20050312003239A

Accident · Substantial damage

FAA accident report · Cessna TU206G · Lancaster, TX · March 12, 2005

Date
March 12, 2005 · 12:30 local
Place
Lancaster, TX
Airport
Lancaster Airport
Phase of flight
Forced Landing
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N6211Z
NTSB investigation
NTSBDFW05CA087
Reported as
Cessna TU206G
Reported engine
Continental TSIO520*
People aboard
2
Fatal injuries
0
Pilot’s flight hours
24,500 total920 in this make and model2 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) Flight from addison, TX to Lancaster, TX upon entering upwind for landing on 17 PIC initiated a left turn and the power failed to respond. Emergency landing was made in a field. PIC stated he attempted to switch tanks and could not restart, manifold pressure was ambient. An engine test run was conducted at the salvage yard and the engine ran very well. The mechanic running the engine stated that the electrical fuel pump was cavitation when first attempting to start due to air in the system. The system had air induced into the fuel lines and there was not ample time to purge the air using the boost pump.

As the FAA filed it

(-23) FLIGHT FROM ADDISON, TX TO LANCASTER, TX UPON ENTERING UPWIND FOR LANDING ON 17 PIC INITIATED A LEFT TURN AND THE POWER FAILED TO RESPOND. EMERGENCY LANDING WAS MADE IN A FIELD. PIC STATED HE ATTEMPTED TO SWITCH TANKS AND COULD NOT RESTART, MANIFOLD PRESSURE WAS AMBIENT. AN ENGINE TEST RUN WAS CONDUCTED AT THE SALVAGE YARD AND THE ENGINE RAN VERY WELL. THE MECHANIC RUNNING THE ENGINE STATED THAT THE ELECTRICAL FUEL PUMP WAS CAVITATION WHEN FIRST ATTEMPTING TO START DUE TO AIR IN THE SYSTEM. THE SYSTEM HAD AIR INDUCED INTO THE FUEL LINES AND THERE WAS NOT AMPLE TIME TO PURGE THE AIR USING THE BOOST PUMP.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.

Other reports on N6211Z · 1

Matched to the same aircraft by N-number and date.