19970821023219A

Accident · Substantial damage

FAA accident report · Beech H35 · Vacaville, CA · August 21, 1997

Date
August 21, 1997 · 17:05 local
Place
Vacaville, CA
Airport
Nuttree Airport
Phase of flight
Final Approach
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N4689D
NTSB investigation
NTSBLAX97LA298
Reported as
Beech H35
Reported engine
Continental O470G
People aboard
2
Fatal injuries
0
Pilot’s flight hours
185 total88 in this make and model3 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.

Aircraft engine quit on landing, landed short of runway. (.4)the pilot reported that the aircraft fuel gauges always read 'full,' so he checked his fuel visually and timed each tank. He stated that he took off with 38 gallons of fuel, with the fuel selector on the left tank, and switched to the right tank about 18 nautical miles from his final destination. While entering the traffic pattern, he heard a 'funny noise.' The pilot reported that he put the throttle forward but the engine didn't seem to respond. He retracted the flaps and turned for the runway. The aircraft crashed in a field approximately 1/4 mile from the end of the runway. The pilot repored to the police officer who responded to the site said he "blew it and ran out of gas.' An FAA inspector examined the aircraft. The fuel selector was in the 'off' position and fuel was present at the carburetor inlet when the line was removed. The fuel was drained from the aircraft. The right tip tank was empty, but had been damaged in the accident; the right auxiliary tank held about 9 gallons, and the right main tank held about 14 gallons. The left tip tank held about 2 gallons; the left auxiliary tank held 6.5 gallon s, and the left main tank held about 3/4 gallon. The inspector stated that the engine was examined and no mechanical problems were found. The aircraft pilot's operating handbook states that the carburetor returns aobut 3 gallons per hour of excess fuel. Fuel return lines are routed through the selector valve to the left main cell. The auxiliary cells and right main cell return fuel to the left main cell only.

As the FAA filed it

AIRCRAFT ENGINE QUIT ON LANDING, LANDED SHORT OF RUNWAY. (.4)THE PILOT REPORTED THAT THE AIRCRAFT FUEL GAUGES ALWAYS READ 'FULL,' SO HE CHECKED HIS FUEL VISUALLY AND TIMED EACH TANK. HE STATED THAT HE TOOK OFF WITH 38 GALLONS OF FUEL, WITH THE FUEL SELECTOR ON THE LEFT TANK, AND SWITCHED TO THE RIGHT TANK ABOUT 18 NAUTICAL MILES FROM HIS FINAL DESTINATION. WHILE ENTERING THE TRAFFIC PATTERN, HE HEARD A 'FUNNY NOISE.' THE PILOT REPORTED THAT HE PUT THE THROTTLE FORWARD BUT THE ENGINE DIDN'T SEEM TO RESPOND. HE RETRACTED THE FLAPS AND TURNED FOR THE RUNWAY. THE AIRCRAFT CRASHED IN A FIELD APPROXIMATELY 1/4 MILE FROM THE END OF THE RUNWAY. THE PILOT REPORED TO THE POLICE OFFICER WHO RESPONDED TO THE SITE SAID HE "BLEW IT AND RAN OUT OF GAS.' AN FAA INSPECTOR EXAMINED THE AIRCRAFT. THE FUEL SELECTOR WAS IN THE 'OFF' POSITION AND FUEL WAS PRESENT AT THE CARBURETOR INLET WHEN THE LINE WAS REMOVED. THE FUEL WAS DRAINED FROM THE AIRCRAFT. THE RIGHT TIP TANK WAS EMPTY, BUT HAD BEEN DAMAGED IN THE ACCIDENT; THE RIGHT AUXILIARY TANK HELD ABOUT 9 GALLONS, AND THE RIGHT MAIN TANK HELD ABOUT 14 GALLONS. THE LEFT TIP TANK HELD ABOUT 2 GALLONS; THE LEFT AUXILIARY TANK HELD 6.5 GALLON S, AND THE LEFT MAIN TANK HELD ABOUT 3/4 GALLON. THE INSPECTOR STATED THAT THE ENGINE WAS EXAMINED AND NO MECHANICAL PROBLEMS WERE FOUND. THE AIRCRAFT PILOT'S OPERATING HANDBOOK STATES THAT THE CARBURETOR RETURNS AOBUT 3 GALLONS PER HOUR OF EXCESS FUEL. FUEL RETURN LINES ARE ROUTED THROUGH THE SELECTOR VALVE TO THE LEFT MAIN CELL. THE AUXILIARY CELLS AND RIGHT MAIN CELL RETURN FUEL TO THE LEFT MAIN CELL ONLY.

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 N4689D · 1

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