LAX95LA216

NTSB accident investigation · Bell 47-G5 · Coalinga, CA · June 18, 1995

Accident · No injuriesLimited investigationFinal report
Date
June 17, 1995, 22:30 local (Jun 18, 1995, 05:30 UTC)
Place
Coalinga, CA
Injuries
1 uninjured
Damage
Destroyed
Phase of flight
Initial climb
Aircraft
N7923JBell 47-G5
Weather
Visual (VMC) · Night/dark
Status
Completed · report January 29, 1996
Report
Approved by Office Director
FAA report
19950617017369A
Case key
29122

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

clutch slippage for undetermined reasons. A factor in the accident was the helicopter's low above ground altitude, which limited the pilot's time and ability to recover main rotor rpm.

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.

Airframe/component/system failure/malfunctionTakeoff - initial climb
Rotor drive system,clutch assembly - slippedCause
Reason for occurrence undetermined
Rotor rpm - not correctedPilot in commandCause
Altitude - inadequateFactor
In flight collision with terrain/waterDescent - uncontrolled

Analysis

The pilot reported that he had just lifted off from a refueling truck and was returning to base at low altitude from applying chemicals to a field when he noted a split in the engine/rotor tachometer. The engine rpm's began to increase while the main rotor speed began to decay. He was attempting to correct the problem with collective and throttle manipulation when the helicopter collided with the ground. The helicopter was examined by an FAA airworthiness inspector. He reported that no abnormalities were noted with either the engine, the transmission, or the freewheeling unit. Heat discoloration and burned oil residue were noted on the clutch.

Factual narrative

On June 17, 1995, at 2230 hours Pacific daylight time, a Bell 47-G5 helicopter, N7923J, lost power to the main rotor and collided with crops while returning from an aerial application operation near Coalinga, California. The aircraft was operated by Breen Aviation, Inc., of Lemoore, California. Visual meteorological conditions prevailed at the time and no flight plan was filed. The helicopter was destroyed in the collision sequence. The certificated commercial pilot, the sole occupant, was not injured. The flight originated at a private strip near Huron, California, about 2200 hours as a local area agricultural application flight.

The pilot reported that he had just lifted off from a refueling truck and was returning to base from applying chemicals to a field when he noted a split in the engine/rotor tachometer. The engine rpm's began to increase while the main rotor speed began to decay. He was attempting to correct the problem with collective and throttle manipulation when the helicopter collided with the ground.

The helicopter was examined by a Federal Aviation Administration (FAA) airworthiness inspector from the Fresno, California, Flight Standards District Office. He reported that no abnormalities were noted with either the engine, the transmission, or the freewheeling unit. Heat discoloration and burned oil residue were noted on the clutch.

Aircraft

Registration
N7923J
Reported as
Bell 47-G5
Category
Helicopter
Serial number
25040
Airframe hours
7,733
Engine
Lycoming VO-435-B1A, 265 horsepower, reciprocating
Damage
Destroyed
Flight
Positioning · Part 91
Operator
Breen Aviation, Inc.
Registered owner
Gilbert Aviation
Airworthiness certificate
Special, Restricted (Special)
Last inspection
Annual · January 5, 1995 · 17 hours before
Departed
3CA4 · Huron, CA

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
Commercial
Airplane ratings
Single-engine land
Instrument ratings
Helicopter
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Center
Flight hours
5,800 total · 300 in this make and model

Weather

Conditions
Visual (VMC) · Night/dark
Wind
330° at 12 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
64 °F, dew point 45 °F
Altimeter
30.00 inHg
Observed at
NLC, 15 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.

Other investigations on N7923J · 4

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