AD/B767/252 - Auxilary Fuel tank Pump Automatic Shut Off Installation (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.

Boeing 767 Series Aeroplanes AD/B767/252 Auxilary Fuel tank Pump 10/2009 Automatic Shut Off Installation

Applicability: Model 767-200, -300, -300F and -400ER series aeroplanes. Requirement: 1. For Model 767 aeroplanes with line numbers 1 through 940 inclusive - Install an automatic shutoff system for the centre tank fuel pump, in accordance with Boeing Service Bulletin (SB) 767-28A0083, Revision 2, dated 12 February 2009 (for Model 767-200, -300 and -300F aeroplanes); or Boeing SB 767-28A0084, Revision 1, dated 26 April 2007 (for Model 767-400ER aeroplanes); as applicable. Installing an automatic shutoff system is also acceptable for compliance with the Requirement 1, if accomplished before the effective date of this Directive in accordance with service information identified in Table 1. Table 1 - Previous Issues of Service Bulletins Boeing Service Information Revision Level Date Alert Service Bulletin 767-28A0083 Original 3 May 2006