Document ID: chunk:federal_register_of_legislation:F2010L00729:body:0
Version: federal_register_of_legislation:F2010L00729
Segment Type: other
Provision Reference: 
Character Range: 0–1363

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.

British Aerospace BAe 125 Series Aeroplanes
AD/HS 125/184  Main Entry Door Frame Pressing  6/2010

Applicability:  Raytheon Model DH 125-1A and -3A series aeroplanes.
Requirement:    Action in accordance with FAA AD 98- 05-16 Amendment 39-10377 dated
                10 April 1998.
Compliance:     In accordance with the Requirement document.
                This Airworthiness Directive becomes effective on 8 April 2010.
Background:     This AD is prompted by reports of fatigue cracking which could lead to loss of structural integrity of the main entry door and, as a consequence, decompression of the cabin.

Mike Higgins
Delegate of the Civil Aviation Safety Authority
16 March 2010