AD/TFE 731/6 - High Pressure Rotor and Nozzle Assembly Bolt - Replacement
1AD/TFE 731/6 - High Pressure Rotor and Nozzle Assembly Bolt - Replacement
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/TFE 731/6 - High Pressure Rotor and Nozzle Assembly Bolt - Replacement.
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 - 106 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text AlliedSignal (Garrett/AiResearch) Turbine Engines - TFE731 Series
AD/TFE731/6 High Pressure Rotor and Nozzle Assembly Bolt - Replacement
Applicability: TFE731-2-1C; TFE731-2-2B; TFE731-2-2J; TFE731-2-2L.
Document: AiResearch SB No. 72-3138, or AD/AIR-T/38.
3/86
Compliance: During the next hot end inspection completed after 30 September 1980 or during the next unscheduled exposure of the area, whichever occurs first.
Background: This Directive is issued to reduce the possibility of damaging the curvic coupling and the forward side of the H.P. turbine rotor by pieces of failed bolts.