FTW94LA166

NTSB accident investigation · Bell 47G · Sulphur, OK · May 18, 1994

Accident · No injuriesLimited investigationFinal report
Date
May 18, 1994, 18:30 local (23:30 UTC)
Place
Sulphur, OK
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N933BBell 47G
Weather
Visual (VMC) · Day
Status
Completed · report November 14, 1994
Report
Approved by Office Director
FAA report
19940518011819A
Case key
19061

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 loss of engine power due to the failure of an engine accessory oil pump gear. A factor was the lack of suitable terrain for the autorotation.

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) - mech failure/malfManeuvering - aerial application
Accessory drive assy,drive gear - failure,totalCause
Forced landingDescent - emergency
Hard landingDescent - emergency
Autorotation - initiatedPilot in command
Terrain condition - none suitableFactor
Object - tree(s)

Analysis

A total loss of engine power occurred at 50 feet above the ground during the initial phase of a turn-around maneuver. Trees hindered the pilot's completion of the autorotation. The helicopter bounced during the landing and the main rotor blade flexed and severed the tailboom. An examination of the engine by the operator revealed the failure of an engine accessory oil pump gear.

Factual narrative

On May 18, 1994, at 1830 central daylight time, a Bell 47G, N933B, sustained substantial damage during a forced landing near Sulphur, Oklahoma. The commercial pilot did not receive injuries. Visual meteorological conditions prevailed for the local aerial application flight.

The pilot reported a total loss of engine power at 50 feet above the ground during the initial phase of a turn-around maneuver. He further said that trees in the area and the height of the helicopter hindered his completion of a successful autorotation. The helicopter bounced during the hard landing and the main rotor blade flexed and severed the tailboom.

During a telephone interview the operator reported the total loss of engine power was due to the failure of the oil pump drive gear in the accessory case.

Aircraft

Registration
N933B
Reported as
Bell 47G
Category
Helicopter
Serial number
662
Engine
Franklin 6V-335-A, 210 horsepower, reciprocating
Damage
Substantial damage
Flight
Aerial application · Part 137
Registered owner
B & S Flying Service, Inc.
Airworthiness certificate
Special, Restricted (Special)
Last inspection
Annual · May 5, 1994 · 21 hours before

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
27
Certificate
Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Right
Flight hours
1,618 total · 1,164 in this make and model · 1,488 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
60° at 3 knots
Visibility
10 statute miles
Lowest ceiling
None

FAA reports on this event · 1

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

Other investigations on N933B · 1

Matched to the same aircraft by N-number and date.