AD/UH-1/2 - Tail Rotor Slider
1AD/UH-1/2 - Tail Rotor Slider
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/UH-1/2 - Tail Rotor Slider.
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 UH-1 Series Helicopters
AD/UH-1/2 Tail Rotor Slider 4/97 DM
Applicability: All models.
Requirement: Measure the outside diameter of the splined shaft (barrel) of the slider Part Number 204-010-720-3, or Part Number 204-010-720-003 at two points that are 90 apart on the outside circumference, at ½” to 1” from either end of the slider. Replace any slider which measures less than 1.300”.
Note: FAA AD 97-01-06 refers.
Compliance: Within 5 hours time in service after 12 February 1997.
Background: US Army “Breakout” spares of this item have been discovered with less than the minimum wall thickness. This Directive is to prevent a possible fatigue failure of a defective slider which would result in the loss of the tail rotor.