AD/BEECH 50/34 Amdt 1 - Forward Elevator Cable (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) AD/BEECH 50/34 and issues the following AD under subregulation 39.001(1) of CASR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

Beechcraft 50 (Twin Bonanza) Series Aeroplanes AD/BEECH 50/34 Amdt 1 Forward Elevator Cable 4/2012

Applicability: All Beechcraft 50 series (Twin Bonanza) aeroplanes fitted with forward elevator control cable configuration as detailed in figure 1 of this AD. Requirement: 1. Inspect the forward elevator control cable assembly for wear, broken wires and corrosion; or replace the forward elevator cable assembly.

2. Remove from service any forward elevator control cable assembly found to be defective as a result of inspection conducted in accordance with Requirement 1 of this AD.

3. Do not install on any aircraft a cable assembly or parts thereof that have been removed in accordance with Requirement 2 of this AD.

Note 1: Inspections carried out in accordance with FAA AC 43-13-1B, chapter 7, Section 8, paragraph 7-149(d) or Beechcraft maintenance data are an acceptable means of compliance for the inspection called up by Requirement 1 of this AD. Compliance: For Requirement 1.