Document ID: chunk:federal_register_of_legislation:F2006B05963:body:0
Version: federal_register_of_legislation:F2006B05963
Segment Type: other
Provision Reference: 
Character Range: 0–792

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

 Piper PA-38 (Tomahawk) Series Aeroplanes

AD/PA-38/24 Elevator Control Travel - Modification 2/85

 Applicability: All model PA-38-112 with S/Nos. 38-78A0001 to 38-82A0122. Requirement:  Piper SB No. 800.
            Compliance: Within 100 hours time in service after 28 February 1985 or at the next scheduled inspection for maintenance release issue after 28 February 1985, which ever is the later.

            Background: It has been reported that when either control wheel is full AFT and an upward-and- forward pressure is applied, the potential exists that the pilot may be unable to move the control yoke out of the full AFT position.