AD/BELL 205/2 - Tail Rotor Yoke - Inspection
1AD/BELL 205/2 - Tail Rotor Yoke - Inspection
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/BELL 205/2 - Tail Rotor Yoke - 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 205 Series Helicopters
AD/BELL 205/2 Tail Rotor Yoke - Inspection 9/68
Applicability: All 205A models fitted with tail rotor yoke P/N 204-010-781-5 or 204-010-781-9.
Requirement: Inspect yoke assembly P/N 204-010-781-5 or 204-010-781-9 by magnetic particle method with particular emphasis on the threaded portion of the yoke spindle.
Maximum amperage 1400 amps. DC or 1100 amps. AC. Do not exceed 4200 ampere turns.
Compliance: At intervals not exceeding 100 hours time in service, after 1 September 1971.