:

             1. Inspect the NLG retracting mechanism down lock system in accordance with Mitsubishi MU-2 SB No. 188 dated 13 July 1981.

            Note: JCAB AD No. TCD-2070-81 refers.

            Compliance: Unless already accomplished, within 100 hours time in service after 30 September 1981.

 Background: The nose landing gear down lock system may be improperly adjusted.