AD/CESSNA 210/65 - Fuel Line Chafing
1AD/CESSNA 210/65 - Fuel Line Chafing
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/CESSNA 210/65 - Fuel Line Chafing.
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 210 Series Aeroplanes
AD/CESSNA 210/65 Fuel Line Chafing 1/92 DM
Applicability: All Cessna 210 series with S/N 21059062 through 21064535, T210-0393 through T210-0454 and P21000001 through P21000760.
Requirement: Unless previously carried out action in accordance with Cessna Service Information Letter SE82-32. A minimum clearance of 6.5mm (0.25 inches) must be obtained between the fuel line/electrical wiring loom.
Note: FAA AD 91-22-01 Amdt 39-8061 refers.
Compliance: Within 50 hours time in service from 22 November 1991 or by 30 April 1992, whichever occurs first.
Background: Chafing of the fuel line by the wiring loom in the nose gear tunnel area could result in an inflight fire.