Document ID: chunk:federal_register_of_legislation:F2006B11364:body:0
Version: federal_register_of_legislation:F2006B11364
Segment Type: other
Provision Reference: 
Character Range: 0–937

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-2/34 Engine Air Intake Bleed Air Tubing Coupling Nut
                     Retorque, Inspection, Modification

 7/84

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

 Document: Mitsubishi SB No. 196 Rev A.

            Note: JCAB AD No. TCD-2342-84 refers.

 Compliance: Before further flight after 31 July 1984.

            Background: Loss of engine bleed air at the intake anti-ice coupling nut can cause malfunction of the engine air intake anti-ice system. The manufacturer has therefore introduced an inspection and a minor modification to ensure permanent security of the coupling nut.