CHI03LA184

NTSB accident investigation · Bell 47G-5A · Sandusky, MI · June 28, 2003

Accident · No injuriesLimited investigationFinal report
Date
June 27, 2003, 21:00 local (Jun 28, 2003, 01:00 UTC)
Place
Sandusky, MI
Injuries
3 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N8413DBell 47G-5A
Weather
Visual (VMC) · Day
Status
Completed · report November 25, 2003
Report
Approved by Office Director
Parties
FAA- Detroit FSDO
FAA report
20030627028979A
Case key
57357

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 failure of the ignition switch leading to an engine power loss in cruise flight and the subsequent high flare during autorotation. Factors contributing to the accident were the pilot's misjudgment of the landing flare and the unsuitable terrain encountered by the pilot on landing.

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
Ignition system,ignition switch - failureCause
Forced landingDescent - emergency
Hard landingEmergency landing
Flare - misjudgedPilot in commandFactor
Flare - highPilot in commandCause
Unsuitable terrain or takeoff/landing/taxi area - encounteredPilot in commandFactor

Analysis

The helicopter sustained substantial damage when it landed hard during an autorotation following an in-flight loss of engine power. The pilot reported the engine failed at approximately 400 feet above ground level while in cruise flight. The pilot noted he performed an autorotation but flared early to avoid a drainage ditch. The pilot stated the helicopter landed hard in a field. An inspection of the helicopter showed engine and flight control continuity. The spark plugs and exhaust tubes were clean and the fuel tanks contained fuel. The magnetos worked when tested independently of the ignition system. The inspection revealed that the ignition switch had an internal fault causing it to ground out the ignition system.

Factual narrative

On June 27, 2003, at 2100 eastern daylight time, a Bell 47G-5A helicopter, N8413D, operated by Adventure Helicopters Inc., sustained substantial damage during an autorotation following an in flight loss of engine power near Sandusky, Michigan. Visual meteorological conditions prevailed at the time of the accident. The airline transport pilot and his two passengers reported no injuries. The 14 CFR Part 91 business flight was not operating on a flight plan. The local flight departed a private helipad near Sandusky, Michigan, about 2100.

The pilot reported the engine failed at approximately 400 feet above ground level. The pilot noted he performed a 180-degree autorotation to the southwest. The pilot stated he thought "it was evident that [the helicopter was] going to land in a large drainage ditch. I elected to flare sooner than I wanted to avoid the ditch." The pilot reported the helicopter subsequently landed hard in a bean field.

A FAA airworthiness inspector conducted an on-scene inspection of the helicopter. The inspection showed engine and control surface continuity and all cylinders exhibited compression. Both fuel tanks contained fuel and the spark plugs and exhaust tubes were clean. The two magnetos worked independently. The inspection revealed that the ignition switch had an internal fault.

Aircraft

Registration
N8413D
Reported as
Bell 47G-5A
Category
Helicopter
Serial number
25091
Engine
Lycoming O435-B1A, 260 horsepower, reciprocating
Damage
Substantial damage
Flight
Business · Part 91
Registered owner
Adventure Helicopters Inc.
Airworthiness certificate
Standard, Normal
Departed
PVT · Sandusky, MI

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
51
Injuries
None
Certificates
Flight instructor, Airline transport
Airplane ratings
Single-engine land, Single-engine sea
Instrument ratings
Airplane, Helicopter
Medical
Class 2, Valid Medical--w/ waivers/lim
Last flight review
March 10, 2002
Seat
Left
Flight hours
10,617 total · 1,600 in this make and model · 10,345 as pilot in command · 70 in the last 90 days · 30 in the last 30 days · 4 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
230° at 7 knots
Visibility
10 statute miles
Lowest ceiling
10,000 ft overcast
Temperature
72 °F, dew point 48 °F
Altimeter
29.87 inHg
Observed at
BAX, 21 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.