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Accidents · NTSB FTW03LA099 · Final report

Robinson R22 Beta II accident near Kent, Texas, February 18, 2003

On February 18, 2003 at about 7:23 pm local time, a Robinson R22 Beta II (helicopter), registered N54TR, was substantially damaged in an accident near Kent, Texas. It was a ferry flight under general aviation rules (Part 91). 1 person had minor injuries; 1 other was unhurt. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The loss of main rotor drive due to a drive belt separation resulting in a forced landing. A contributing factor was the lack of suitable terrain for the forced landing.

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

What the record shows

Date
February 18, 2003 · about 7:23 pm local time
Place
Kent, Texas · map
Type
Accident
Injuries
1 person had minor injuries; 1 other was unhurt.
Weather
visual conditions (good weather)
Aircraft
Robinson R22 Beta II · all R22 Beta IIs on the register
Registration
N54TR · no longer on the register · serial 3412
Damage
Substantial damage
Flight
Ferry flight · general aviation rules (Part 91)

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

While ferrying a helicopter to its new owner/operator, the 1,351-hour pilot experienced a loss of main rotor drive. The pilot reported that the helicopter was in level cruise flight at an altitude of 700 to 900 feet AGL at an indicated airspeed of 70 to 75 knots, when they heard a loud "thump" coming from the area behind the cabin, immediately followed by the activation of the clutch light and accompanied with a change in engine and rotor noise. Within a couple of seconds, the pilot reported hearing another "thump" and, subsequently, the engine RPM started to increase as the rotor RPM was decreasing. The pilot initiated a 180-degree turn to position the helicopter into the wind while maintaining 70 knots as he entered an autorotation into rolling rough and uneven terrain. The helicopter came to rest in an upright position. Examination of the wreckage by the FAA inspectors, who traveled to the accident site, revealed that both main rotor blades were damaged and the tailboom was severed from the helicopter and broken into several pieces consistent with the main rotor contacting the tailboom during the landing. The engine showed evidence of an overspeed greater than about 110%. One of the two drive belts was missing and the remaining belt was off of the upper sheave and showed considerable damage. The wreckage was recovered to the Robinson Helicopter Company facility in Torrance, California, for a detailed examination. No discrepancies were noted, apart from impact related damage, in the assembly, installation or alignment of the engine, clutch assembly or actuator assembly. No evidence of pre-impact damage to the flight and powerplant controls was found. The failed belt was found separated between the vees with only a 5-inch section still intact.

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: flight instructor, commercial pilot
  • Ratings: instructor: helicopter; rotorcraft: helicopter
  • Flight time: 1,351 hours in all; 1,230 in this make and model; 114 in the last 90 days; 57 in the last 30 days; 1,255 as pilot in command; 927 on instruments
  • Last flight review: June 1, 2001
  • Medical certificate: Class 2 (valid medical--no waivers/lim.)
  • Seat: rgt
  • Injury: no injuries

Co-pilot

  • Certificate: private
  • Ratings: single-engine land; rotorcraft: helicopter
  • Flight time: 295 hours in all; 75 in this make and model; 33 in the last 90 days; 24 in the last 30 days; 195 as pilot in command
  • Medical certificate: Class 3 (with waivers/limitations)
  • Seat: left
  • Injury: minor injuries

The aircraft

  • Airframe total time: 19.9 hours
  • Last inspection: inspection type not recorded; 19.9 hours since
  • Maximum gross weight: 1,370 lb
  • Seats: 2
  • Landing gear: fixed
  • Engine: Lycoming O-360-J2A (piston); 0 hours total
  • Operator: Robinson Helicopters Company

The flight

  • Departed from: T27 El Paso TX at 6:00 pm
  • Destination: FST Fort Stockton TX
  • Flight plan: none
  • A second pilot was aboard

Weather at the time

  • Light: daylight
  • Wind: from 290° at 12 knots, gusting 19
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 27°F (-3°C), dew point -4°F (-20°C)
  • Altimeter: 29.94 inHg
  • Observation at 7:53 pm from KFST, 67 miles away

Injuries

FatalSeriousMinorNone
Crew1
Passengers1

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.