AD/BEECH 33/40 - Elevator Trim Tab Actuator
1AD/BEECH 33/40 - Elevator Trim Tab Actuator
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/BEECH 33/40 - Elevator Trim Tab 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 Beechcraft 33 and 35-33 (Debonair/Bonanza) Series Aeroplanes
AD/BEECH 33/40 Elevator Trim Tab Actuator 2/92
Applicability: Models and serial numbers as listed in Beechcraft Service Bulletin 2399. Requirement: Action in accordance with mandatory Beechcraft Service Bulletin 2399.
Note: FAA AD 91-17-01 Amdt 39-7099 refers.
Compliance: At the next scheduled inspection for Maintenance Release issue after 29 February 1992.
Background: There have been two fatal accidents reported, in which the elevator trim tab actuators were reversed following maintenance. The actions specified in this Directive are intended to prevent interchanging the right-hand and left-hand trim tab actuators that, if reversed, could result in loss of control of the aircraft.