AD/BEECH 200/17 Nacelle Wheel Well Fender Installation Cancelled (Cth)

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 200/17.

Beechcraft 200 (Super King Air) Series Aeroplanes

AD/BEECH 200/17 Nacelle Wheel Well Fender Installation 4/2008

Requirement:	CANCELLED.
This AD is cancelled on 10 April 2008.
Background:	This AD was raised in 1977 against manufacturer’s mandatory Service Instruction 0897 applicable to aircraft manufactured with high flotation landing gear.  The SI required inspection of the main gear wheel well fender installation for possible loose rivets and modification of wheel well fender brackets.  The inspection was required at the next 100 hour inspection after 31 July 1977 and thereafter at intervals not exceeding 100 hours TIS until modified prior to the accumulation of 500 hours TIS.  As all aircraft would long have been modified, this AD is no longer required.

David Villiers
Delegate of the Civil Aviation Safety Authority

26 February 2008