Service difficulty report · Flow Divider · Cessna 560CESSNA

Difficulty date
November 12, 2008
Submitted
June 5, 2009
Operation
Air carrier
Aircraft
N302QS
Make and model
Cessna 560CESSNA
Aircraft serial
5600402
Aircraft time
10,013 hours, 8,223 cycles
Engine
Pwa JT15D5
Part
Flow Divider
Condition
Misrigged
Location
Rt Engine
Stage of operation
LD
How discovered
O
Nature of condition
X, J
Precautionary procedure
O

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

What was found

RT ENGINE QUIT ON LANDING ROLL OUT. ENGINE QUIT WHEN RT THROTTLE WAS BROUGHT TO IDLE. RT THROTTLE SEEMS TO HAVE AN EXCESSIVE AMOUNT OF SLOP WHEN BROUGHT BACK TO IDLE THRUST. VERIFIED DISCREPANCY, FOUND RT ENGINE CONTROLS AT FCU AND FUEL FLOW DIVIDER IMPROPERLY RIGGED. FOUND FCU CONTROL LEVER MIS CLOCKED. PERFORMED ONE COMPLETE RIGGING OF FCU AND FFD AS REQUIRED. PERFORMED ENG RUN AND RAPID ACCELERATION, ALL CHECK SATISFACTORY. ALL DONE IAW MM 76-11-00, 71-00-00. REPLACED OIL FILTER PN 3119604-01 AND FILTER ELEMENT PN 3059779-01.