- Date
- August 16, 1994, 18:28 local (22:28 UTC)
- Place
- Stewartsville, NJ
- Injuries
- 3 uninjured
- Damage
- Substantial damage
- Phase of flight
- Enroute
- Aircraft
- N13CMEnstrom F-28A
- Weather
- Visual (VMC) · Day
- Status
- Completed · report May 4, 1995
- Report
- Approved by Office Director
- FAA report
- 19940816021569A
- Case key
- 8959
From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.
On this page
Probable cause
The loss of engine power for undetermined reason.
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.
Analysis
While in cruise flight over rough uneven terrain, the helicopter's engine lost partial power and the pilot made an autorotation landing in a corn field. The pilot stated that due to uneven terrain, he '...made [the] decision to zero out airspeed during touchdown.' The pilot stated he leveled the helicopter and '...pulled collective to cushion.' During the landing a main rotor blade separated the tail boom from the fuselage. Examination of the helicopter did not disclose evidence of mechanical malfunction.
Factual narrative
On August 16, 1994, at 1828 eastern daylight time, a Enstrom F- 28A, N13CM, lost partial engine power during cruise flight. The pilot executed a precautionary landing into a field in Stewartsville, New Jersey. During the landing the tailboom was severed. The pilot and two passengers were not injured. Visual meteorological conditions prevailed. The local sightseeing flight departed the Warren County Fairgrounds, Warren County, New Jersey, and was conducted under 14 CFR Part 91.
The pilot reported, "Aircraft was over Reservoir when engine began to loose power. Excessive yawing of A/C began." He said he flew the helicopter over a field and began a descent down into the field. The pilot reported, "In my low Recon of these fields I noticed the fields were unimproved and made decision to zero out airspeed prior to touchdown...with tail rotor upslope and near zero airspeed, I leveled A/C and pulled collective to cushion. A/C settled vertically, upon touchdown [main rotor] blade flexed down and cut tailboom off."
Postaccident examination of the airframe and engine did not reveal any anomalies. The engine was started and ran with no anomalies noted. (See attached Inspector's Statement for details of examination).
Aircraft
- Registration
- N13CM
- Reported as
- Enstrom F-28A
- Category
- Helicopter
- Serial number
- 090
- Airframe hours
- 1,464
- Engine
- Lycoming HIO-360-E1AD, reciprocating
- Damage
- Substantial damage
- Flight
- Other work use · Part 91
- Registered owner
- Innovative Air Helicopter Inc.
- Airworthiness certificate
- Standard, Transport; Special, Experimental (Special); Standard, Normal
- Last inspection
- Continuous airworthiness · August 15, 1994 · 5 hours before
- Departed
- Warren County, NJ
- Destination
- NJ
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
- Certificates
- Foreign, Commercial, Airline transport, Student
- Airplane ratings
- Single-engine land, Single-engine sea
- Instrument ratings
- Helicopter
- Medical
- Class 2, Valid Medical--w/ waivers/lim
- Seat
- Left
- Flight hours
- 2,400 total · 100 in this make and model · 2,200 as pilot in command · 80 in the last 90 days · 50 in the last 30 days · 7 in the last 24 hours
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 260° at 5 knots
- Visibility
- 12 statute miles
- Lowest ceiling
- 22,000 ft overcast
- Temperature
- 75 °F, dew point 59 °F
- Altimeter
- 30.00 inHg
- Observed at
- ABE
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 N13CM · 2
Matched to the same aircraft by N-number and date.