Document ID: chunk:federal_register_of_legislation:F2006B03917:body:0
Version: federal_register_of_legislation:F2006B03917
Segment Type: other
Provision Reference: 
Character Range: 0–840

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.