- Date
- August 26, 1994, 17:45 local (22:45 UTC)
- Place
- Lake City, MN
- Injuries
- 1 uninjured
- Damage
- Substantial damage
- Phase of flight
- Maneuvering
- Aircraft
- N19JMBell 47 MARK-6
- Weather
- Visual (VMC) · Day
- Status
- Completed · report February 24, 1995
- Report
- Approved by Office Director
- FAA report
- 19940826034149A
- Case key
- 9656
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 lift resulting from the pilot's failure to maintain rotor RPM during an aerial application turn. The power available from the engine was less than that required to regain the lost rotor RPM.
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 performing a low level agricultural application turn, the pilot reported completing his turn and having a lower than normal rotor RPM. The temperature was approximately 74 degrees fahrenheit and the humidity was reported by the pilot as high. Density altitude was approximately 2000 feet. Attempting to regain RPM and level off was not successful, and the helicopter spray booms contacted the corn crop. The helicopter stopped and overturned.
Factual narrative
On August 26, 1994, at 1745 hours central daylight time, a Bell BH-47 Mark-6 helicopter, N19JM, operated by Northland Helicopter, Inc., of Stacyville, Iowa, impacted in a crop field 4 miles south of Lake City, Minnesota, and was substantially damaged. The commercially certificated pilot was uninjured and no fire occurred. Visual meteorological conditions existed at the time of the accident and no flight plan was filed. The flight operated under 14 CFR Part 137 as an agricultural application aircraft, and the flight had originated from a tending vehicle near the accident site at 1530 hours CDT.
The pilot reported that after making an application turn, rotor RPM decayed and he was unable to maintain level flight or regain the rotor rpm. The temperature was 74 degrees Farenheit, the humidity was described by the pilot as high, the elevation was 1300 feet above mean sea level, and the density altitude was at least 2000 feet. Post crash inspection of the helicopter and powerplant failed to reveal any discrepancies.
Aircraft
- Registration
- N19JM
- Reported as
- Bell 47 MARK-6
- Category
- Helicopter
- Serial number
- 1921
- Airframe hours
- 5,852
- Engine
- Lycoming V0-435-A1F, 260 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Aerial application · Part 137
- Operator
- Northland Helicopter Inc
- Registered owner
- Northland Helicopters, Inc
- Airworthiness certificate
- Special, Restricted (Special)
- Last inspection
- Annual · October 10, 1993 · 170 hours before
Flight crew
As NTSB recorded them. NTSB leaves out names.
- Role
- Pilot
- Age
- 46
- Certificate
- Commercial
- Airplane ratings
- Single-engine land
- Medical
- Class 2, Valid Medical--no waivers/lim.
- Seat
- Front
- Flight hours
- 5,796 total · 4,600 in this make and model · 5,766 as pilot in command
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 60° at 6 knots
- Visibility
- 12 statute miles
- Lowest ceiling
- 2,900 ft broken
- Temperature
- 73 °F, dew point 70 °F
- Altimeter
- 30.00 inHg
- Observed at
- RST, 30 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.