Robinson Helicopter Company R44 II accident near Borrego Springs, California, April 30, 2018
On April 30, 2018 at about 8:30 pm local time, a 2013 Robinson Helicopter Company R44 II, registered N423ML, was substantially damaged in an accident during landing near Borrego Springs, California (Palm Springs Intl airport). It was a business flight under general aviation rules (Part 91). 1 person had minor injuries; 4 others were unhurt. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The loss of the helicopter’s drive system for reasons that could not be determined from the available evidence, which led to an autorotation that resulted in a hard landing and rollover on uneven sandy terrain.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- April 30, 2018 · about 8:30 pm local time
- Place
- Borrego Springs, California · Palm Springs Intl · map
- Type
- Accident
- Injuries
- 1 person had minor injuries; 4 others were unhurt.
- Weather
- visual conditions (good weather)
- Aircraft
- Robinson Helicopter Company R44 II II, built 2013
- Registration
- N423ML · no longer on the register · serial 13453
- Damage
- Substantial damage
- Flight
- Business flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The pilot of a Robinson Helicopter Company R44 II reported that, after takeoff, he heard a “light thump” and that the helicopter yawed from left to right. Shortly thereafter, the clutch light illuminated; 5 seconds later, the low rotor rpm light illuminated, and the low rotor warning horn sounded. The pilot performed an autorotation by fully lowering the collective and applying aft cyclic to load the main rotor blade system and maintain the airspeed. During the autorotation, the low rotor rpm horn and light continued, and the clutch light went out. The rotor rpm then increased to 100%, and the warning light and horn extinguished. The pilot continued the landing, however while descending through an altitude of 50 ft agl, the wind switched from a headwind to a tailwind, and the low rotor rpm light and horn annunciated again. Due to the helicopter’s low altitude, he was not able to maneuver back into the wind to land. As the helicopter settled through 5 ft agl, it weathervaned, bringing the nose to the left. The pilot used full collective just before touchdown and the helicopter landed hard on its skids on uneven sandy terrain and came to rest on its right side. The Robinson Helicopter Company R44 II pilot’s operating handbook stated that a drive system failure would be indicated by the low rotor rpm horn and possibly an unusual noise or a yaw to the right or left, all of which the pilot reported. Thus, the available evidence for this investigation indicated that the likely cause of the accident was a drive system loss of power. The handbook also stated that, if the clutch light illuminates during flight and does not extinguish within 10 seconds, “land immediately if there are other indications of drive system failure” and advised that, under those circumstances, the drive system should be inspected for a possible malfunction. However, postaccident examination of the helicopter revealed no mechanical malfunctions or anomalies that would have precluded normal operation of the drive system. As a result, the National Transportation Safety Board was unable to determine, from the available evidence, why the drive system loss of power occurred.
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
- Off-field or emergency landing during landing defining event
- Hard landing during landing
The NTSB's findings
- Aircraft › Aircraft propeller/rotor › Main rotor drive › Rotor/drive indicating system › Unknown/Not determined
- Environmental issues › Physical environment › Terrain › Sloped/uneven terrain › Effect on operation
- Not determined › Not determined › (general) › (general) › Unknown/Not determined
Pilot
- Certificate: airline transport pilot, flight instructor, commercial pilot
- Ratings: multi-engine land; single-engine land; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: helicopter; instructor: instrument airplane; instrument: airplane; rotorcraft: helicopter
- Flight time: 5,551 hours in all; 610 in this make and model; 180 in the last 90 days; 67 in the last 30 days; 4,266 as pilot in command; 3,293 on instruments
- Last flight review: August 16, 2017
- Medical certificate: Class 1 (without waivers/limitations)
- Seat: rgt
- Injury: no injuries
Passenger
- Seat: left
- Injury: no injuries
Passenger
- Seat: left
- Injury: no injuries
Passenger
- Seat: rgt
- Injury: minor injuries
The aircraft
- Airframe total time: 941.7 hours
- Last inspection: 100-hour inspection, April 27, 2018; 6.2 hours since
- Maximum gross weight: 2,500 lb
- Seats: 4
- Landing gear: fixed
- Engine: Lycoming IO-540-AE1A5 (piston); 942 hours total
- Operator: Big Blue CORP INC
The flight
- Departed from: Borrego Springs CA at 8:50 pm
- Destination: TRM Palm Springs CA
- Flight plan: none
Weather at the time
- Light: daylight
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 82°F (28°C), dew point 37°F (3°C)
- Altimeter: 29.77 inHg
- Observation at 1:52 pm from KTRM, 25 miles away
Weather report (METAR): METAR KTRM 302052Z AUTO VRB03G15KT 10SM CLR 28/03 A2977 RMK AO2 SLP084 T02830028 56021=
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 | |||
| Passengers | 1 | 3 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
11 documents, released by the NTSB on July 13, 2022. 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, 9 pages | View Download |
| 2 | Record of Conversation (Evans) | PDF, 2 pages | View Download |
| 3 | NTSB Wreckage Exam Report | PDF, 9 pages | View Download |
| 4 | Summary of Findings (FAA) | PDF, 1 page | View Download |
| 5 | Summary of Findings (Insurance Company) | PDF, 1 page | View Download |
| 6 | Rhc Emergency Procedures Section 3 - Clutch | PDF, 1 page | View Download |
| 7 | Rhc Emergency Procedures - Low Rpm | PDF, 1 page | View Download |
| 8 | Rhc Emergency Procedure Power Failure General | PDF, 1 page | View Download |
| 9 | Statement of Party Representatives to NTSB Investigation | PDF, 1 page | View Download |
| 10 | Release of Aircraft Wreckage, NTSB Form 6120.15 | PDF, 1 page | View Download |
| 11 | Photos | PDF, 3 pages | 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.
