Ad/F100/97 Amdt 1 - State of Design Airworthiness Directives (Cth)

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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/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 18/2011

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

     94-129

31 August 1994

Lavatory Pump and Filter Assembly

     94-114-4

31 July 1996

No. 1 Pitot Heating System - Replacement

     94-029

21 February 1994

Circuit Breaker Terminal Bolts

Netherlands AD

Issue Date

Title

     91-031-2

23 April 1993

MLG Downlock Actuator Mechanism

     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

     91-013

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 Amendment becomes effective on 9 September 2011.

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.

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.

Mike Higgins
Delegate of the Civil Aviation Safety Authority

31 August 2011

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