Document ID: chunk:federal_register_of_legislation:F2006B11130:body:0
Version: federal_register_of_legislation:F2006B11130
Segment Type: other
Provision Reference: 
Character Range: 0–824

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/14
 Amdt 1

      Upper Cabin Door Locking Mechanism - Inspection And Modification

 2/80

            Applicability: All models 23, 24 and 25 with S/Nos. 23-003 to 23-099, 24-100 to 24-356 and 25-003 to 25-238, with 36 inch cabin door.

 Document: Gates Learjet SB 23/24/25-280A.

            Compliance: Within 100 hours time in service after achieving 3000 hours time in service and thereafter as per requirement document or until Gates Learjet Modification Kit No. AMK 78-2 is fitted.

            Background: Failure of the door locking mechanism during door closing can result in a hidden door unsafe condition.