AD/LEARJET 35/13 - Upper Cabin Door Lock Mechanism Bolts - Modification
1AD/LEARJET 35/13 - Upper Cabin Door Lock Mechanism Bolts - Modification
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/LEARJET 35/13 - Upper Cabin Door Lock Mechanism Bolts - Modification.
meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-generator: Aspose.Words for .NET 22.10.0
?xml version="1.0" encoding="utf-8" standalone="no"?>
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 35 and 36 Series Aeroplanes
AD/LEARJET 35/13 Upper Cabin Door Lock Mechanism Bolts - Modification
Applicability: All model 35 with S/Nos. 35-001 to 35-274 and 278;
All model 36 with S/Nos. 36-001 to 36-044.
4/80
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.