Robinson R44 accident near Lucerne Valley, California, May 28, 2005
On May 28, 2005 at about 6:50 pm local time, a Robinson R44 (helicopter), registered N7015Q, was destroyed in an accident near Lucerne Valley, California. It was a personal flight under general aviation rules (Part 91). 3 people were seriously injured. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
the pilot's failure to maintain adequate main rotor rpm and directional control while maneuvering at low altitude. Contributing factors in the accident were the helicopter's gross weight in excess of the maximum hover out of ground effect limit, a high density altitude, and the pilot's lack of overall experience with regard to low rpm and settling-with-power recovery techniques.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- May 28, 2005 · about 6:50 pm local time
- Place
- Lucerne Valley, California · map
- Type
- Accident
- Injuries
- 3 people were seriously injured.
- Weather
- visual conditions (good weather)
- Aircraft
- Robinson R44 · all R44s on the register
- Registration
- N7015Q · no longer on the register · serial 0462
- Damage
- Destroyed
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The helicopter impacted level terrain and rolled onto its left side while maneuvering during a low-level photo flight. The pilot was flying southbound along a racecourse on a photo flight when he made a hard 180-degree turn, and lost control of the helicopter. As the helicopter began a spin to the right, the pilot noted a loss of rpm and altitude. He asked the certified flight instructor (CFI)/safety pilot to take the flight controls. As the CFI took control of the helicopter, he realized that the rpm's were decaying and that the helicopter was too low to recover the rpm. He attempted to cushion the impact with the collective. Both pilots reported that there were no preimpact mechanical anomalies with the airframe or engine. No evidence of any preimpact mechanical malfunction was found during the post accident investigation that would have precluded normal operation. During the accident flight, the helicopter was running approximately 131 pounds over the maximum gross weight for an Out of Ground Effect hover for the existing atmospheric conditions. The helicopter was being operated in a high density altitude environment, which was computed to be 7,350 feet mean sea level. The pilot received his rotorcraft helicopter rating 7 days prior to the accident. He had approximately 77 hours of total rotorcraft flight time at the time of the accident. The helicopter manufacturer indicated that photo flights were a high risk phase of flight and issued a safety notice SN-34. Safety Notice SN-34 recommended at least 500 hours and extensive training in both low rpm and settling-with-power recovery techniques prior to flying photo shoot type flights.
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
Pilot
- Certificate: private
- Ratings: multi-engine land; single-engine land; rotorcraft: helicopter
- Flight time: 1,600 hours in all; 50 in this make and model; 1,410 as pilot in command
- Last flight review: May 1, 2005
- Medical certificate: Class 3 (without waivers/limitations)
- Seat: rgt
- Injury: serious injuries
Flight instructor
- Certificate: commercial pilot
- Ratings: instructor: helicopter; rotorcraft: helicopter
- Flight time: 520 hours in all; 30 in the last 30 days; 130 on instruments
- Medical certificate: Class 2 (without waivers/limitations)
- Seat: left
- Injury: serious injuries
The aircraft
- Airframe total time: 580 hours
- Last inspection: annual inspection, December 1, 2004; 80 hours since
- Maximum gross weight: 2,400 lb
- Seats: 4
- Landing gear: fixed
- Engine: Lycoming O-540-F1B5 (piston); 0 hours total
- Fire on the ground
The flight
- Departed from: L12 Redlands CA at 4:51 pm
- Flight plan: none
- A second pilot was aboard
Weather at the time
- Light: daylight
- Wind: from 240° at 10 knots, gusting 16
- Visibility: 20 statute miles
- Sky: clear
- Temperature: 91°F (33°C), dew point 39°F (4°C)
- Altimeter: 29.81 inHg
- Observation at 6:54 pm from DAG, 17 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Crew | 2 | |||
| Passengers | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.
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.
