AD/BEECH 400/15 - Outflow/Safety Valve

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Legislation au F2006B03917 In force Legislative Instrument

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Beechcraft 400 Series Aeroplanes

 

AD/BEECH 400/15 Outflow/Safety Valve 12/96

Applicability: All model 400 and 400A series aircraft equipped with outflow/safety valve P/N 103570-25 or -27 and with S/N as listed in the Requirement Document.

 

Requirement: Unless previously carried out, action in accordance with Allied Signal SB 103570-21-4012 R1 dated May 30, 1995.

 

Note: FAA AD 96-17-10 Amdt 39-9719 refers.

 

Compliance: Prior to 30 March 1998.

 

Background:  The manufacturer has reported cracking of the outflow/safety valves. This has resulted in several valve failures which could result in a rapid decompression of the aircraft cabin.

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.