CHI84LA279

NTSB accident investigation · Bell 47G2 · Detroit, MI · July 4, 1984

Accident · Serious injuriesLimited investigationFinal report
Date
July 4, 1984, 16:15 local (20:15 UTC)
Place
Detroit, MI
Injuries
3 serious
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
CFISHBell 47G2
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
Case key
12685

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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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(partial) - nonmechanicalManeuvering
Ignition system,spark plug - corrodedCause
Ignition system,spark plug - wornCause
Throttle/power control - reducedPilot in commandFactor
Pilot in commandFactor
PanicPilot in commandFactor
Forced landingDescent - emergency
Autorotation - attemptedPilot in command
Adequate rotor rpm - not maintainedPilot in commandCause
Throttle/power control - improper use ofPilot in commandCause
In flight collision with terrain/waterLanding - flare/touchdown
Terrain condition - water,roughFactor
Landing gear,float assembly - burstFactor

Analysis

The acft landed in the Detroit river after the engine sputtered and the acft vibrated. The plt reduced pwr & collective and pushed the cyclic forward. The RPM reduced from 3000 to 2500 but the rotor and engine RPM remained married. The plt adjusted descent with collective, forward speed with cyclic and pulled all collective just prior to impact. The acft was at about 150 ft AGL when the engine sputtered. One passenger described a sputtering noise but said the engine was running until impact. Another passenger described the engine noise as a muffled misfiring sound. The passengers alsosaid the plt did not mention the problem to them and the helicopter seemed under control until impact. Post accident examination of the engine after recovery from the water showed that the spark plugs were worn and contained a heavy build-up of carbon and lead. Near the operators hanger were 5 sealed and 1 unsealed fuel drums with standing water on the tops. No other evidence was found to indicate any malfunction of the acft.

Aircraft

Registration
CFISH
Reported as
Bell 47G2
Category
Helicopter
Serial number
1522
Airframe hours
11,482
Engine
Lycoming VO-435-A1E, 240 horsepower, reciprocating
Damage
Destroyed
Flight
Business · Part 91
Registered owner
Arrow Smith Limited
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · May 17, 1984 · 59 hours before
Airport
DET · Detroit City

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
24
Certificate
Commercial
Medical
Class 1, Valid Medical--no waivers/lim.
Flight hours
218 total · 218 in this make and model · 147 as pilot in command · 122 in the last 90 days · 7 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
170° at 12 knots
Visibility
5 statute miles
Lowest ceiling
4,000 ft broken
Temperature
84 °F, dew point 68 °F
Altimeter
29.00 inHg
Observed at
DET, 6 nm away