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/F100/97 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.
Fokker F100 (F28 Mk 100) Series Aeroplanes
AD/F100/97 Amdt 1
State of Design Airworthiness Directives
Fokker Aircraft B.V. F28 Mark 0100 aeroplanes.
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.
30 June 1997
Emergency Lighting Control Panel Placard
31 December 1996
Leading Edge Torsion Box Drainage
28 June 1996
MLG Upper Torque Link Pin
31 October 1995
Overwing Emergency Exit Release Handle
31 August 1995
Wing Leading Edge Bleed Air Holes
28 February 1997
Airstair Passenger Door Back-up Structure
31 May 1995
Flight Compartment Flexible Oxygen Hoses
28 February 1995
Landing Gear Wheel Brake Assembly
31 January 1996
Outer Wing Collector Tank Area
31 August 1994
Lavatory Pump and Filter Assembly
31 July 1996
No. 1 Pitot Heating System - Replacement
21 February 1994
Circuit Breaker Terminal Bolts
23 April 1993
MLG Downlock Actuator Mechanism
28 January 1994
Hydraulic Return Filter Diaphragm Assembly
12 July 1993
Flight Control Lock Handle and Switch
22 March 1993
Fuel Supply Line/Hydraulic Line Clearance
27 November 1992
APU - Fuel Supply and Drain Lines
23 October 1992
Liftdumper System Electrical Wiring
5 October 1992
Airborne Auxiliary Power - Mounting Frame
25 September 1992
Rudder Pedal Assemblies
24 April 1992
Cabin Attendants - Oxygen Drop-out Panels
8 April 1992
Horiz Stabilizer/Actuator Attach Link Bolts
25 February 1992
Autopilot Rudder Servo Input Brackets
22 March 1993
HP Bleed Air Shut-off Valve Circuit Breakers
20 January 1993
Return Filter Bypass Valve Assemblies
24 January 1992
Flight Control Computer
26 June 1992
APU Fuel Supply Line
18 October 1991
Service/Emergency Door C-Latch Nylon Bushes
13 September 1991
Flight Mode Panel
6 September 1991
Engine Fire Detection Wire
6 April 1992
Passenger Address System
8 January 1991
Primary Flight Control Servo Mounts and Motors
26 October 1990
Main Wheel Assembly
Note 1: Netherlands ADs may be accessed via the internet at the following URL:
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 Amendment becomes effective on 9 September 2011.
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.
Amendment 1 of this Airworthiness Directive has been issued to remove reference to Netherlands AD 94-146 from Table 1. The release of EASA AD No. 2011-0158 (26 August 2011) supersedes Netherlands AD 94-146, thus removing the requirement to comply with AD 94-146 via this Directive.
Delegate of the Civil Aviation Safety Authority
31 August 2011