AD/750XL/8 - Fuselage Roof, Station 180.85 (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 39.001(1) of CASR 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.

Pacific Aerospace 750XL Series Aeroplanes AD/750XL/8 Fuselage Roof, Station 180.85 11/2006

Applicability: Model 750XL aircraft, serial numbers 102, 104 through 120, 122, and 125. Requirement: Inspect in accordance with the Accomplishment Instructions of Pacific Aerospace Corporation (PAC) Service Bulletin No. PACSB/XL/019 Rev 1, dated 21 April 2006.

Note: NZ CAA AD DCA/750XL/8 refers. Compliance: Within 150 hours time in service after 26 October 2006. This Airworthiness Directive becomes effective on 26 October 2006. Background: During routine inspection of an aircraft at PAC, a row of rivets on top of the fuselage were identified as being 1/8-inch solid rivets rather than the specified 5/32-inch solid rivets. Inspection of other aircraft at PAC revealed all had correct specification rivets. As this rivet error could have occurred in earlier production aircraft, this Directive requires a detailed inspection of certain fuselage top rivets.

David Villiers Delegate of the Civil Aviation Safety Authority

13 September 2006