IAD98LA084

NTSB accident investigation · Beech BE24 · Beckley, WV · July 26, 1998

Accident · Minor injuriesLimited investigationFinal report
Date
July 26, 1998, 13:30 local (17:30 UTC)
Place
Beckley, WV
Injuries
1 minor
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N9711LBeech BE24
Weather
Visual (VMC) · Day
Status
Completed · report January 28, 2000
Report
Approved by Office Director
FAA report
19980726017759A
Case key
43525

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

The pilot's mismanagement of the fuel supply in that the fuel selector was selected to the improper fuel tank, which resulted in fuel starvation and the loss of engine power.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine power(total) - nonmechanicalCruise
Fuel management - inadequatePilot in commandCause
Fluid,fuel - starvation
Fuel tank selector position - improperPilot in commandCause
Forced landingDescent - emergency
In flight collision with terrain/waterEmergency descent/landing
Object - tree(s)
Terrain condition - water

Analysis

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.

Factual narrative

On July 26, 1998 at 1330 eastern daylight time, a Beech BE 24, N9711L, was substantially damaged during a forced landing to the Glade Springs Resort, Beckley, West Virginia. The certificated commercial pilot received minor injuries. Visual meteorological conditions prevailed for the personal flight that originated at the Raleigh County Memorial Airport (BKW), Beckley, West Virginia, approximately 1300. No flight plan was filed for the flight conducted under 14 CFR Part 91.

In a telephone interview, a Federal Aviation Administration (FAA) Aviation Safety Inspector stated he had interviewed the pilot. According to the Inspector, the purpose of the flight was to charge the airplane's battery. The pilot reported he was in cruise flight, approximately 15 minutes after departing Beckley, when the engine started "...surging and sputtering." The pilot reported he turned for the Raleigh County 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.

After the accident, the pilot was interviewed by a Trooper of the West Virginia State Police. According to the Trooper's report:

"The engine stopped running at about 4,000 feet. He was attempting to land on the fairway of Glade Springs Golf course. The plane hit some trees and lost part of the left wing. The plane came to rest in a pond. The plane was totally covered by the water. Mr. Hicks had to swim to the bank."

The airplane remained submerged for approximately 48 hours. Recovery of the wreckage was supervised by two FAA Aviation Safety Inspectors. In a written statement, one Inspector said their 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. Further examination revealed the left tank contained approximately 27 gallons of fuel and an unknown quantity of water. According to the Inspector, the left and right fuel tanks had a capacity of 29.9 gallons each.

The pilot reported he had 30 gallons of fuel on board at last takeoff.

The propeller was turned by hand and continuity was established through the power train to the accessory section. 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 fuel records revealed the airplane's most recent fuel service was for 23 gallons of fuel on May 30, 1998. The pilot reported to the FAA Aviation Safety Inspectors that the airplane accumulated approximately two hours of flight time after the service.

Aircraft

Registration
N9711L
Reported as
Beech BE24
Category
Airplane
Serial number
MC-124
Engine
Lycoming O-360-A1B, 200 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Dorse L Hicks
Airworthiness certificate
Standard, Normal
Last inspection
Annual · October 14, 1997
Departed
BKW · WV

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
59
Certificate
Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
6,600 total · 30 in this make and model · 100 in the last 90 days · 30 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
Variable at 4 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
81 °F, dew point 54 °F
Altimeter
30.00 inHg
Observed at
BKW, 3 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.