Service difficulty report · O-Ring · Cndair CL6002B19

Difficulty date
December 7, 2000
Submitted
January 19, 2001
Operation
General aviation
Make and model
Cndair CL6002B19
Engine
Ge CF343B1
Part
O-Ring
Part number
6078T55P13
Condition
Leaking
Location
Throttle Body
Part time
3,265 hours
Component
Throttle Body · Woodward · 6078T55P13
Stage of operation
IN
How discovered
V
Nature of condition
K
Precautionary procedure
K

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

(CAN) THE MAINTENANCE WAS DOING AN ENGINE RUN WHEN THEY NOTICED A FUEL LEAK THROUGH THE LT CORE COWL DRAIN.THE MAINTENANCE OPENED THE LOWER CORE COWL AND THEY FOUND THAT THE FUEL WAS LEAKING THROUGH THE LT MFC THROTTLE SHAFT BODY WITH THE STANDBY FUEL PUMPS ON. THE MFC WAS REPLACED. 2001-01-03TC: MANUFACTURE OF AIRCRAFT AND ENGINE HAS DISCUSSED SDR WITH TC.FAA ASB PENDING, AND AIRWORTHINESS LIMITATION SECTION BEING REVISED IN TYPE CERTIFICATE.THIS OCCURRENCE IS ASSOCIATED WITH SDR 20010102009