AD/B737/285 Amdt 2 - State of Design Airworthiness Directives (Cth)

AIRWORTHINESS DIRECTIVE On the effective date specified below, and for the reasons set out in the background section, the CASA delegate whose signature appears below revokes Airworthiness Directive (AD) AD/B737/285 Amdt 1 and issues the following 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 737 Series Aeroplanes AD/B737/285 Amdt 2 State of Design Airworthiness Directives 10/2006

Applicability: Boeing Model 737-100 and -200 series aeroplanes. Requirement: 1. If not previously accomplished, determine the applicability of the United States Federal Aviation Administration (FAA) Airworthiness Directives (AD) listed in Table 1. 2. If it is determined that a FAA ADs is applicable and has not been previously accomplished, perform the actions required by that AD. Table 1 FAA AD Number Effective Date Title 75-24-09 12 September 1977 Hydraulic System Fluid 79-26-02 31 December 1979 Ground Proximity Warning System Flap Position Switches 83-01-05 R2 4 August 1986 Engine Starter Operation Indication 85-02-03 1 March 1985 Runaway Stabiliser Trim 92-08-06 29 May 1992 Sperry SP177 Autopilot Flight Control Computers and Mode Control Panels 96-22-11 11 December 1996 Waterman Hydraulic Fuses 96-23-04 19 December 1996 Static Inverters 2001-24-33 16 January 2002 Auxiliary Power Unit Generator Power Feeder Wire Bundle Compliance: For Requirements 1 and 2 - Within 30 days after the effective date of this Amendment. This Amendment becomes effective on 28 September 2006.