MIA98LA154

NTSB accident investigation · Bell 47G-2 · Fort Walton Bch, FL · May 9, 1998

Accident · Minor injuriesLimited investigationFinal report
Date
May 9, 1998, 15:00 local (20:00 UTC)
Place
Fort Walton Bch, FL
Injuries
3 minor
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N6714DBell 47G-2
Weather
Visual (VMC) · Day
Status
Completed · report February 15, 2001
Report
Approved by Office Director
FAA report
19980509008539A
Case key
38515

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 NTSB’s determination of the probable cause, and any contributing factors.

The loss of engine power for undetermined reasons.

Analysis

While in cruise flight at 500-600 feet the engine failed. A autorotation was performed and the helicopter touched down in 4-5 feet of water. After touchdown the waves rolled the helicopter to the right and the main rotor contacted the water and stopped. The pilot stated the helicopter contained about 20 gallons of fuel at the time of the accident. Examination of the engine and accessories showed no evidence of mechanical failure or malfunction. All fuel lines were found unobstructed.

Factual narrative

On May 9, 1998, about 1500 central daylight time, a Bell 47G-2, N6714D, registered to Penguin-Air Helicopters, Inc., ditched in the Gulf of Mexico, near Fort Walton Beach, Florida, following loss of engine power, while on a Title 14 CFR Part 91 sightseeing flight. Visual meteorological conditions prevailed at the time and no flight plan was filed. The helicopter received substantial damage and the commercial-rated pilot and two passengers received minor injuries. The flight originated from Fort Walton Beach, Florida, a few minutes before the accident.

The pilot stated that he had refueled the helicopter and had about 20 gallons of fuel onboard at the time of the accident. He had completed giving three rides. While on the fourth ride, over the Gulf of Mexico near Fort Walton Beach, at an altitude of 500-600 feet, the engine failed. He entered autorotation and touched down in 4-5 feet of water. The waves caused the helicopter to roll over to the right and the main rotor blades contacted the water and stopped. He and the two passengers then exited the helicopter.

Examination of the engine by a mechanic, under the supervision of an FAA inspector, showed the engine assembly rotated and continuity of the crankshaft, valve train, and all accessory drives gears was confirmed. The magneto switch operated normally and each magneto rotated. The magnetos would not fire due to water damage. The carburetor was opened and all ports were found unobstructed. All airframe and engine fuel lines were unobstructed.

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 powerCruise
Reason for occurrence undeterminedCause
DitchingDescent - emergency

Aircraft

Registration
N6714D
Reported as
Bell 47G-2
Category
Helicopter
Serial number
2199
Airframe hours
6,227
Engine
Lycoming VO-435-A1D, 260 horsepower, reciprocating
Damage
Substantial damage
Flight
Part 91
Registered owner
Penguin-Air Helicopter, Inc.
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · April 1, 1998 · 25 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
45
Certificate
Commercial
Instrument ratings
Helicopter
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
3,900 total · 800 in this make and model · 3,000 as pilot in command · 45 in the last 90 days · 20 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
160° at 6 knots
Visibility
4 statute miles
Lowest ceiling
None
Temperature
81 °F, dew point 72 °F
Altimeter
29.00 inHg
Observed at
DTS, 5 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 N6714D · 2

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