Document ID: chunk:federal_register_of_legislation:F2007L01729:body:0:p1
Version: federal_register_of_legislation:F2007L01729
Segment Type: other
Provision Reference: 
Character Range: 0–6408

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.

Avions de Transport Regional ATR 42 Series Aeroplanes
AD/ATR 42/1  State of Design Airworthiness Directives  8/2007 DM

Applicability:     ATR 42 series aeroplanes, as identified in the individual Airworthiness Directive (AD) listed Tables 1 and 2.
Requirement:          1. Determine the applicability of the ADs issued by the Direction Générale de l'Aviation Civile of France (DGAC), listed in Table 1, and the ADs issued by the European Aviation Safety Agency (EASA), listed in Table 2.
                      2. If it is determined that an DGAC or EASA AD listed in Table 1 or 2 is applicable and has not been previously accomplished, perform the actions required by that AD.
                   Table 1
DGAC AD            Issue Date                                                                                                                                                                                                                    Title
F-1986-085-002 R1  28 May 1986                                                                                                                                                                                                                   Oil cooling system
F-1986-078-001 R1  23 July 1986                                                                                                                                                                                                                  Ipeco pilot and copilot seats - ATR Airplanes
F-1986-130-003 R1  26 March 1997                                                                                                                                                                                                                 Flaps 45º Configuration
F-1987-022-004     4 January 1987                                                                                                                                                                                                                Automatic stop of the flight and cockpit voice recorders
                   F-1987-046-005 R1                                                                                                                                                                                                             10 June 1987                                              Attitude and heading system
                   F-1987-155-007                                                                                                                                                                                                                10 November 1987                                          Elevator trims
                   F-1987-156-008 R1                                                                                                                                                                                                             16 November 1988                                          Propeller brake control system
                   F-1987-173-009                                                                                                                                                                                                                9 December 1987                                           Protection for auto pilot roll actuator
                   F-1988-051-010 R2                                                                                                                                                                                                             21 February 1990                                          Fuel quantity indicators
                   F-1988-070-011                                                                                                                                                                                                                11 May 1988                                               Rudder control channel cables
                   F-1988-080-012                                                                                                                                                                                                                22 June 1988                                              Engine and propeller flexible control shafts
                   F-1988-092-013                                                                                                                                                                                                                17 August 1988                                            Honeywell-Sperry navigation equipment

   F-1988-135-014     19 October 1988   Main gear wheel bearing
   F-1988-147-015     16 November 1988  Propeller brake control pushbutton
   F-1988-186-016 R1  31 May 1989       Test system of the smoke detectors in cargo compartment areas
   F-1989-033-019 R1  31 May 1989       Pitch trim
   F-1989-042-018 R1  5 April 1989      Oil pressure transmitter manifold
   F-1989-067-020 R2  20 March 1991     Main L/G retraction jacks fitting bolts
   F-1989-077-021 R2  19 July 1989      Aileron tab inboard hingepin
   F-1989-093-022     28 June 1989      Automatic cut-off of the voice recorders
   F-1989-197-025 R1  4 April 1990      Fire extinguishing system
   F-1990-028-026     21 February 1990  Nose landing gear retraction system
   F-1990-029-027     21 February 1990  Emergency lighting
   F-1990-030-028 R1  23 January 1991   Propeller brake
   F-1990-109-029     13 June 1990      Main frames
   F-1990-155-030 R1  27 November 1991  Emergency oxygen system for cabin attendants
   F-1990-163-031     3 October 1990