AD/ENST 28/21 - Tail Rotor Blade Grip - Inspection and Modification
1AD/ENST 28/21 - Tail Rotor Blade Grip - Inspection and Modification
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/ENST 28/21 - Tail Rotor Blade Grip - Inspection and Modification.
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 Enstrom F-28 Series Helicopters
AD/ENST 28/21 Tail Rotor Blade Grip - Inspection
and Modification
5/79
Applicability: All models F-28C and 280C with Tail Rotor Blade Grip P/N 28-150013-1 wide chord.
Document: Enstrom Service Directive Bulletin No. 0048. Compliance: As per requirement document.
The Preflight Inspections may be carried out by the pilot in command in which case certification is not required.
Background: The manufacturer has received several field reports of crack indications being found in the wide chord tail rotor blade retentions grip.