Document ID: chunk:federal_register_of_legislation:F2006B04899:body:0
Version: federal_register_of_legislation:F2006B04899
Segment Type: other
Provision Reference: 
Character Range: 0–1658

COMMONWEALTH OF AUSTRALIA (Civil Aviation Safety Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

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 39.1 (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.

 Cessna 120 and 140 Series Aeroplanes

AD/CESSNA 120/11 Primer Line 7/2003

 Applicability: Cessna 120 and 140 aircraft up to and including serial number 11842.

           Requirement: Unless previously accomplished reroute the primer line, adjust the strainer, and install a shield to the primer liner in accordance with Cessna Service Letter 34.

           Note: FAA AD 47-43-01 refers.

 Compliance: At the next scheduled maintenance visit.

           This Airworthiness Directive becomes effective on 10 July 2003.

           Background: Failure to reroute the primer could lead to fuel coming into contact with exhaust manifold.

 Jim Coyne
 Delegate of the Civil Aviation Safety Authority 28 May 2003

 The above AD is notified in the Commonwealth of Australia Gazette on 18 June 2003.

 Page 1 of 1