19980726017759A

Accident · Substantial damage

FAA accident report · Beech A24R · Beckely, WV · July 26, 1998

Date
July 26, 1998 · 13:30 local
Place
Beckely, WV
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N9711L
NTSB investigation
NTSBIAD98LA084
Reported as
Beech A24R
Reported engine
Lycoming IO360A1B
Fatal injuries
0
Pilot’s flight hours
6,600 total30 in this make and model100 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.

Acft experienced engine failure during forced landing, the plane hit trees ripping off the left wing, acft totally submerged in pond, (.4) the airplane was in cruise flight, approximately 15 minutes after departure, when the engine started to surge and sputter. The pilot turned to the departure airport and initiated a climb. He said he changed the fuel selector from the right tank position to the left, but `...nothing happened.' He moved the fuel selector back to the right tank, and selected a golf course for a forced landing site where the airplane struck trees and came to rest in a pond. Examination of the wreckage revealed that the right fuel tank was completely empty, not contaminated by water, and that the fuel selector was in the right tank position. The left tank contained approximately 27 gallons of fuel and an unknown quantity of water. The pilot reported he had 30 gallons of fuel on board at takeoff. The fuel system was examined and no evidence of fuel was found in the engine-driven fuel pump, fuel injector, or flow divider manifold. No evidence of fuel was found in the fuel line to the fuel pressure gauge. Examination of records revealed the airplane's most recent fuel service was for 23 gallons of fuel and that the airplane accumulated approximately 2 hours of flight time after the service.

As the FAA filed it

ACFT EXPERIENCED ENGINE FAILURE DURING FORCED LANDING, THE PLANE HIT TREES RIPPING OFF THE LEFT WING, ACFT TOTALLY SUBMERGED IN POND, (.4) THE AIRPLANE WAS IN CRUISE FLIGHT, APPROXIMATELY 15 MINUTES AFTER DEPARTURE, WHEN THE ENGINE STARTED TO SURGE AND SPUTTER. THE PILOT TURNED TO THE DEPARTURE AIRPORT AND INITIATED A CLIMB. HE SAID HE CHANGED THE FUEL SELECTOR FROM THE RIGHT TANK POSITION TO THE LEFT, BUT `...NOTHING HAPPENED.' HE MOVED THE FUEL SELECTOR BACK TO THE RIGHT TANK, AND SELECTED A GOLF COURSE FOR A FORCED LANDING SITE WHERE THE AIRPLANE STRUCK TREES AND CAME TO REST IN A POND. EXAMINATION OF THE WRECKAGE REVEALED THAT THE RIGHT FUEL TANK WAS COMPLETELY EMPTY, NOT CONTAMINATED BY WATER, AND THAT THE FUEL SELECTOR WAS IN THE RIGHT TANK POSITION. THE LEFT TANK CONTAINED APPROXIMATELY 27 GALLONS OF FUEL AND AN UNKNOWN QUANTITY OF WATER. THE PILOT REPORTED HE HAD 30 GALLONS OF FUEL ON BOARD AT TAKEOFF. THE FUEL SYSTEM WAS EXAMINED AND NO EVIDENCE OF FUEL WAS FOUND IN THE ENGINE-DRIVEN FUEL PUMP, FUEL INJECTOR, OR FLOW DIVIDER MANIFOLD. NO EVIDENCE OF FUEL WAS FOUND IN THE FUEL LINE TO THE FUEL PRESSURE GAUGE. EXAMINATION OF RECORDS REVEALED THE AIRPLANE'S MOST RECENT FUEL SERVICE WAS FOR 23 GALLONS OF FUEL AND THAT THE AIRPLANE ACCUMULATED APPROXIMATELY 2 HOURS OF FLIGHT TIME AFTER THE SERVICE.

NTSB investigation

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