FTW92LA226

NTSB accident investigation · Bell 47-J2A · Booneville, AR · September 16, 1992

Accident · No injuriesLimited investigationFinal report
Date
September 16, 1992, 12:13 local (17:13 UTC)
Place
Booneville, AR
Injuries
3 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N291FWBell 47-J2A
Weather
Visual (VMC) · Day
Status
Completed · report August 26, 1993
Report
Approved by Office Director
FAA report
19920916037079A
Case key
18567

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

On this page

Probable cause

The pilot's failure to maintain adequate rotor RPM during autorotative landing. Factors were fuel exhaustion, the pilot's improper fuel consumption calculations, and the pilot not refueling the helicopter.

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
Fluid,fuel - exhaustionFactor
Refueling - not performedPilot in commandFactor
Fuel consumption calculations - improperPilot in commandFactor
Forced landingDescent - emergency
Autorotation - initiatedPilot in command
Miscellaneous/otherLanding - flare/touchdown
Misc rotorcraft,tail boom - separation
Adequate rotor rpm - not maintainedPilot in commandCause

Analysis

The pilot had flown the helicopter on the power line aerial observation flight for approximately 3 hours and 8 minutes when a power loss occurred. He initiated an autorotation to an open field. During the flare, he failed to maintain adequate rotor RPM and the main rotor blades severed the tailboom. The helicopter landed hard. The owner of the helicopter drained a small amount of fuel from the tanks and said that he was certain that lack of fuel caused the forced landing. The pilot performed a calculated fuel consumption check two days before the accident which he said showed a fuel burn rate of 13.7 gallons per hour or 3 hours and 47 minutes of flight time. He used a stop watch in the cockpit to account for flight time. The manufacturer states the fuel system holds 47.5 gallons of usable fuel, the engine's fuel burn rate is 19 gallons per hour at cruise, and lists the maximum cruise time as 3 hours and 18 minutes with the engine leaned.

Aircraft

Registration
N291FW
Reported as
Bell 47-J2A
Category
Helicopter
Serial number
3303
Airframe hours
5,494
Engine
Lycoming VO-540-B1B3, 260 horsepower, reciprocating
Damage
Substantial damage
Flight
Aerial observation · Part 91
Operator
Ruggles, Don C., doing business as Helicopter Southwest
Registered owner
Ruggles, Don C.
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · March 16, 1992 · 99 hours before
Departed
M39 · Mena, AR
Destination
4M2 · Booneville, AR

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
43
Certificate
Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane, Helicopter
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Front
Flight hours
8,134 total · 104 in this make and model · 7,035 as pilot in command · 186 in the last 90 days · 38 in the last 30 days · 4 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
180° at 5 knots
Visibility
7 statute miles
Lowest ceiling
None
Temperature
84 °F

FAA reports on this event · 1

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