AD/LEARJET/20 - Upper Cabin Door Lock Mechanism Bolts - Modification
1AD/LEARJET/20 - Upper Cabin Door Lock Mechanism Bolts - Modification
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Gates Learjet 24 & 25 Series Aeroplanes
AD/LEARJET/20 Upper Cabin Door Lock Mechanism
Bolts - Modification
Applicability: All model 24 with S/Nos. 24-100 to 24-357,
All model 25 with S/Nos. 25-003 to 25-291.
3/80
Requirement: Modify the upper cabin door lock mechanism bolts by installing Gates Learjet Kit No. AMK 79-9.
Compliance: Within 150 hours time in service after 30 April 1980.
Background: Modification kit AMK 79-9 provides an additional safety feature to the upper cabin door lock mechanism by installing drilled bolts and lockwiring these bolts in situ.