AD/BEECH 56/21 - Control Surface Trim Tab Systems
1AD/BEECH 56/21 - Control Surface Trim Tab Systems
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/BEECH 56/21 - Control Surface Trim Tab Systems.
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 56TC (Turbo Baron) Series Aeroplanes
AD/BEECH 56/21 Control Surface Trim Tab Systems 6/80
Applicability: All models 56TC and A56TC with S/Nos. TG-2 to TG-94. Requirement: Action in accordance with Beechcraft SI No. 0846-152, Rev. 2.
Compliance: Within 100 hours’ time in service after 30 June 1980 and thereafter at intervals not exceeding 100 hours’ time in service.
Background: The inspection procedure defines maximum allowable control surface trim tab free play caused by accumulative wear in control linkage and actuators.