- Date
- September 27, 2001, 12:30 local (17:30 UTC)
- Place
- Park Rapids, MN
- Injuries
- 4 minor
- Damage
- Substantial damage
- Phase of flight
- Maneuvering
- Aircraft
- N56MCBell 206B-III
- Weather
- Visual (VMC) · Day
- Status
- Completed · report March 30, 2004
- Report
- Approved by Office Director
- Parties
- Rolls-Royce Corporation, Bell Helicopter Textron Inc., Federal Aviation Administration
- FAA report
- 20010927026439A
- Case key
- 53525
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 pilot not maintaining altitude/clearance when he maneuvered above the glassy lake. A factor to the accident was the glassy lake condition.
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
The helicopter sustained substantial damage on impact with water while maneuvering over a glassy lake. The pilot stated, "Potato Lake selected for low altitude water/shoreline footage. Did high recon, no observed boat traffic in conflict with flight path over water at approx 40 to 50 ft. Commenced with descent profile of 80 mph and 600 [feet per minute]. The descent was to continue until treetop level then terminate descent and cruise over water for length of lake. Flight path was south to north with planned airspeed of 60 - 80 mph, then climb out. Reached target altitude confirmed with left and right shoreline sight picture, raised collective pitch with [simultaneous] forward cyclic pressure to commence over water cruise. Engine appeared non-responsive to power demand. Descent was not arrested. Added additional collective, no response to power demand. Leveled aircraft and impacted water with forward velocity." The front left seat passenger stated, "The pilot did not give us any pre-flight safety briefing or instructions. The pilot did not demonstrate or explain how to use the seat belts or how to egress from the helicopter in case of an emergency. ... Shortly after takeoff, I noticed were flying very low over the lake. Suddenly the helicopter abruptly dove down nose first crashing into the lake. The helicopter quickly began to sink into the water. ... I could not unbuckle the safety harness strap. My clothing was getting very heavy and I began to swallow water uncontrollably. I thought I was going to die. I continued to unsuccessfully struggle with the safety harness. Finally, somehow, I was able to wiggle out of the buckled safety harness." Wind was calm, sky condition clear, and the temperature was 20 degrees C. An on-scene investigation of the recovered wreckage revealed no pre-impact anomalies. A study of an on-board video revealed sounds consistent with the gas producer section of the engine and the main rotor system. Both rear passengers were not wearing their seat belts.
Factual narrative
History of flight
On September 27, 2001, about 1230 central daylight time, a Bell 206B-III, N56MC, operated by EAC Helicopters, Inc., sustained substantial damage on impact with water while maneuvering over Potato Lake, near Park Rapids, Minnesota. The pilot reported that the business flight was operating under 14 CFR Part 91. Visual meteorological conditions prevailed at the time of the accident. The commercial pilot reported that he and three passengers sustained minor injuries. No flight plan was on file. The local aerial photography flight departed from Park Rapids Municipal Airport (PKD), Park Rapids, Minnesota, at 1220 and was maneuvering at the time of the accident.
The pilot stated:
Departed Park Rapids enroute to Lake Itasca (20 mi. north). Potato
Lake selected for low altitude water/shoreline footage. Did high
recon, no observed boat traffic in conflict with flight path over water
at approx 40 to 50 ft. Commenced with descent profile of 80 mph
and 600 [feet per minute]. The descent was to continue until treetop
level then terminate descent and cruise over water for length of lake.
Flight path was south to north with planned airspeed of 60 - 80 mph,
then climb out.
Reached target altitude confirmed with left and right shoreline sight
picture, raised collective pitch with [simultaneous] forward cyclic
pressure to commence over water cruise. Engine appeared
non-responsive to power demand. Descent was not arrested. Added
additional collective, no response to power demand. Leveled
aircraft and impacted water with forward velocity.
The passenger in the front left seat stated:
We discussed the film project and the flight itinerary with the pilot
prior to takeoff. During this pre-flight meeting, I informed the pilot
that we wanted to film the headwaters. The pilot did not give us any
pre-flight safety briefing or instructions. The pilot did not
demonstrate or explain how to use the seat belts or how to egress
from the helicopter in case of an emergency.
After boarding, I sat next to the pilot and my two co-workers sat in
the back of the helicopter. Shortly after takeoff, I noticed we were
flying very low over the lake. Suddenly the helicopter abruptly dove
down nose first crashing into the lake. The helicopter quickly began
to sink into the water. For some time, I lost consciousness and
when I awoke, I was descending further down into the water. I began
to struggle to unsnap my seatbelt. At that point I realized I was
trapped to my seat sinking and that my seat had broken off from the
plane. I could not unbuckle the safety harness strap. My clothing
was getting very heavy and I began to swallow water uncontrollably.
I thought I was going to die.
I continued to unsuccessfully struggle with the safety harness. Finally,
somehow, I was able to wiggle out of the buckled safety harness.
Once free from the seat, I was so deep into the water that I could not
tell which way was up to the surface. I began to just swim, not
knowing which direction to go in. Eventually, I emerged at the lake's
surface.
I was the last one to reach the surface. When I emerged I saw my two
co-workers helping the pilot to stay afloat.
The right rear passenger stated:
While I was riding in the helicopter, I did not wear seat belt since I
was shooting with video camera.
The flight began, and after about 10 minutes the helicopter suddenly
began to lose altitude over Potato Lake. Since the helicopter did not
exhibit any other unusual signs such as an abnormal noise or smoke,
and was not falling in a way that suggested it was going to crash, I
believed that it was probably falling due to operation by the pilot. In
the past, I occasionally have had experiences where a pilot will fly
lower to show off for us, and on this occasion as well I believed that
the pilot was demonstrating to us his flying skill. Since I had not told
him that we planned to shoot lakes on the way from a low altitude or
anything like that, I thought that perhaps we might have arrived
already at Lake Itasca, and after exchanging glances with [the left
rear passenger], I turned to the intercom and was about to ask, 'Have
we arrived at Lake Itasca?' At that moment, the helicopter fell into
the lake.
The left rear passenger stated:
The helicopter took off at noon. At first I had my seat belt on. Five
to 10 minutes after take off we could see the lake as a dot right in
front of us, and [the front seat passenger] began to film this using a
video camera. I took off my seatbelt so that I could take the
photographs to be used for the show, and began taking photographs
with my camera. From the time the helicopter took off to the time it
crashed there was not conversation between the people inside.
After a few minutes, I could see a large lake right in front of me. I
was viewing the lake through the finder on my camera and saw the
lake getting bigger and bigger, so I realized the helicopter was going
down. The helicopter was in no particular state of instability so I
thought the pilot was causing it to dive down by design.
Nonetheless, since Lake Itaska, the subject of filming, was supposed
to be farther away, I thought to myself, 'Why is the helicopter going
down here?' and I looked over at [the right rear passenger].
Immediately thereafter I heard the intercom switch being turned on
and then right after that I heard a 'bang!' and received a heavy jolt.
Personnel information
The pilot held a commercial pilot certificate with a rating for rotorcraft/helicopter. He held a certified flight instructor certificate for rotorcraft/helicopter. He also held a private pilot certificate with a rating for airplane single engine land. The pilot did not possess an instrument rating. The pilot stated that he had accumulated 3,032 hours of total flight experience, 2,992 hours of which were in rotorcraft. The pilot listed 538 hours of flight experience in this make and model of helicopter.
The pilot reported his most recent biennial flight review was completed in a Bell 206B-III on July 24, 2001.
The pilot's most recent Federal Aviation Administration (FAA) second-class medical certificate was issued on September 26, 2001. The pilot reported that the medical had a limitation of "corrective lenses."
Aircraft information
The 206B-III helicopter, serial number 3573, was a single engine, two-bladed semi-rigid main rotor, five-seat aircraft, which was manufactured by Bell Helicopter. It was powered by an Allison 250-C20J, serial number CAE-270014, turbo shaft, reverse flow engine, that had a maximum sea level rating of 420 horsepower. The pilot reported that the airframe had 3,182.2 hours of total flight time and that the engine had accumulated 1,444 hours since its last overhaul. The pilot stated that the last inspection the helicopter received was a 100-hour inspection on July 23, 2001. The pilot reported that the helicopter accumulated 12 hours of flight time since that inspection.
Meteorological information
At 1253, the PKD weather was: Wind calm, visibility 10 statute miles, sky condition clear; temperature 20 degrees C; dew point 4 degrees C; altimeter 30.17 inches of mercury. At 1253, the calculated density altitude at PKD was 2,067 feet.
Wreckage and impact information
The recovered helicopter wreckage was stored at PKD. Front cabin components to include the collective, console, and the cyclic stick were not recovered. The NTSB examined the recovered wreckage at PKD on November 5, 2003. The tailcone was separated from the aft fuselage. Control push-pull tubes were traced from the rotor pedals to the tail rotor. All separations in the control tubing were consistent with overload. The cyclic and collective p
Aircraft
- Registration
- N56MC
- Reported as
- Bell 206B-III
- Category
- Helicopter
- Serial number
- 3573
- Airframe hours
- 3,182.2
- Engine
- Allison 250 C20J, 420 horsepower, turbo shaft
- Damage
- Substantial damage
- Flight
- Business · Part 91
- Operator
- EAC Helicopters, Inc.
- Registered owner
- MJG Leasing Co. LLC
- Airworthiness certificate
- Standard, Normal
- Last inspection
- Annual · July 23, 2001 · 12 hours before
- Departed
- PKD · Park Rapids, MN
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
- 45
- Injuries
- Minor
- Certificates
- Flight instructor, Commercial
- Airplane ratings
- Single-engine land
- Medical
- Class 2, Valid Medical--w/ waivers/lim
- Seat
- Right
- Flight hours
- 3,032 total · 538 in this make and model · 2,975 as pilot in command · 92 in the last 90 days · 14 in the last 30 days · 0 in the last 24 hours
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 0° at 0 knots
- Visibility
- 10 statute miles
- Lowest ceiling
- None
- Temperature
- 68 °F, dew point 39 °F
- Altimeter
- 30.17 inHg
- Observed at
- PKD, 5 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.