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Accidents · NTSB WPR18FA077 · Final report

Robinson Helicopter R44 accident near Newport Beach, California, January 30, 2018

On January 30, 2018 at about 9:50 pm local time, a 2003 Robinson Helicopter R44, registered N7530R, was destroyed in an accident during enroute (climb to cruise) near Newport Beach, California (John Wayne Airport-Orange Coun). It was a personal flight under general aviation rules (Part 91). 3 people were killed and 1 person was seriously injured. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The pilot's failure to perform weight and balance calculations before departing on the flight, which resulted in his operation of the helicopter outside of its published weight and balance limitations and a subsequent loss of control shortly after takeoff.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
January 30, 2018 · about 9:50 pm local time
Place
Newport Beach, California · John Wayne Airport-Orange Coun · map
Type
Accident
Injuries
3 people were killed and 1 person was seriously injured.
Weather
visual conditions (good weather)
Aircraft
Robinson Helicopter R44 UNDESIGNAT, built 2003 · all R44s on the register
Registration
N7530R · no longer on the register · serial 1295
Damage
Destroyed
Flight
Personal flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

The private pilot of the helicopter departed with three passengers on a cross-country flight in day visual meteorological conditions. Surveillance video of the takeoff showed that the helicopter assumed a nose-low attitude upon lifting off the ground and mostly maintained that attitude throughout the takeoff and initial climb. Radar data indicated that the helicopter reached a maximum altitude of 500 ft mean sea level before it entered a rapid descent and impacted homes and the ground less than 1 mile from the departure airport. The surviving passenger described the descent as "straight down." An examination of the airframe, engine, and related systems revealed no evidence of preimpact mechanical malfunctions or failures that would have precluded normal operation. Weight and balance calculations revealed that the helicopter was operating 76 lbs over its published maximum gross weight and near the published forward center of gravity (CG) limits. The helicopter's observed nose-low attitude throughout the flight is consistent with a forward CG, which would have required additional aft cyclic control inputs to maintain level flight and may have resulted in reduced cyclic control travel. The passenger stated that the pilot did not ask any of the passengers for their weights, nor did he instruct them where to sit, suggesting that the pilot did not perform weight and balance calculations before the flight. Given the lack of mechanical anomalies, it is likely that the pilot experienced a loss of helicopter control due to his decision to operate the helicopter outside of its published weight and balance limitations.

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

  1. Aircraft loading event during prior to flight
  2. Loss of control in flight during enroute (climb to cruise) defining event
  3. Collision with terrain or object (not controlled flight into terrain) during enroute (climb to cruise)

The NTSB's findings

  • cause Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Pilot
  • cause Aircraft › Aircraft oper/perf/capability › Aircraft capability › Maximum weight › Capability exceeded
  • cause Aircraft › Aircraft oper/perf/capability › Aircraft capability › CG/weight distribution › Capability exceeded
  • cause Personnel issues › Task performance › Planning/preparation › Weight/balance calculations › Pilot
  • cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot

Pilot

  • Certificate: private
  • Ratings: instrument: helicopter
  • Flight time: 195 hours in all
  • Medical certificate: Class 3 (without waivers/limitations)
  • Seat: rgt
  • Injury: fatal

The aircraft

  • Airframe total time: 6,966.3 hours
  • Last inspection: 100-hour inspection, December 7, 2017
  • Maximum gross weight: 2,400 lb
  • Landing gear: fixed
  • Engine: Lycoming O-540-F1B5 (piston); 0 hours total

The flight

  • Departed from: SNA Santa Ana CA at 9:49 pm
  • Destination: Catalina Island CA
  • Flight plan: none

Weather at the time

  • Light: daylight
  • Wind: from 210° at 5 knots
  • Visibility: 10 statute miles
  • Sky: broken clouds at 18,000 ft; a few clouds at 13,000 ft
  • Temperature: 79°F (26°C), dew point 28°F (-2°C)
  • Altimeter: 29.97 inHg
  • Observation at 9:53 pm from KSNA, 1 miles away

Injuries

FatalSeriousMinorNone
Flight crew1
Passengers21

Documents from the investigation the NTSB's docket: the evidence folder behind the report

15 documents, released by the NTSB on December 10, 2019. 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.

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.