AD/CIRRUS/9 - Rudder and Aileron Rigging (Cth)

AIRWORTHINESS DIRECTIVE For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (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.

Cirrus Design SR20 and SR22 Series Aeroplanes AD/CIRRUS/9 Rudder and Aileron Rigging 5/2008

Applicability: Cirrus Design Corporation Model SR20 aeroplanes, serial numbers (SN) 1005 through 1861, and Model SR22 aeroplanes, SN 0002 through 2333, SN 2335 through 2419, and SN 2421 through 2437 all inclusive. Requirement: 1. Inspect the rudder, aileron, and rudder-aileron interconnect rigging; correct any out-of-rig condition; and replace the attaching hardware for the rudder-aileron interconnect in accordance with Cirrus Service Bulletin No. SB 2X-27-14 R3, dated 10 October 2007.

2. Report to CASA via the Service Difficulty Reporting (SDR) system any out-of-rig conditions discovered as a result of the inspection detailed in Requirement 1 of this AD.

Include the following information in the report. 1. Inspection Performed By: 2. Telephone: 3. Aircraft Model: 4. Aeroplane Serial Number: 5. Aircraft Total Hours Time-in-Service: 6. Date of inspection detailed in Requirement 1 of this AD: 7.a. Do any of the aircraft logs contain entries describing flight control system maintenance, preventative maintenance, or alteration: 7.b. If Yes, copy the log book entry(s) and include the date of the entry.