AD/BELL 205/48 - Fuselage Main Beams Splice - Modification
1AD/BELL 205/48 - Fuselage Main Beams Splice - Modification
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/BELL 205/48 - Fuselage Main Beams Splice - 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
Bell Helicopter Textron 205 Series Helicopters
AD/BELL 205/48 Fuselage Main Beams Splice - Modification 4/80
Applicability: All model 205A-1 with S/Nos. 30001 to 30287 and 30289 to 30296. Documents: 1. Bell Technical Bulletin No. 205-79-34; or
- FAA AD 80-03-07 Amdt. 39-3681.
Compliance: Unless already accomplished, before 3 April 1980.
Background: At manufacture aluminium rivets were installed in the subject splice instead of Monel rivets.