BFO87FA057

NTSB accident investigation · Bell 206B · Washington, DC · August 21, 1987

Accident · FatalField investigationFinal report
Date
August 21, 1987, 07:36 local (11:36 UTC)
Place
Washington, DC
Injuries
3 fatal, 1 serious
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N83080Bell 206B
Weather
Visual (VMC) · Day
Status
Completed · report October 6, 1988
Report
Approved by Office Director
Case key
11291

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

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/malfHover
Fluid,oil - contaminationFactor
Turboshaft engine,gas generator turbine shaft - wornCause
Turboshaft engine,gas generator turbine shaft - fatigueCause
Forced landingDescent - emergency
In-flight planning/decision - improperPilot in commandFactor
Airspeed - reduced
Proper altitude - not maintained
Autorotation - not possible
In flight collision with terrain/waterDescent - emergency
Terrain condition - water

Analysis

The helicopter was on a LCL photography (sight-seeing) flt. While hovering at aprx 200' abv the potomac river, the eng lost pwr. The plt initiated an autorotation & deployed the emerg floats. Subsequently, the helicopter impacted in the river & rolled ovr, but was supported (upside down) in the water by the floats. After recovery, no preimpact part fail- ure or malfunction of the airframe was fnd. However, a teardown of the eng revealed the spur adapter gearshaft (sag), pn 6890482, had failed from wear & subsequent fatigue. The failure occurred at the fwd, splined end of the sag. Debris (82% silicon) was fnd inside the oil delivery tube. The oil jets for the #2 & #3 brgs were obstructed, but the jet for sag was not obstructed. The precise nature of the conds & circumstances that led to excessive wear was not determined. The height/velocity diagram in the flt manual showed hovering flt btn 10 & 400 ft should be avoided (to allow for successful autorotative lndg in the event of a pwr loss).

Aircraft

Registration
N83080
Reported as
Bell 206B
Category
Helicopter
Serial number
900
Airframe hours
3,421
Engine
Allison 250-C20, 317 horsepower, turbo shaft
Damage
Destroyed
Flight
Part 91
Operator
Stuart Aviation
Registered owner
Advest Credit Corporation
Airworthiness certificate
Standard, Normal
Last inspection
Annual · June 22, 1987 · 23 hours before
Departed
DCA · Washington, DC

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
38
Certificates
Airline transport, Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane, Helicopter
Medical
Class 1, Invalid Medical for flight
Seat
Left
Flight hours
7,100 total · 391 in this make and model · 6,500 as pilot in command · 6 in the last 90 days · 2 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
60° at 3 knots
Visibility
15 statute miles
Lowest ceiling
None
Temperature
75 °F, dew point 57 °F
Altimeter
30.00 inHg
Observed at
DCA, 1 nm away