AD/HU 369/91 - "Flight Trials" Hardpoints

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

Legislation au F2006B10756 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

 


McDonnell Douglas (Hughes) and Kawasaki 369 Series Helicopters

 

AD/HU 369/91 "Flight Trials" Hardpoints  8/96 DM

Applicability:  Models 369D, 369E, 369F, 369FF, and 500N that have been modified using Flight Trials Helicopter Inc. hardpoint assemblies in accordance with either United States FAA:

 

  1. Supplementary Type Certificate SH6080NM approved by this Authority, or

 

b.    Form 337 "Major Repair and Alteration", prior to import into Australia. Requirement:              Remove from service any Flight Trials Helicopter Inc. hardpoints not marked with:

  1. a Part Number (P/N) FTH 105 LH Mod 1 for the port side and FTH 105 RH Mod 1 for the starboard side; and

 

b.    a Serial Number (S/N).

 

Note 1. Access may be gained by removing the NAS 1351-3 cap screw that secures the hardpoint to the P/N 369H2521-1 and -2 jacking fittings, and slipping the hardpoint assembly out of the step mount.

 

Note 2. FAA AD 96-08-03 refers.

 

Compliance: Before further flight after 22 May 1996.

 

Background: This Directive is raised to prevent failure of a hardpoint assembly with separation from the helicopter, and subsequent possible contact with the fuselage or rotor system.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.