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Accidents · NTSB WPR11CA264 · Final report

Robinson Helicopter R22 BETA accident near Prescott, Arizona, June 18, 2011

On June 18, 2011 at about 6:30 pm local time, a Robinson Helicopter R22 BETA, registered N334DC, was substantially damaged in an accident during taxi (into takeoff position) near Prescott, Arizona (Ernest H Love Field). 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

The pilot's inadequate compensation for the wind conditions and failure to maintain directional control of the helicopter during taxi, resulting in a loss of tail rotor effectiveness and a subsequent hard landing.

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

What the record shows

Date
June 18, 2011 · about 6:30 pm local time
Place
Prescott, Arizona · Ernest H Love Field · map
Type
Accident
Injuries
No one was hurt; 2 people were on board or involved.
Weather
visual conditions (good weather)
Aircraft
Robinson Helicopter R22 BETA · all R22 BETAs on the register
Registration
N334DC · no longer on the register · serial 3511
Damage
Substantial damage
Flight
Instructional flight · general aviation rules (Part 91)

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

The instructor reported that his student was taxiing the helicopter in a north direction along a taxiway parallel to the runway with a near direct tailwind of 10 knots with gusts to 19. The student started to lose tail rotor authority over the helicopter. At this time the instructor took control of the helicopter and proceeded to apply full left pedal until he regained tail rotor authority and directional control. Because of the strong wind from the south, the instructor opted to keep control of the helicopter until they were airborne and he proceeded to continue their taxi to the displaced threshold of the runway. Upon reaching the displaced threshold, the instructor started a 220 degree turn to the left in order to line up with a takeoff direction to the south into the wind. The instructor reported that half way through the turn the helicopter violently yawed to the left, and he applied full right pedal to cancel the yaw but was unable to arrest the helicopter's left yawing moment. The helicopter landed hard on the skids, damaging the main rotor and severing the tail boom aft of the tail rotor blades hazard guard and before the tail rotor transmission. The pilot reported no mechanical issues with the helicopter prior to the flight. The wind limitation listed in the Pilot's Operating Handbook for the helicopter is 25 knots including any gust factor.

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. Loss of tail rotor effectiveness during taxi (into takeoff position) defining event
  2. Loss of control on ground during taxi (into takeoff position)
  3. Collision with terrain or object (not controlled flight into terrain) during taxi (into takeoff position)

The NTSB's findings

  • cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
  • Environmental issues › Conditions/weather/phenomena › Wind › Tailwind › Effect on equipment
  • cause Environmental issues › Conditions/weather/phenomena › Wind › Tailwind › Response/compensation
  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Directional control › Not attained/maintained

Flight instructor

  • Certificate: commercial pilot
  • Ratings: instructor: helicopter; rotorcraft: helicopter
  • Flight time: 339 hours in all; 187 in this make and model; 85 in the last 90 days; 49 in the last 30 days; 234 as pilot in command; 91 on instruments
  • Last flight review: December 1, 2010
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: left
  • Injury: no injuries

The aircraft

  • Airframe total time: 4,352 hours
  • Last inspection: 100-hour inspection, May 12, 2011; 89 hours since
  • Maximum gross weight: 1,370 lb
  • Seats: 2
  • Landing gear: fixed
  • Engine: Lycoming O-360 SERIES (piston); 0 hours total
  • Operator: Guidance Helicopters INC

The flight

  • Departed from: KPRC Prescott AZ
  • Destination: KPRC Prescott AZ
  • Flight plan: none
  • Runway 12, 4,408 ft by 75 ft
  • A second pilot was aboard

Weather at the time

  • Light: daylight
  • Wind: from 170° at 10 knots, gusting 19
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 81°F (27°C), dew point 19°F (-7°C)
  • Altimeter: 30.04 inHg

Injuries

FatalSeriousMinorNone
Flight crew2

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.

Other NTSB records under N334DC the same tail number, which may have belonged to a different aircraft at the time

2019-07-08CEN19LA245 · accident near Water Valley, TX · substantial damage · no injuries

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.