AD/CESSNA 400/36 - Wing Leading Edge Fuel Line - Inspection
1AD/CESSNA 400/36 - Wing Leading Edge Fuel Line - Inspection
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/CESSNA 400/36 - Wing Leading Edge Fuel Line - 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 Cessna 400 Series Aeroplanes
AD/CESSNA 400/36 Wing Leading Edge Fuel Line - Inspection 8/73
Applicability: All models 401 and 402 with S/Nos. below 401-0135 and 402-0135, fitted with turbocharger cooling duct P/N S1053E20T and fuel line P/N 5200106-55.
Requirement: 1. For aircraft fitted with wing leading edge turbocharger cooling flexible ducts - Through access panel No. 43, inspect fuel line P/N 5200106-55 for chafing by flexible duct P/N S1053E20T.
- Rectify any chafing and ensure adequate clearance is maintained by realignment of flexible duct.
Compliance: Before 1 October 1973.