19960723019209A

Accident · Substantial damage

FAA accident report · Beech J35 · Lovelock, NV · July 23, 1996

Date
July 23, 1996 · 17:30 local
Place
Lovelock, NV
Phase of flight
Forced/Precautionary Landing
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N8399J
NTSB investigation
NTSBLAX96LA286
Reported as
Beech J35
Reported engine
Continental IO470C
Fatal injuries
0
Pilot’s flight hours
5,200 total200 in this make and model36 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.

Engine failed on takeoff and crashed. (.4)the pilot performed 8 or 9 touch-and-go landings, and after liftoff, at approximately 200 feet AGL, the engine lost power and quit. On previous takeoffs, at approximately 300 plus feet AGL, he would switch from the main fuel tank to the auxiliary tanks, fly out about 5 miles and return. During the downwind leg of the pattern he would switch from the auxiliary tanks back to the left main tank for the touch-and-go landing. He stated that he thought that he may have lost fuel flow when the engine quit; however, he did not visually check the fuel pressure gauge. Postaccident examination of the fuel distributor valve, fuel pump vapor return line, and the fuel pump outlet line revealed that they were dry. He reported that he had been airborne for approximately 1.5 hours.

As the FAA filed it

ENGINE FAILED ON TAKEOFF AND CRASHED. (.4)THE PILOT PERFORMED 8 OR 9 TOUCH-AND-GO LANDINGS, AND AFTER LIFTOFF, AT APPROXIMATELY 200 FEET AGL, THE ENGINE LOST POWER AND QUIT. ON PREVIOUS TAKEOFFS, AT APPROXIMATELY 300 PLUS FEET AGL, HE WOULD SWITCH FROM THE MAIN FUEL TANK TO THE AUXILIARY TANKS, FLY OUT ABOUT 5 MILES AND RETURN. DURING THE DOWNWIND LEG OF THE PATTERN HE WOULD SWITCH FROM THE AUXILIARY TANKS BACK TO THE LEFT MAIN TANK FOR THE TOUCH-AND-GO LANDING. HE STATED THAT HE THOUGHT THAT HE MAY HAVE LOST FUEL FLOW WHEN THE ENGINE QUIT; HOWEVER, HE DID NOT VISUALLY CHECK THE FUEL PRESSURE GAUGE. POSTACCIDENT EXAMINATION OF THE FUEL DISTRIBUTOR VALVE, FUEL PUMP VAPOR RETURN LINE, AND THE FUEL PUMP OUTLET LINE REVEALED THAT THEY WERE DRY. HE REPORTED THAT HE HAD BEEN AIRBORNE FOR APPROXIMATELY 1.5 HOURS.

NTSB investigation

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