AD/DHC-3/1 - Rudder Quadrant, Rudder Pedal Linkage, Tail Wheel Assembly and Rear Fuselage
1AD/DHC-3/1 - Rudder Quadrant, Rudder Pedal Linkage, Tail Wheel Assembly and Rear Fuselage
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/DHC-3/1 - Rudder Quadrant, Rudder Pedal Linkage, Tail Wheel Assembly and Rear Fuselage.
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 DHC-3 (Otter) Series Aeroplanes
AD/DHC-3/1 Rudder Quadrant, Rudder Pedal Linkage, NK Tail Wheel Assembly and Rear Fuselage
Applicability: As detailed in Requirement Document.
Requirement: Action in accordance with De H Canada TNS Otter Nos 3 or 4, 6 and 9.
Note: Canadian AD 53-16 refers.
Compliance: Forthwith.