AD/B767/34 - Control Wheel Aids Transducer
1AD/B767/34 - Control Wheel Aids Transducer
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/B767/34 - Control Wheel Aids Transducer.
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 767 Series Aeroplanes
AD/B767/34 Control Wheel Aids Transducer 4/90
Applicability: All models listed in the referenced Service Bulletin. Requirement: Action in accordance with Boeing Alert SB 767-31A-0029.
Note: FAA AD 89-24-05 also refers.
Compliance: Prior to 30 April 1990.
Background: Removal of the AIDS transducer is required to prevent binding of the control wheel.