AD/BELL 206/39 - Nut P/N 1022A14 Main Rotor Hub Latch Bolt and Blade Retention Bolt - Inspection
1AD/BELL 206/39 - Nut P/N 1022A14 Main Rotor Hub Latch Bolt and 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 206/39 - Nut P/N 1022A14 Main Rotor Hub Latch Bolt and 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
Image unavailable in extracted text Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters
AD/BELL 206/39 Nut P/N 1022A14 Main Rotor Hub Latch Bolt
and Blade Retention Bolt - Inspection
Applicability: All models delivered prior to 20 November 1972. Document: Bell SB No. 206-24, or Agusta SB No. BT206-56.
1/73
Compliance: 1. Visual Inspection - At each daily or overnight inspection after 15 December 1972 until the magnetic particle inspection is performed.
- Magnetic Particle Inspection - within 25 hours time in service after 15 December 1972.
Background: AD/Agusta 206/28 equivalent.