- Date
- June 18, 2011, 18:45 local (23:45 UTC)
- Place
- Montgomery City, MO
- Injuries
- 1 uninjured
- Damage
- Substantial damage
- Phase of flight
- Landing
- Aircraft
- N24HMBell 47G-4A
- Defining event
- Landing: Hard landing
- Weather
- Visual (VMC) · Day
- Status
- Completed · report October 4, 2011
- Report
- Approved by Office Director
- NTSB office
- Central Region
- FAA report
- 20110618012569A
- Case key
- 80823
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
A loss of control during the precautionary landing, which resulted in inadvertent contact between the main rotor and the tailboom. Contributing to the accident was the overloaded condition.
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 had returned from an agricultural application to reload the cleaning solution. Unbeknownst to the pilot, the helicopter was loaded with approximately 90 gallons of solution, instead of the expected 70 gallons for the flight. The pilot reported that he increased engine power and lifted off; however, immediately after lift off the engine and rotor speed began to decrease. He selected a suitable landing point and flared for touchdown about 10 feet above ground level to minimize the forward speed. The helicopter touched down on the rear portion of the landing skids and began to pitch forward. He applied aft cyclic control to prevent the helicopter from nosing over. He subsequently heard a bang and observed debris coming from the aircraft. He shut down the engine and secured the helicopter. A postaccident examination revealed that the main rotor had struck the tailboom resulting in substantial damage to the airframe. The pilot said the helicopter may have been on a slight incline when the solution was loaded, allowing the right side tank to fill more than the left side tank. He was unaware of the overload condition. The pilot added that closer monitoring of the helicopter and chemical truck incline, and the final amount of solution being loaded onto the helicopter, might have prevented the accident. The pilot did not report any failures or malfunctions that would have precluded normal operation.
Factual narrative
The pilot reported that he had returned from a prior agricultural application flight. The helicopter chemical tank was loaded with cleaning solution. The pilot stated that he increased engine power and lifted off again. However, immediately after takeoff, the engine and rotor speed began to decrease, and the pilot selected a nearby location for a landing. He flared for touchdown about 10 feet above ground level in order to minimize the forward speed. The helicopter touched down on the rear portion of the landing skids and began to pitch forward. The pilot responded by applying aft cyclic control to prevent the helicopter from nosing over. He subsequently heard a bang and observed debris coming from the aircraft. He shut down the engine and secured the helicopter. A postaccident examination revealed that the main rotor had struck the tailboom resulting in substantial damage to the airframe. The pilot did not report any failures or malfunctions related to the helicopter that occurred prior to the accident. However, the chemical tank was determined to have been loaded with approximately 90 gallons of cleaning solution, instead of the intended 70 gallons. He commented that the aircraft may have been on a slight incline when the solution was loaded, allowing the right side tank to fill more than the left side tank. As a result, he was unaware of the overload condition. The pilot added that closer monitoring of the helicopter and chemical truck incline, and the final amount of solution being loaded onto the helicopter, might have prevented the accident.
Aircraft
- Registration
- N24HM
- Reported as
- Bell 47G-4A
- Category
- Helicopter
- Serial number
- 7688
- Airframe hours
- 11,153
- Engine
- Lycoming VO-540 SERIES, 310 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Aerial application · Part 137
- Operator
- Rhineland Grain Inc
- Registered owner
- Rhineland Grain Inc
- Airworthiness certificate
- Special, Restricted (Special)
- Last inspection
- Annual · February 26, 2011
- Departed
- PVT · Montgomery City, MO
- Destination
- PVT · Montgomery City, MO
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
- 27
- Injuries
- None
- Certificates
- Flight instructor, Commercial
- Instrument ratings
- Helicopter
- Medical
- Class 2, Without waivers/limitations
- Last flight review
- March 31, 2011
- Seat
- Left
- Flight hours
- 1,900 total · 880 in this make and model · 1,810 as pilot in command · 55 in the last 90 days · 40 in the last 30 days · 3 in the last 24 hours
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 180° at 5 knots
- Visibility
- 10 statute miles
- Lowest ceiling
- None
Docket · 2
The files NTSB released with the investigation on July 21, 2011, on NTSB’s docket system: statements, records, photos and specialists’ reports. 444 KB 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 N24HM · 1
Matched to the same aircraft by N-number and date.