AD/HU 369/41 Amdt 10 - Main Rotor Blade Root Fitting Assembly and Hub Lead-Lag Link Assemblies (Cth)

McDonnell Douglas (Hughes) and Kawasaki 369 Series Helicopters

AIRWORTHINESS DIRECTIVE

For the reasons set out in the background section, the CASA delegate whose signature appears below revokes Airworthiness Directive (AD) AD/HU 369/41 Amdt 9 and issues the following AD under subregulation 39.1 (1) of CAR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

AD/HU 369/41 Amdt 10

Main Rotor Blade Root Fitting Assembly and Hub Lead-Lag Link Assemblies

7/2000

DM

Applicability: Model 369 series equipped with main rotor blade assemblies and main rotor hub lead- lag link assemblies listed in the Requirement document.

Requirement: Action in accordance with MD Helicopters SB Nos. HN-211.6, DN-51.8, EN-42.6, and FN-31.6 dated 3 January 2000.

Note 1: FAA AD 95-03-13 refers to Amendment 9.

Note 2: FAA AD 91-17-04 refers to Amendment 6 and earlier amendments of this Directive.

Compliance: 1. Requirement Document:

1. Part I: As applicable:

* Unless already accomplished in accordance with the previous amendment of this directive, within 25 hours time in service after the effective date of this directive, or

* 100 hours time in service after the last inspection in accordance with Amendment 9 of this directive, and

* thereafter every 100 hours time in service; and