Robinson Helicopter R44 II accident near Herriman, Utah, July 13, 2024
On July 13, 2024 at about 4:35 pm local time, a 2023 Robinson Helicopter R44 II, registered N6960, was substantially damaged in an accident near Herriman, Utah. It was an instructional flight under general aviation rules (Part 91). No one was hurt; 2 people were on board or involved. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
A hard landing following a total loss of engine power due to fuel starvation as a result of the improper idle setting of the helicopter’s engine. Contributing to the loss of engine power was the instructor’s reduction of engine power past that recommended by the manufacturer for practice autorotations.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- July 13, 2024 · about 4:35 pm local time
- Place
- Herriman, Utah · map
- Type
- Accident
- Injuries
- No one was hurt; 2 people were on board or involved.
- Weather
- visual conditions (good weather)
- Aircraft
- Robinson Helicopter R44 II, built 2023 · all R44 IIs on the register
- Registration
- N6960 · registry record · serial 14632
- Damage
- Substantial damage
- Flight
- Instructional flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The helicopter flight instructor was demonstrating a practice autorotation with a power recovery for the student. The instructor stated that he reduced the throttle to idle and entered the autorotation. After noticing several caution lights illuminate, the instructor attempted to increase engine power and realized that the engine had lost total power. The cockpit video recorder showed that the engine tachometer needle decreased from 100% to below 46% rpm, below idle. The instructor continued the autorotation to a field and the helicopter landed hard. During the landing, the main rotor blades struck the tailboom, resulting in substantial damage. A postaccident examination and engine run revealed that the engine would not start and idle unless the electric boost pump was set to ON. Subsequent bench testing of the mechanical fuel pump and fuel injection servo revealed no anomalies. The flight instructor reported that he noticed the helicopter’s engine would idle about 50-52% rpm, but stated that the engine did not have any issues when he previously demonstrated practice autorotations. He added that he did not notify maintenance of the low idle setting, as he was not aware that it was adjustable. According to the operator’s maintenance manual, the idle setting for the accident engine mode should be 58-62%. According to the pilot’s operating handbook (POH), “Idle mixture and speed may require adjustment as conditions vary from sea level standard.” The accident helicopter’s maintenance logs did not indicate that the flight idle was adjusted as recommended by the manufacturer after the helicopter was received from the factory. It is likely that, given the engine’s low idle setting, the instructor did not immediately recognize that the rpm continued to decrease past idle and the subsequent loss of engine power due to fuel starvation. It is also likely that, had the instructor followed the manufacturer's recommendation to lower tachometer needle separation to the desired level, usually below 80% but above idle, the engine would not have lost power.
The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.
The factual record from the NTSB's investigation tables, in plain English
What happened, in order
- Autorotation Loss of engine power (total) defining event
- Autorotation Hard landing
The NTSB's findings
- Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Instructor/check pilot
- Aircraft › Aircraft power plant › Engine fuel and control › Fuel control/carburetor › Not serviced/maintained
- Environmental issues › Physical environment › Terrain › Sloped/uneven terrain › Effect on equipment
- Organizational issues › Support/oversight/monitoring › Oversight › Oversight of operation › Operator
- Personnel issues › Task performance › Use of equip/info › Use of policy/procedure › Instructor/check pilot
Pilot
- Certificate: flight instructor, commercial pilot
- Ratings: instructor: helicopter; instructor: instrument helicopter; instrument: helicopter; rotorcraft: helicopter
- Flight time: 755 hours in all; 217 in this make and model; 177 in the last 90 days; 80 in the last 30 days; 646 as pilot in command; 416 on instruments
- Last flight review: September 21, 2023
- Medical certificate: Class 2 (with waivers/limitations)
- Seat: left
- Injury: no injuries
Dual student
- Certificate: private
- Ratings: single-engine land
- Flight time: 115 hours in all; 12 in this make and model; 12 in the last 90 days; 5 in the last 30 days; 49 as pilot in command
- Last flight review: August 27, 2011
- Medical certificate: Class 2 (without waivers/limitations)
- Seat: rgt
- Injury: no injuries
The aircraft
- Airframe total time: 56.5 hours
- Last inspection: annual inspection, June 20, 2024; 31.7 hours since
- Maximum gross weight: 2,500 lb
- Seats: 4
- Landing gear: fixed
- Engine: Lycoming L-38290-48E (piston); 88 hours total
- Operator: Takeflight LLC
The flight
- Departed from: U42 West Jordan UT at 4:30 pm
- Flight plan: none
- A second pilot was aboard
Weather at the time
- Light: daylight
- Wind: from 160° at 4 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 90°F (32°C), dew point 32°F (0°C)
- Altimeter: 30.16 inHg
- Observation at 10:35 am from KU42, 7 miles away
Weather report (METAR): KU42 131635Z AUTO 16004KT 10SM CLR 32/00 A3016 RMK AO1 T03230000
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 2 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
17 documents, released by the NTSB on May 21, 2026. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.
| # | Document | What it is | |
|---|---|---|---|
| 1 | Pilot/operator Aircraft Accident Report, NTSB Form 6120.1 | PDF, 11 pages | View Download |
| 2 | Mor - CFI | PDF, 2 pages | View Download |
| 3 | Manual Excerpts | PDF, 6 pages | View Download |
| 4 | Logbook Entries | PDF, 2 pages | View Download |
| 5 | ADS-B | map file | Download |
| 6 | ADS-B Csv File | spreadsheet | Download |
| 7 | Accident Photos | PDF, 3 pages | View Download |
| 8 | Follow-up Examination Report Summary | PDF, 15 pages | View Download |
| 9 | Mor Mechanic | PDF, 1 page | View Download |
| 10 | Mor Lycoming | PDF, 1 page | View Download |
| 11 | Mor Fuel Pump Testing | PDF, 2 pages | View Download |
| 12 | Mor Fuel Servo Exam | PDF, 5 pages | View Download |
| 13 | Mor- Helicopter Manufacturer | PDF, 2 pages | View Download |
| 14 | Onboard Image Recorder - Specialist's Factual Report | PDF, 5 pages | View Download |
| 15 | Release of Aircraft Wreckage, NTSB Form 6120.15 | PDF, 1 page | View Download |
| 16 | Evidence Control Form | PDF, 4 pages | View Download |
| 17 | Statement of Party Representatives to NTSB Investigation | PDF, 1 page | View Download |
The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.
Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.
