Ad/F100/97 Amdt 1 - 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/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:
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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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