20000909040509A

Accident · Substantial damage

FAA accident report · Cessna 120 · Sacramento, CA · September 9, 2000

Date
September 9, 2000 · 13:30 local
Place
Sacramento, CA
Airport
Sacramento Executive Airport
Phase of flight
Forced/Precautionary Landing
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N76261
NTSB investigation
NTSBLAX00LA332
Reported as
Cessna 120
Reported engine
AMTR O200
People aboard
1
Fatal injuries
0
Pilot’s flight hours
1,295 total500 in this make and model35 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) Engine quit during takeoff. (.4) during the takeoff climb the airplane lost power and collided with the tops of trees during the ensuing emergency landing. The pilot stated there were no mechanical anomalies noted with the preflight, or taxi to the active runway. Prior to takeoff, the airport closed for about 5 minutes. About 4 minutes after the airport reopened, the pilot was cleared for takeoff. After takeoff the engine rpm's dropped. He suspected carburetor icing and applied the carburetor heat. The engine continued to lose power. His intent was to land in-between trees on a golf course. At the last minute he had to maneuver the airplane to avoid a golf cart. He attempted to stall the airplane into the tops of the trees. Witnesses to the accident heard the engine sputtering. At the accident site fuel was found in the left tank, and on the ground underneath the right wing. The airframe and power plant were examined. The fuel selector was stiff to move and the main discharge nozzle was leaking and stained. The carburetor heat control cable retainer bolt washer, and the mixture control cable rod end retainer bolt were both loose. The c arburetor was inspected and found in noncompliance with airworthiness directives. No further mechanical anomalies were noted with the airframe, power plant, or carburetor. Conditions at the time of the accident were conducive to carburetor icing.

As the FAA filed it

(-23) ENGINE QUIT DURING TAKEOFF. (.4) DURING THE TAKEOFF CLIMB THE AIRPLANE LOST POWER AND COLLIDED WITH THE TOPS OF TREES DURING THE ENSUING EMERGENCY LANDING. THE PILOT STATED THERE WERE NO MECHANICAL ANOMALIES NOTED WITH THE PREFLIGHT, OR TAXI TO THE ACTIVE RUNWAY. PRIOR TO TAKEOFF, THE AIRPORT CLOSED FOR ABOUT 5 MINUTES. ABOUT 4 MINUTES AFTER THE AIRPORT REOPENED, THE PILOT WAS CLEARED FOR TAKEOFF. AFTER TAKEOFF THE ENGINE RPM'S DROPPED. HE SUSPECTED CARBURETOR ICING AND APPLIED THE CARBURETOR HEAT. THE ENGINE CONTINUED TO LOSE POWER. HIS INTENT WAS TO LAND IN-BETWEEN TREES ON A GOLF COURSE. AT THE LAST MINUTE HE HAD TO MANEUVER THE AIRPLANE TO AVOID A GOLF CART. HE ATTEMPTED TO STALL THE AIRPLANE INTO THE TOPS OF THE TREES. WITNESSES TO THE ACCIDENT HEARD THE ENGINE SPUTTERING. AT THE ACCIDENT SITE FUEL WAS FOUND IN THE LEFT TANK, AND ON THE GROUND UNDERNEATH THE RIGHT WING. THE AIRFRAME AND POWER PLANT WERE EXAMINED. THE FUEL SELECTOR WAS STIFF TO MOVE AND THE MAIN DISCHARGE NOZZLE WAS LEAKING AND STAINED. THE CARBURETOR HEAT CONTROL CABLE RETAINER BOLT WASHER, AND THE MIXTURE CONTROL CABLE ROD END RETAINER BOLT WERE BOTH LOOSE. THE C ARBURETOR WAS INSPECTED AND FOUND IN NONCOMPLIANCE WITH AIRWORTHINESS DIRECTIVES. NO FURTHER MECHANICAL ANOMALIES WERE NOTED WITH THE AIRFRAME, POWER PLANT, OR CARBURETOR. CONDITIONS AT THE TIME OF THE ACCIDENT WERE CONDUCIVE TO CARBURETOR ICING.

NTSB investigation

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