AD/MU-2/23 - Nose Landing Gear Retracting Mechanism - Inspection

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B11352 In force Legislative Instrument

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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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.