AD/BEECH 300/9 Amdt 1 - Outflow/Safety Valve

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Legislation au F2006B03779 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 300 Series Aeroplanes

 

AD/BEECH 300/9

Amdt 1


Outflow/Safety Valve 3/98

 

Applicability: All model 300 series aircraft with serial numbers as listed in the requirement document.

 

Requirement: Inspect and if necessary replace the outflow/safety valve in accordance with the procedures detailed in Beech SB 2484 Revision 1 dated October 1995.

 

Aircraft previously certified against the initial issue of this Directive can be certified as compliant with Amdt 1.

 

No person shall install on any aircraft any Outflow/Safety Valve found to be unserviceable in accordance with this directive.

 

Note: FAA AD 97-25-01 Amdt 39-10224 refers and replaces FAA AD 96-17-10 Amdt 39-9719.

 

Compliance: Within 200 hours time in service or 4 months, whichever occurs first, from the effective date of this directive.

 

This amendment becomes effective on 26 February 1998.

 

Background: Manufacturing problems with the safety valve may cause a rapid decompression of the aircraft should a valve failure occur. This amendment expands the range of serial numbers per outflow/safety valves affected.

 

The original issue of this airworthiness directive became effective on 7 November 1996.

 

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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.