Service difficulty report · Tube · Beech F33A

Difficulty date
May 12, 2015
Submitted
May 12, 2015
Operation
General aviation
Aircraft
N6197U
Make and model
Beech F33A
Aircraft serial
CE987
Aircraft time
4,227 hours
Engine
Cont IO520BB
Engine time
1,675 hours
Propeller
Mcauly 2A36C23
Part
Tube
Part number
35921155129
Condition
Damaged
Location
Fuel System
Part time
4,227 hours
Stage of operation
TX
How discovered
O
Nature of condition
K, Y, R
Precautionary procedure
E

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

What was found

ENGINE RAN FINE ONE DAY, BUT NEXT DAY ALTHOUGH IT WOULD START, IT WOULD DIE AFTER JUST A FEW SECONDS. FOUND IT WOULD CONTINUE TO RUN ONLY IF BOOST PUMP WAS LEFT ON. ASSUMED ENGINE DRIVEN PUMP HAD FAILED. REPLACED ENGINE PUMP BUT PROBLEM PERSISTED. EVENTUALLY SECOND MECHANIC, SPOTTER, NOTICED FUEL LEAKING UNDER MID-FUSELAGE DURING TEST RUN, BUT AFTER SHUTDOWN COULD NOT FIND ANY EVIDENCE OF A FUEL LEAK. FIGURING IT MUST BE IN VICINITY OF FUEL SELECTOR AND/OR BOOST PUMP, THE COCKPIT CARPET AND SUB-FLOOR PLYWOOD PANELS WERE REMOVED AND BOOST PUMP WAS TURNED ON. FOUND FUEL SPRAYING INTO CABIN SIDEWALL AND INSULATION AND RUNNING DOWN INTO FLOOR STRUCTURE FROM LEAKING IN MAIN FUEL LINE FROM BOOST PUMP TO BACKSIDE OF FIREWALL. FUEL LINE APPEARS TO HAVE BEEN CHAFED AND/OR CORRODED DUE TO CONTACT WITH STEEL-WIRE SCAT VENTILATION DUCT BEHIND SIDEWALL UPHOLSTERY PANEL TO LEFT OF AND ABOVE PILOT'S LT RUDDER PEDAL. NOTE: AREA OF PROBLEM IS OUTSIDE OF NORMAL SCOPE OF ANNUAL OR 100-HOUR INSPECTIONS.

More about the Beech F33A