AD/DHC-2/3 Rudder Pedal Assembly Modification Cancelled (Cth)

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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/DHC-2/3.

DHC-2 (Beaver) Series Aeroplanes

AD/DHC-2/3 Rudder Pedal Assembly - Modification 11/2008

Requirement:

CANCELLED.

This AD is cancelled on 23 October 2008.

Background:

This AD, raised in 1963 against De Havilland (Canada) Engineering Bulletin (EB) Series "B" No.2, issue 2, dated 24 February 1958, required a modification to improve rigidity of the rudder pedal assembly by introduction of an interconnecting linkage.

Compliance was required before issue of CofA or on conversion from Landplane to Floatplane.

As all aircraft will have been modified long ago, this AD is no longer required.

David Villiers
Delegate of the Civil Aviation Safety Authority

9 September 2008

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