AD/B727/138 - Main Cargo Door
1AD/B727/138 - Main Cargo Door
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/B727/138 - Main Cargo Door.
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 Boeing 727 Series Aeroplanes
AD/B727/138 Main Cargo Door 1/92
Applicability: Model 727 series as listed in the requirement document.
Requirement: Action in accordance with the technical requirements of FAA AD 91-22-04 Amdt 39-8064.
Note: Boeing SB 727-52-0142 refers.
Compliance: As specified in the requirement document with a revised effective date of 12 January 1992 for Australian Registered Aircraft.
Background: This AD arises from reports of worn latch cams and worn pressure relief door hinge fittings, and a report of a main cargo door that opened in flight. The effective date required by the FAA is extended by approximately one month.