AD/BAe 146/43 - N2 Limitations for Anti-Ice Selection - Placard

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Legislation au F2006B03494 Not 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

 


British Aerospace BAe 146 Series Aeroplanes

 

AD/BAe 146/43 N2 Limitations for Anti-Ice Selection - Placard 5/92

Applicability: All BAe146 series aeroplanes specified in the Requirement Document.

 

Requirement: Action in accordance with British Aerospace Mandatory Service Bulletin # SB.11-97- 01285A.

 

Compliance: Prior to 31 September 1992.

 

Background: There have been incidents of engine N1/N2 mismatch resulting in engine roll back which cannot be restored within TGT limits when operating above FL250 with engine Anti-Ice on and after selecting airframe Anti-Ice on. In addition to introducing a placard giving a flight level and RPM limitation, wiring changes are introduced to inhibit the thrust lever actuated airbrake auto-retract function to enable the airbrake to be operated at high altitude to assist in descent when the thrust levers are forward in compliance with the placard requirements.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.