FTW93FA008

NTSB accident investigation · Beech 95-B55B · Chatham, LA · October 8, 1992

Accident · FatalField investigationFinal report
Date
October 7, 1992, 21:33 local (Oct 8, 1992, 02:33 UTC)
Place
Chatham, LA
Injuries
1 fatal
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N153QBeech 95-B55B
Weather
Visual (VMC) · Night/dark
Status
Completed · report September 14, 1993
Report
Approved by Office Director
FAA report
19921007042989A
Case key
18577

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 inadvertent stall and spin. Factors were the power loss due to fuel starvation, the dark night, and his failure to use the boost pump for engine restart.

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 - normal
1 engine
Fluid,fuel - starvation
Fuel system,electric boost pump - not engagedPilot in commandFactor
Loss of control - in flightCruise - normal
Stall/spin - inadvertentPilot in commandCause
Light condition - dark nightFactor
In flight collision with terrain/waterDescent - uncontrolled

Analysis

The private pilot had previously made only one night cross-country flight as the only rated pilot in the airplane. Another pilot who usually served as a crew member reported that during the cruise portion of the second leg of his cross country flight, the pilot would normally run the engines on the auxiliary tanks until they were empty and then switch to the main fuel tanks and air start the engines. This procedure requires that the fuel boost pumps be in the 'on' position. The fuel boost pumps were in the 'off' position at the accident site. The right main fuel tank had ruptured and only four gallons of fuel remained. Twenty seven gallons of fuel remained in the left main tank. Each of the auxiliary tanks contained less than one pint of fuel. Witnesses three miles from the accident site reported a dark night. Engine test runs were performed on both engines throughout all power ranges and there were no anomalies found that would have contributed to the accident. A review of the air traffic control data revealed that the pilot declared an emergency and reported the airplane out of control in a flat spin. The pilot did not refuel prior to departing on the second leg of his night cross country flight.

Aircraft

Registration
N153Q
Reported as
Beech 95-B55B
Category
Airplane
Serial number
TC-761
Airframe hours
3,427
Engine
Continental IO-520-E2B, 300 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Larocca, Victor T.
Registered owner
Larocca, Victor T.
Airworthiness certificate
Standard, Normal
Last inspection
Annual · April 8, 1992 · 58 hours before
Departed
OM6 · Batesville, MS
Destination
BMT · Beaumont, TX

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
33
Certificate
Private
Airplane ratings
Single-engine land, Multi-engine land
Medical
Class 3, Valid Medical--no waivers/lim.
Seat
Left
Toxicology
Performed
Flight hours
629 total · 19 in this make and model · 558 as pilot in command · 17 in the last 30 days · 3 in the last 24 hours

Weather

Conditions
Visual (VMC) · Night/dark
Wind
150° at 7 knots
Visibility
8 statute miles
Lowest ceiling
8,000 ft broken
Temperature
64 °F, dew point 55 °F
Altimeter
29.00 inHg
Observed at
MLU, 28 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.