AD/ENST 28/8 - Fuselage Structure - Inspection
1AD/ENST 28/8 - Fuselage Structure - Inspection
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/ENST 28/8 - Fuselage Structure - 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 Enstrom F-28 Series Helicopters
AD/ENST 28/8 Fuselage Structure - Inspection 10/73
Applicability: All models.
Requirement: Visually inspect for cracks the fuselage structure in the vicinity of the main rotor transmission assembly attachment.
Compliance: Within 50 hours time in service after 17 October 1975 and thereafter at intervals not exceeding 100 hours time in service.