Commonwealth legislation

AD/HS 125/184 - Main Entry Door Frame Pressing

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This directive requires owners/operators of Raytheon Model DH 125-1A and -3A aircraft to carry out the inspections and repairs set out in FAA AD 98-05-16 for the main entry door frame pressing. It becomes effective 8 April 2010.

The measure responds to reports of fatigue cracking that could cause loss of door integrity and cabin decompression. Operators pay for inspections/repairs and must change maintenance scheduling; CASA enforces compliance by adopting the FAA AD.

JSON API

Deep dive

Want the full deep dive?

Zoe can write the in-depth analysis on top of the summary above: how it works, who it affects and what each part actually does.

Current sections

Direct links to the current provisions in AD/HS 125/184 - Main Entry Door Frame Pressing.

British Aerospace BAe 125 Series Aeropla

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 dated10 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.

View image in the official source

Mike Higgins
Delegate of the Civil Aviation Safety Authority

16 March 2010

AD/HS 125/184

Main Entry Door Frame Pressing

6/2010

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.

British Aerospace BAe 125 Series Aeropla British Aerospace BAe 125 Series Aeroplanes

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 dated10 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.

AD/HS 125/184 - Main Entry Door Frame Pressing

Plain English Summary

Deep dive

Current sections

British Aerospace BAe 125 Series Aeroplanes

British Aerospace BAe 125 Series Aeroplanes

AD/HS 125/184

AD/HS 125/184

Main Entry Door Frame Pressing

Main Entry Door Frame Pressing

6/2010

6/2010

Source text

British Aerospace BAe 125 Series Aeropla British Aerospace BAe 125 Series Aeroplanes

British Aerospace BAe 125 Series Aeroplanes

AD/HS 125/184 AD/HS 125/184

AD/HS 125/184

Main Entry Door Frame Pressing Main Entry Door Frame Pressing

Main Entry Door Frame Pressing

6/2010 6/2010

6/2010