Document ID: chunk:federal_register_of_legislation:F2006B11139:body:0
Version: federal_register_of_legislation:F2006B11139
Segment Type: other
Provision Reference: 
Character Range: 0–583

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

 Gates Learjet 24 & 25 Series Aeroplanes

AD/LEARJET/22 Aft Engine Beam Pylon Bolts - Inspection 5/80

Applicability: All model 23 S/Nos. 23-003 to 23-099;

All model 24 S/Nos. 24-100 to 24-357;

            All model 25 S/Nos. 25-003 to 25-286 and 25-288.

 Document: Gates Learjet SB 23/24/25-299. Compliance: As per requirement document.
 Background: To ensure that the aft engine beam pylon bolts are secure and properly torqued.