AD/BELL 206/11 - Main Rotor Blade Retention Bolt - Inspection
1AD/BELL 206/11 - Main Rotor Blade Retention Bolt - Inspection
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/BELL 206/11 - Main Rotor Blade Retention Bolt - Inspection.
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
Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters
AD/BELL 206/11 Main Rotor Blade Retention Bolt - Inspection 2/69
Applicability: All model 206A prior to S/Nos. 175 and AB-206A prior to S/No. 8080, plus spare blade retention bolts P/N | 206-010-152-1.
Document: Bell SL No. 206A-55.
Note: Agusta SB No. BT206-21 refers.
Compliance: Within 100 hours time in service after 14 Feb. 1969 for installed bolts, and before installation in an aircraft for replacement bolts.
Background: AD/Agusta 206/3 equivalent.