ATL92FA013

NTSB accident investigation · Beech 58 · Pelham, AL · October 22, 1991

Accident · Serious injuriesField investigationFinal report
Date
October 21, 1991, 21:10 local (Oct 22, 1991, 02:10 UTC)
Place
Pelham, AL
Injuries
1 serious
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N99CKBeech 58
Weather
Visual (VMC) · Night/dark
Status
Completed · report February 8, 1993
Report
Approved by Office Director
FAA report
19911021051139A
Case key
8485

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 failure to correct the position of the fuel selector before takeoff, and her inattentiveness to fuel consumption during the flight, which resulted in fuel starvation. Factors were the non-performance of engine out emergency procedures and the dark, night conditions.

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) - nonmechanicalDescent - normal
All engines
Light condition - dark nightFactor
Fluid,fuel - starvationCause
Fuel tank selector position - not correctedPilot in commandCause
Self-induced pressurePilot in command
In-flight planning/decision - inattentivePilot in commandCause
Emergency procedure - not performedPilot in commandFactor
Forced landingDescent - emergency
In flight collision with terrain/waterDescent - emergency
Terrain condition - ditchFactor

Analysis

The airplane had been fueled to capacity then flown on multiple flights. At the last stop 18 gallons of fuel was added to each wing tank, which gave 60 gallons total, the pilot said. As the pilot prepared to leave, the left fuel boost pump was discovered to be inoperative. The pilot told a mechanic that she tried to start the left engine by placing the left fuel selector on the left engine & the right fuel selector to crossfeed. Since the right boost pump is downstream, between the right engine & the fuel selector, it would not pressurize fuel to the left engine. The left boost pump was replaced & the pilot departed. Approaching the destination the pilot reported a loss of engine power & crashed in an open field. The throttle quadrant was not set for an engine malfunction. No fuel was found in the left wing tank. The left fuel selector was in the left tank position and the right fuel selector was in the crossfeed position, so that both engines would have been fed from the left wing tank.

Aircraft

Registration
N99CK
Reported as
Beech 58
Category
Airplane
Serial number
TH-1125
Airframe hours
3,646
Engine
Continental IO-520-CB, 285 horsepower, reciprocating
Damage
Substantial damage
Flight
Executive/Corporate · Part 91
Operator
Green Hills Aviation Co., Inc.
Registered owner
Green Hills Aviation Co., Inc.
Airworthiness certificate
Standard, Normal
Last inspection
Annual · May 2, 1991 · 70 hours before
Departed
PFN · Panama City, FL
Destination
BHM · Birmingham, AL

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
35
Certificate
Airline transport
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
4,435 total · 742 in this make and model · 3,396 as pilot in command · 82 in the last 90 days · 36 in the last 30 days · 4 in the last 24 hours

Weather

Conditions
Visual (VMC) · Night/dark
Wind
120° at 5 knots
Visibility
7 statute miles
Lowest ceiling
None
Temperature
68 °F, dew point 57 °F
Altimeter
30.00 inHg
Observed at
BHM, 14 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.