AD/HU 369/67 Amdt 1 - Main Rotor Retention Strap

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Legislation au F2006B10731 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 369/67

Amdt 1

Applicability: All models.


Main Rotor Retention Strap 4/88

 

Requirement: Action in accordance with Part 1 of McDonnell Douglas SIN HN214, DN154, EN44 or FN33 as applicable.

 

Compliance: As applicable by helicopter model, either:

 

(a)      within three months or one hundred hours time in service after the previous compliance with AD/HU 369/28D whichever occurs first; or

 

(b)     within nine months or three hundred hours time in service after the previous compliance with the initial issue of this Directive whichever occurs first;

 

(c)      and thereafter in accordance with the Requirement document. Background: The manufacturer has consolidated the inspection within the single SIN.

 

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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.