ATL86LA236

NTSB accident investigation · Enstrom F-28C · Coshocton, OH · September 1, 1986

Accident · No injuriesLimited investigationFinal report
Date
September 1, 1986, 11:50 local (15:50 UTC)
Place
Coshocton, OH
Injuries
3 uninjured
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N549HEnstrom F-28C
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19860901043529A
Case key
7175

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.

Miscellaneous/otherTakeoff - initial climb
Planning/decision - improperPilot in commandCause
Terrain condition - high obstruction(s)Factor
Collective - excessivePilot in commandCause
Throttle/power control - improper use ofPilot in commandCause
Aircraft performance,climb capability - other
Rotor rpm - not maintainedPilot in commandCause
In flight collision with terrain/waterTakeoff

Analysis

The plt initiated a maximum power takeoff from a confined parking lot with 2 passengers on board. The area was boardered by obstructions & people. The plt rprtd that during lift-off, she increased power to 2900 RPM, lifted off to a 4' hover with 33' of manifold pressure, then began a max performance takeoff, 'pulling power and turning throttle' for extra RPM with slow forward speed, reaching 36' of manifold pressure. At aprx 15' AGL, the plt noted a decrease in RPM. She increased throttle application, then decreased the collective, but was unable to recover the loss of RPM. She made a left pedal turn to avoid obstructions & people. Subsequently, the helicopter touched down hard & was damaged. An exam of the eng did not reveal any defects. The flt manual warned that loss of rotor & eng RPM would follow when the eng was overboosted. At 36.5' of manifold pressure, the pop-off valve would have activated which would have resulted in a slight power loss.

Aircraft

Registration
N549H
Reported as
Enstrom F-28C
Category
Helicopter
Serial number
345
Airframe hours
1,132
Engine
Lycoming HIO-360-E1AD, 205 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Trans Rotor, Inc.
Airworthiness certificate
Standard, Normal
Last inspection
Annual · April 11, 1986 · 68 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
33
Certificate
Commercial
Airplane ratings
Single-engine land
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Right
Flight hours
412 total · 388 in this make and model · 291 as pilot in command · 35 in the last 90 days · 7 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
150° at 9 knots
Visibility
7 statute miles
Lowest ceiling
1,700 ft overcast
Temperature
70 °F, dew point 61 °F
Altimeter
30.00 inHg
Observed at
ZZV, 20 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.