AD/HU 269/29 - Tail Rotor Blade Assembly - Inspection
1AD/HU 269/29 - Tail Rotor Blade Assembly - Inspection
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/HU 269/29 - Tail Rotor Blade Assembly - 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
Image unavailable in extracted text Schweizer (Hughes) 269 Series Helicopters
AD/HU 269/29 Tail Rotor Blade Assembly - Inspection 12/68
Applicability: All models with tail rotor blade assemblies S/Nos up to and including 126-3312. Document: Hughes SIN N-58.
Compliance: Within 25 hours time in service after 9 December 1968 and thereafter at intervals not exceeding 25 hours time in service.