AD/BAe 146/4 Amdt 1 - Flight Controls - Stall Identification

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B03490 In force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


British Aerospace BAe 146 Series Aeroplanes

 

AD/BAe 146/4

Amdt 1


Flight Controls - Stall Identification 1/87

 

Applicability: Series 100 and 100A, and Series 200 and 200A, fitted with the suspect valves identified in the Requirement Document.

 

Requirement: Action in accordance with British Aerospace Service Bulletin 27-58.

 

Note: SB 27-58 supersedes SB 27-53.

 

Compliance: Inspect within 60 flights after 2 May 1986 and thereafter at intervals not exceeding 60 flights until replaced with modified valve.

 

For spares prior to installation in an aircraft and thereafter a intervals not exceeding 60 flights until replaced with modified valve.

 

Background: A number of stick push valves in service may become defective as a result of internal corrosion within the solenoid assembly. This could lead to a dormant failure not apparent on the flight deck.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.