AD/CL-600/7 - Horizontal Stabiliser Pitch Trim Actuator - Modification
1AD/CL-600/7 - Horizontal Stabiliser Pitch Trim Actuator - Modification
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/CL-600/7 - Horizontal Stabiliser Pitch Trim Actuator - 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 Bombardier (Canadair) CL-600 (Challenger) Series Aeroplanes
AD/CL-600/7 Horizontal Stabiliser Pitch Trim Actuator - Modification
Applicability: Pitch trim actuators as listed in requirement document. Document: Canadair Challenger Alert SB No. A600-0084.
Note: Canadian Dept. of Transport AD CF-82-05 refers.
Compliance: Before issue of Australian Certificate of Airworthiness.
3/83
Background: Pitch trim actuators are suspected of having possible loose motor drive gear pinions.
This could result in damage to internal control wiring.