Document ID: chunk:federal_register_of_legislation:F2006B11353:body:0
Version: federal_register_of_legislation:F2006B11353
Segment Type: other
Provision Reference: 
Character Range: 0–1257

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-2/24
 Amdt 1

  Nose Landing Gear L/H Drag Strut Attach Bracket - Inspection and Replacement

 11/83

            Applicability: All models MU-2B-30/-35/-36 with S/Nos. 501 thru 696, excepting S/Nos. 652 and 661. All models MU-2B-35/-36A/-60 with S/Nos. 652SA, 661SA, 697SA through 799SA, 1501SA through 1553SA. 1555SA through 1562SA.

 Document: 1. Mitsubishi SB No. 195. or

            2. Mitsubishi Aircraft International S.B. No. SBO 46/32-005 whichever is applicable.

            Note: JCAB AD No. TCD-2263-83 also refers.

 Compliance: Unless already accomplished:

              1. Inspect within 100 hours time in service after 30 June 1983 for components with more than 1000 hours time in service.

2.    Inspect within 100 hours time in service after component achieves 1000 hours time in service.

3.    Replace with improved bracket P/No. 030A-31121-11 in accordance with requirement document.

            Background:  This Directive has been raised in issue to include additional aircraft model applicability and requirement document references.