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Accidents · NTSB WPR19FA188 · Final report

Robinson R44 accident near Hayward, California, July 15, 2019

On July 15, 2019 at about 9:26 pm local time, a 2003 Robinson R44 (helicopter), registered N144TG, was substantially damaged in an accident during maneuvering (low-alt flying) near Hayward, California (Hayward Executive airport). It was an instructional flight under general aviation rules (Part 91). 1 person was killed and 1 person was seriously injured. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The pilots’ loss of control during a low altitude maneuver for undetermined reasons, which resulted in impact with terrain.

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

What the record shows

Date
July 15, 2019 · about 9:26 pm local time
Place
Hayward, California · Hayward Executive · map
Type
Accident
Injuries
1 person was killed and 1 person was seriously injured.
Weather
visual conditions (good weather)
Aircraft
Robinson R44 II, built 2003 · all R44s on the register
Registration
N144TG · no longer on the register · serial 10227
Damage
Substantial damage
Flight
Instructional flight · general aviation rules (Part 91)

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

Following several rounds in the helicopter airport traffic pattern, the flight instructor and student pilot performed hovering maneuvers on a taxiway designated for helicopter training. During one of the hovering maneuvers, the helicopter drifted away from the taxiway, over the grass area, and rapidly advanced towards a fence line. According to the student pilot, the flight instructor initiated a left turn, and the helicopter turned “very rapidly.” Analysis of a surveillance video indicated the helicopter rolled left about 70° as it neared the fence line. The helicopter’s bank angle decreased to about 40° as the helicopter continued to turn left. As the helicopter turned to a northern heading, the left roll angle increased to about 90°. The main rotor blades contacted the ground immediately after and the helicopter came to rest. Postaccident examination of the helicopter revealed a punch tool at the aft bulkhead of the cabin resting against the tail rotor control bell crank. Testing performed by the helicopter manufacturer indicated the proximity of the punch to the tail rotor control bell crank could have inhibited some tail rotor control authority. However, as the examination did not reveal any other anomalies with the flight control system or powerplant, even if the pilot’s tail rotor authority was inhibited, he still had the authority to reduce engine power, lower the collective and land the helicopter at any moment during the flight. Further, the restricted tail rotor authority would not have affected the helicopter’s roll axis, and the rapid, steep roll angles that occurred moments before impact. The instructor and student pilot likely lost control of the helicopter during its final 90° left bank, but the cause of this and previous excessive bank angles and whether they were intended during the helicopter’s final movements could not be determined. The student pilot’s history with another flight instructor, of aggressive control inputs and lack of attention to the surrounding environment suggest that the instructor, in the accident, may have been forced to intervene and recover the helicopter. However, a lack of available evidence precluded the investigation from determining when this intervention occurred and whether it contributed to the accident.

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. Unknown or undetermined during maneuvering (low-alt flying) defining event
  2. Loss of control in flight during maneuvering (low-alt flying)
  3. Low altitude operation/event during maneuvering (low-alt flying)

The NTSB's findings

  • Personnel issues › Task performance › Use of equip/info › Aircraft control › Instructor/check pilot
  • Not determined › Not determined › (general) › (general) › Unknown/Not determined
  • Aircraft › Aircraft oper/perf/capability › Performance/control parameters › (general) › Unknown/Not determined

Pilot

  • Certificate: flight instructor, commercial pilot
  • Ratings: instructor: helicopter; instrument: helicopter; rotorcraft: helicopter
  • Flight time: 3,026.8 hours in all; 112.6 in this make and model; 2,104.3 on instruments
  • Last flight review: March 29, 2019
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: left
  • Injury: fatal

Dual student

  • Flight time: 20.3 hours in all; 20.3 in this make and model; 0 in the last 90 days; 0 in the last 30 days
  • Medical certificate: None
  • Seat: rgt
  • Injury: serious injuries

The aircraft

  • Airframe total time: 2,595 hours
  • Last inspection: 100-hour inspection, June 6, 2019; 25 hours since
  • Maximum gross weight: 2,500 lb
  • Seats: 4
  • Landing gear: fixed
  • Engine: Lycoming IO-540-AE1A5 (piston); 4,784 hours total
  • Operator: Pacific Helicopters LLC

The flight

  • Departed from: HWD Hayward CA at 8:41 pm
  • Flight plan: none

Weather at the time

  • Light: daylight
  • Wind: from 270° at 11 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 72°F (22°C), dew point 55°F (13°C)
  • Altimeter: 30.01 inHg
  • Observation at 9:48 pm from HWD

Injuries

FatalSeriousMinorNone
Flight crew11

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

17 documents, released by the NTSB on September 29, 2021. 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.