Document ID: chunk:federal_register_of_legislation:F2006B06412:body:0
Version: federal_register_of_legislation:F2006B06412
Segment Type: other
Provision Reference: 
Character Range: 0–815

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

 PZL M18 Dromader Series Aeroplanes

AD/PZL/3 Upper Fin Rudder Attachment 8/91

 Applicability: Serial Number 1Z001-01 to 1Z021-30.

            Requirement: Action in accordance with the Technical Requirements of FAA AD 90-17-15, Amendment 39-6678.

            Note: PZL-Mielec Mandatory Engineering Bulletin (MEB) No. K/02.135/89, dated 29 December 1989, refers.

            Compliance: As specified in the Requirement Document with revised effective date of 8 August 1991.

            Background: This AD provides for inspection and reinforcement of the fin in the area of the upper rudder attach point, following two reports of cracks and damage to the area.