- Date
- June 8, 2016, 12:05 local (17:05 UTC)
- Place
- Hastings, MN
- Injuries
- 1 uninjured
- Damage
- Substantial damage
- Phase of flight
- Takeoff
- Aircraft
- N25LBBell 47G
- Defining event
- Takeoff: Loss of control in flight
- Weather
- Visual (VMC) · Day
- Status
- Completed · report July 14, 2016
- Report
- Approved by Office Director
- NTSB office
- General Aviation Accidents
- Parties
- FAA
- FAA report
- 20160608009259A
- Case key
- 93345
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's failure to attain a positive rate of climb during takeoff from a service truck, which resulted in an impact with terrain and substantial damage to the tail boom and fuselage.
Findings · 2
NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.
Sequence of events
The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.
Analysis
The pilot reported that he was conducting aerial agricultural operations in a helicopter and that he landed on the bed of the service truck to reload with insecticide and fuel. The pilot further reported that he began to lift off and during the transition to forward flight he pitched the helicopter forward to gain airspeed, but helicopter continued to descend. The pilot reported that he "never gained lift from the ground effect" and subsequently impacted the terrain. The helicopter sustained substantial damage to the tail boom and fuselage. The pilot reported there were no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. FAA Helicopter Flying Handbook Chapter 2 "Aerodynamics" defines "In Ground Effect (IGE)" as the increased efficiency of the rotor system caused by interference of the airflow when near the ground. The air pressure or density is increased, which acts to decrease the downward velocity of air. Ground effect permits relative wind to be more horizontal, lift vector to be more vertical, and induced drag to be reduced. These conditions allow the rotor system to be more efficient. Maximum ground effect is achieved when hovering over smooth hard surfaces. When hovering over surfaces as tall grass, trees, bushes, rough terrain, and water, maximum ground effect is reduced. Rotor efficiency is increased by ground effect to a height of about one rotor diameter (measured from the ground to the rotor disk) for most helicopters.
Factual narrative
The pilot reported that he was conducting aerial agricultural operations in a helicopter and that he landed on the bed of the service truck to reload with insecticide and fuel. The pilot further reported that he began to lift off and during the transition to forward flight he pitched the helicopter forward to gain airspeed, but helicopter continued to descend. The pilot reported that he "never gained lift from the ground effect" and subsequently impacted the terrain. The helicopter sustained substantial damage to the tail boom and fuselage. The pilot reported there were no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. FAA Helicopter Flying Handbook Chapter 2 "Aerodynamics" defines "In Ground Effect (IGE)" as the increased efficiency of the rotor system caused by interference of the airflow when near the ground. The air pressure or density is increased, which acts to decrease the downward velocity of air. Ground effect permits relative wind to be more horizontal, lift vector to be more vertical, and induced drag to be reduced. These conditions allow the rotor system to be more efficient. Maximum ground effect is achieved when hovering over smooth hard surfaces. When hovering over surfaces as tall grass, trees, bushes, rough terrain, and water, maximum ground effect is reduced. Rotor efficiency is increased by ground effect to a height of about one rotor diameter (measured from the ground to the rotor disk) for most helicopters.
Aircraft
- Registration
- N25LB
- Reported as
- Bell 47G (5A)
- Category
- Helicopter
- Serial number
- 25102
- Built
- 1978
- Airframe hours
- 14,764.8
- Engine
- Allison 250-C18A, 317 horsepower, turbo shaft
- Damage
- Substantial damage
- Flight
- Aerial application · Part 137
- Airworthiness certificate
- Special, Restricted (Special)
- Last inspection
- 100 hour · March 1, 2016
- Departed
- 12Y · Le Sueur, MN
- Destination
- Hastings, MN
- Equipment
- Handheld GPS
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
- 31
- Injuries
- None
- Certificate
- Commercial
- Medical
- Class 2, Without waivers/limitations
- Last flight review
- November 19, 2015
- Seat
- Left
- Restraint
- 3-point
- Flight hours
- 1,296 total · 25 in this make and model · 1,252 as pilot in command · 25 in the last 90 days · 25 in the last 30 days · 5 in the last 24 hours
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 150° at 5 knots
- Visibility
- 10 statute miles
- Lowest ceiling
- None
- Temperature
- 72 °F, dew point 46 °F
- Altimeter
- 29.97 inHg
- Observed at
- KSYN, 12 nm away
Docket · 2
The files NTSB released with the investigation on July 12, 2016, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.3 MB in all.
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 N25LB · 1
Matched to the same aircraft by N-number and date.