AD/F50/102 - State of Design Airworthiness Directives (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.

Fokker F50 (F27 Mk 50) Series Aeroplanes AD/F50/102 State of Design Airworthiness Directives 12/2010

Applicability: Fokker Aircraft B.V. F27 Mark 050 aeroplanes. Requirement: 1. Determine the applicability of the Netherlands Airworthiness Directives (AD) listed in Table 1. 2. If it is determined that a Netherlands AD listed in Table 1 is applicable and has not been previously accomplished, perform the actions required by that AD or later EASA-approved revision. Table 1 Netherlands AD Issue Date Title 97-060 30 June 1997 Emergency Lighting Control Panel Placard 94-029 21 February 1994 Circuit Breaker Terminal Bolts 93-130 17 September 1993 Propeller Operating Cylinder Retaining Bolts 92-073 10 July 1992 Fuel (Motive) Flow Tube Assembly 92-072 10 July 1992 Mechanical Fuel Control Unit 92-002 24 January 1992 Honeywell Autopilot Computer Replacement 91-128-2 30 January 1998 Engine Compressor Case Fire Detection Element 91-020 1 March 1991 Alternate Gear Handle & Gust Lock Lever 90-129 9 November 1990 Engine Auto-Feather Unit Torque Sensors 90-105 28 September 1990 Manoeuvering Speed Limitation Placards