Service difficulty report · Bleed Valve · Cessna 560XL

Difficulty date
April 2, 2012
Submitted
September 14, 2015
Operation
General aviation
Make and model
Cessna 560XL
Engine
Pwa PW545A
Part
Bleed Valve
Condition
Faulty
Location
Engine
Stage of operation
TO
How discovered
O
Nature of condition
J
Precautionary procedure
C

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

What was found

(CAN) DURING DEPARTURE TAKEOFF POWER WAS SET FOR 3-5 SECONDS, LT ELECTRONIC ENGINE CONTROL ANNUNCIATOR ILLUMINATED AND ENGINE REVERTED TO MANUAL MODE, TAKEOFF WAS ABORTED AT 50 KNOTS. ACFT WAS SENT TO MFG, TROUBLESHOOTING ONGOING. PERFORMED GROUND RUN AND CAPTURED FAULT FI-01. DCU REPLACED AND BOTH DCU INITIALISED. BOV TM FOUND TO BE ROOT CAUSE FOR THE EEC REVERSION. NEW BOV TM INSTALLED.

More about the Cessna 560XL