19980615016139A

Accident · Substantial damage

FAA accident report · Cessna T210M · Lapine, OR · June 15, 1998

Date
June 15, 1998 · 17:43 local
Place
Lapine, OR
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N22CT
NTSB investigation
NTSBSEA98LA099
Reported as
Cessna T210M
Reported engine
Continental TSIO520R
Fatal injuries
0
Pilot’s flight hours
1,670 total32 in this make and model63 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.

(.4)The pilot stated that while in cruise flight at 10,500 feet MSL, the engine slowly lost power and then quit approximately two hours after takeoff, shortly after switching from the right fuel tank to the left fuel tank. She said she used the emergency check list, switched tanks, and attempted to restart the engine on both the left and right tanks, without success. She provided a fueling invoice for 71.2 gallons of fuel, with 39.6 in the right tank and 31.6 in the left tank, for refueling accomplished on the day before the accident. FAA inspectors found the fuel system to be uncompromised, except for the tanks, which had been breached during the accident. The left side sump tank contained approximately 98 ounces of fuel; the right sump tank appeared to be empty. The fuel injection spider contained fuel and the screen was clean. The firewall fuel strainer contained approximately 2 ounces of fuel and its screen was clean. At the time of inspection, the fuel totalizer was energized and gave a momentary reading of 41.3 gallons used. No anomalies were found during the post-accident investigation that would preclude normal operation of the engine. (-23) no narrative.

As the FAA filed it

(.4)THE PILOT STATED THAT WHILE IN CRUISE FLIGHT AT 10,500 FEET MSL, THE ENGINE SLOWLY LOST POWER AND THEN QUIT APPROXIMATELY TWO HOURS AFTER TAKEOFF, SHORTLY AFTER SWITCHING FROM THE RIGHT FUEL TANK TO THE LEFT FUEL TANK. SHE SAID SHE USED THE EMERGENCY CHECK LIST, SWITCHED TANKS, AND ATTEMPTED TO RESTART THE ENGINE ON BOTH THE LEFT AND RIGHT TANKS, WITHOUT SUCCESS. SHE PROVIDED A FUELING INVOICE FOR 71.2 GALLONS OF FUEL, WITH 39.6 IN THE RIGHT TANK AND 31.6 IN THE LEFT TANK, FOR REFUELING ACCOMPLISHED ON THE DAY BEFORE THE ACCIDENT. FAA INSPECTORS FOUND THE FUEL SYSTEM TO BE UNCOMPROMISED, EXCEPT FOR THE TANKS, WHICH HAD BEEN BREACHED DURING THE ACCIDENT. THE LEFT SIDE SUMP TANK CONTAINED APPROXIMATELY 98 OUNCES OF FUEL; THE RIGHT SUMP TANK APPEARED TO BE EMPTY. THE FUEL INJECTION SPIDER CONTAINED FUEL AND THE SCREEN WAS CLEAN. THE FIREWALL FUEL STRAINER CONTAINED APPROXIMATELY 2 OUNCES OF FUEL AND ITS SCREEN WAS CLEAN. AT THE TIME OF INSPECTION, THE FUEL TOTALIZER WAS ENERGIZED AND GAVE A MOMENTARY READING OF 41.3 GALLONS USED. NO ANOMALIES WERE FOUND DURING THE POST-ACCIDENT INVESTIGATION THAT WOULD PRECLUDE NORMAL OPERATION OF THE ENGINE. (-23) NO NARRATIVE.

NTSB investigation

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