AD/SWSA226/76 - Main Landing Gear Door Actuator
1AD/SWSA226/76 - Main Landing Gear Door Actuator
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/SWSA226/76 - Main Landing Gear Door Actuator.
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 Fairchild (Swearingen) SA226 and SA227 Series Aeroplanes
AD/SWSA226/76 Main Landing Gear Door Actuator 4/96
Applicability: Models SA226-T, SA226-T(B), SA226-AT and SA226-TC S/N range as specified in the requirement document.
Requirement: Unless previously carried out, action in accordance with Fairchild Aircraft Service Bulletin 226-32-059 dated February 14, 1991.
Note: FAA AD 95-25-07 amdt 39-9452 refers.
Compliance: Within 1000 hours time in service from 28 March 1996.
Background: The manufacturer has advised that if the gear door actuator is misrigged the gear doors may fail to open.