Document ID: chunk:federal_register_of_legislation:F2006B06627:body:0
Version: federal_register_of_legislation:F2006B06627
Segment Type: other
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Character Range: 0–897

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

 Robin Aviation Series Aeroplanes

AD/ROBIN/29 Hydraulic Lines 11/96

Applicability: All HR 100/250 and HR 100/285 series aircraft fitted with retractable landing gear.

 Requirement: Replace the inlet and outlet pipes of the Retractable Gear (R/G) hydraulic pump as required by Avions Pierre Robin SB No 148 dated April 26, 1996.

            Note: DGAC AD 96-147(A) refers.

            Compliance: Unless previously carried out, at the next scheduled aircraft maintenance inspection and thereafter, at every second disassembly of the pipes.

            Background: The manufacturer has advised that frequent removal and re-tightening of the tube fitting nuts located at the end of the fluid pipes has resulted in cracking of the tubing flares.