Document ID: chunk:federal_register_of_legislation:F2010L01613:body:0:p1
Version: federal_register_of_legislation:F2010L01613
Segment Type: other
Provision Reference: 
Character Range: 0–10097

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

                Netherlands AD                                                                                                                                                                                                                                                                                                              Issue Date                                    Title
   90-055    18 May 1990                                                                                                                                                                                                                                                                                                                  Fuel Drain Tank Vent Sleeve
   89-022    13 February 1989                                                                                                                                                                                                                                                                                                             AFCS Altitude Select Mode Wiring
  88-086     21 October 1988                                                                                                                                                                                                                                                                                                              Propeller Overspeed Governor Inspection
  88-061-2   28 February 1997                                                                                                                                                                                                                                                                                                             Engine Handling Bleed Valve Relay
  88-044-2   9 June 1989                                                                                                                                                                                                                                                                                                                  Upper Nacelle Brace Struts
  88-043     23 June 1988                                                                                                                                                                                                                                                                                                                 Cockpit Voice Recorder System Modification
  88-041     13 June 1988                                                                                                                                                                                                                                                                                                                 Engine Nacelle Hinged Fairing Folding Strut
  88-027     11 April 1988                                                                                                                                                                                                                                                                                                                Stall Warning System Modification
  88-023     30 March 1988                                                                                                                                                                                                                                                                                                                Right Hinged Cowl Door Air Intake
  87-090     7 December 1987                                                                                                                                                                                                                                                                                                              Propeller Attachment Bolts Torque Check
             Note 1:  Netherlands ADs may be accessed via the internet at the following URL:

             http://ad.easa.europa.eu/
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 7 July 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.