AIRWORTHINESS DIRECTIVE
Beechcraft King Air 100 · Airworthiness Directives
Overview
This document is an Airworthiness Directive (AD) issued by the Civil Aviation Safety Authority of Australia concerning the Beechcraft 200 series aircraft, specifically the Super King Air. The directive outlines the cancellation of a previous AD that mandated inspections of the left-hand rudder cable installation. The cancellation is based on the fact that all aircraft have been modified to rectify the previously identified unsafe condition. The document serves as a formal notice to pilots and maintenance personnel regarding the status of the AD and the safety of the aircraft.
- The Airworthiness Directive AD/BEECH 200/32 has been cancelled as of 10 April 2008.
- The original directive required inspections of the left-hand rudder cable installation due to potential safety risks.
- Compliance with the original AD was required within 100 hours after 31 July 1981.
- The unsafe condition identified in the original AD no longer exists due to modifications made to all affected aircraft.
Document
Source
Originally published by services.casa.gov.au. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Airworthiness Directives
- Year
- 2008
- Pages
- 1
- File size
- 11 KB
- Publisher
- services.casa.gov.au
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- Pilot's Operating Handbook / AFM
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- Type Certificate (TCDS)
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In this document
Airworthiness Directive Cancellation
The document officially cancels Airworthiness Directive AD/BEECH 200/32, which was issued in 1981. This directive required inspections of the left-hand rudder cable installation to prevent abnormal wear and potential in-flight cable separation. The cancellation is effective as of 10 April 2008.
Background of the Directive
The original directive mandated compliance within 100 hours of time in service after 31 July 1981. It required inspections to be conducted according to Beechcraft Service Instruction 1172. The unsafe condition was determined to no longer exist as all aircraft have been modified.
Full document text
COMMONWEALTH OF AUSTRALIA (Civil Aviation Safety Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES Page 1 of 1 AIRWORTHINESS DIRECTIVE On the effective date specified below, and for the reasons set out in the background section, the CASA delegate whose signature appears below revokes Airworthiness Directive AD/BEECH 200/32. Beechcraft 200 (Super King Air) Series Aeroplanes AD/BEECH 200/32 Left Hand Rudder Cable Installation 4/2008 Requirement: CANCELLED. This AD is cancelled on 10 April 2008. Background: This unique Australian airworthiness directive (AD), issued in 1981, required inspection of the LH rudder cable to ensure the cable had been correctly routed in the under-floor area as incorrect routing would cause abnormal wear that could lead to in- flight cable separation. The inspection was to be carried out in accordance with Beechcraft Service Instruction (SI) 1172 rather than a State of Design airworthiness directive. Compliance with the AD was required within 100 hours time in service after 31 July 1981. As all aircraft would now be modified, the unsafe condition no longer exists. David Punshon Delegate of the Civil Aviation Safety Authority 28 February 2008


