AD/F100/97 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 F100 (F28 Mk 100) Series Aeroplanes

AD/F100/97 State of Design Airworthiness Directives 12/2010

Applicability:	Fokker Aircraft B.V. F28 Mark 0100 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
96-153	31 December 1996	Leading Edge Torsion Box Drainage
96-074	28 June 1996	MLG Upper Torque Link Pin
95-104	31 October 1995	Overwing Emergency Exit Release Handle
95-087	31 August 1995	Wing Leading Edge Bleed Air Holes
95-086-2	28 February 1997	Airstair Passenger Door Back-up Structure
95-050	31 May 1995	Flight Compartment Flexible Oxygen Hoses
95-013	28 February 1995	Landing Gear Wheel Brake Assembly
94-172-2	31 January 1996	Outer Wing Collector Tank Area
94-146	30 September 1994	Fuel Balance Transfer System
94-129	31 August 1994	Lavatory Pump and Filter Assembly
94-114-4	31 July 1996	No. 1 Pitot Heating System - Replacement

Netherlands AD	Issue Date	Title
94-029	21 February 1994	Circuit Breaker Terminal Bolts
94-024	28 January 1994	Hydraulic Return Filter Diaphragm Assembly
93-088	12 July 1993	Flight Control Lock Handle and Switch
93-042	22 March 1993	Fuel Supply Line/Hydraulic Line Clearance
92-139	27 November 1992	APU - Fuel Supply and Drain Lines
92-120	23 October 1992	Liftdumper System Electrical Wiring
92-103	5 October 1992	Airborne Auxiliary Power - Mounting Frame
92-087	25 September 1992	Rudder Pedal Assemblies
92-058	24 April 1992	Cabin Attendants - Oxygen Drop-out Panels
92-051	8 April 1992	Horiz Stabilizer/Actuator Attach Link Bolts
92-034	25 February 1992	Autopilot Rudder Servo Input Brackets
92-033-2	22 March 1993	HP Bleed Air Shut-off Valve Circuit Breakers
92-028-2	20 January 1993	Return Filter Bypass Valve Assemblies
92-016	24 January 1992	Flight Control Computer
92-015-2	26 June 1992	APU Fuel Supply Line
91-116	18 October 1991	Service/Emergency Door C-Latch Nylon Bushes
91-106	13 September 1991	Flight Mode  Panel
91-105	6 September 1991	Engine Fire Detection Wire
91-071-2	6 April 1992	Passenger Address System

Netherlands AD	Issue Date	Title
91-031-2	23 April 1993	MLG Downlock Actuator Mechanism
91-013	8 January 1991	Primary Flight Control Servo Mounts and Motors
90-122	26 October 1990	Main Wheel Assembly
Note 1:  Netherlands ADs may be accessed via the internet at the following URL:
Compliance:	If a certificate of airworthiness has not been issued for the aircraft - before issue of the certificate of airworthiness. If a certificate of airworthiness has been issued for the aircraft - within 60 days after the effective date of this Directive.
This Airworthiness Directive becomes effective on 30 June 2010.
Background:	The Netherlands ADs listed in Table 1 of this Directive require once-only actions for which the compliance date and/or period has passed.  CASA has determined that these ADs may be applicable to recently-registered Australian aircraft.  This Directive is issued to ensure all State of Design ADs are complied with. CASA appreciates that, due to date of aircraft manufacture or aircraft configuration and modification status, some of the ADs listed in Table 1 will not be applicable to some aeroplanes.

Charles Lenarcic
Delegate of the Civil Aviation Safety Authority

10 June 2010