AD/PHZL/75 - Propeller Hub Replacement (Cth)

AIRWORTHINESS DIRECTIVE For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (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.

Propellers - Variable Pitch - Hartzell

AD/PHZL/75 Propeller Hub Replacement 3/2003

Applicability: Hartzell 2 Bladed "Y" shank propellers fitted with aluminium hub part numbers D- 6522-1, D-6522-2, D-6529-1, and D-6559-3 with a hub serial number that is listed in Table 1 of this Directive.

Requirement: Remove from service applicable Hartzell aluminium hubs in accordance with Hartzell ASB HC-ASB-61-259.

Note 1: FAA AD 2003-01-03 Amdt 39-13014 refers.

Note 2: Hubs listed in Table 1 of this Directive are not to be installed.

Compliance: 1. Within 50 hours propeller hub time since new or 12 months from the effective date of this Directive, whichever occurs first, for propeller hubs installed on:

1. Piper PA-32 series aircraft with Textron Lycoming 540 series engines that are rated at 300HP or higher; or

b. Pilatus Britten Norman or Britten Norman BN-2 series aircraft (also known as Islander or Trislander) with Textron Lycoming 540 series engines; or

c. Any aircraft certified in the acrobatic category; or

d. Any aircraft routinely exposed to acrobatic manoeuvres; or