AD/HU 369/67 Amdt 1 - Main Rotor Retention Strap
1AD/HU 369/67 Amdt 1 - Main Rotor Retention Strap
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text 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.