Document ID: chunk:federal_register_of_legislation:F2007L02441:body:0
Version: federal_register_of_legislation:F2007L02441
Segment Type: other
Provision Reference: 
Character Range: 0–1335

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 42/16  Windshield Frame  9/2007

Applicability:  Model ATR 42 -200, -300, and -320 aircraft, without modification 1392 incorporated.
Requirement:    Action in accordance with the Requirements of DGAC AD 95-126-061(B).
Compliance:     Before the accumulation of 24,000 flights.
                This Airworthiness Directive becomes effective on 30 August 2007.
Background:     This Directive requires inspection and modification of the windshield frame in order to prevent the initiation and development of fatigue damage.

David Villiers
Delegate of the Civil Aviation Safety Authority

10 July 2007