Bell Helicopter Textron Canada 407 accident near Decatur, Texas, December 25, 2009
On December 25, 2009 at about 7:00 pm local time, a Bell Helicopter Textron Canada 407, registered N600CE, was substantially damaged in an accident during takeoff near Decatur, Texas (Wise Regional Health System airport). It was a positioning flight under general aviation rules (Part 91). 2 people were seriously injured and 1 person had minor injuries. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot's inadequate preflight inspection and the momentary loss of engine power due to snow or ice ingestion.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- December 25, 2009 · about 7:00 pm local time
- Place
- Decatur, Texas · Wise Regional Health System · map
- Type
- Accident
- Injuries
- 2 people were seriously injured and 1 person had minor injuries.
- Weather
- visual conditions (good weather)
- Aircraft
- Bell Helicopter Textron Canada 407 · all 407s on the register
- Registration
- N600CE · no longer on the register · serial 53347
- Damage
- Substantial damage
- Flight
- Positioning flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The pilot, flight medic, and flight nurse were departing from a hospital helipad for the purpose of a cross-country positioning flight. As the helicopter ascended about 50 to 60 feet above ground level (agl), the pilot heard two warning horns sound, followed by the helicopter yawing 90 degrees to the left. The pilot lowered the collective in an effort to preserve rotor rpm and maneuvered the helicopter back over the helipad. Around 5 to 8 feet agl the pilot increased collective pitch, but the helicopter continued a quick descent until it experienced a hard landing back on the helipad. A review of hospital video surveillance footage for the 24 hours prior to the accident revealed that the helicopter remained parked outside for approximately 5 hours in blowing snow conditions; during this time, it was not equipped with plugs or covers over the engine inlets or the exhaust. The plugs and covers were installed later and the helicopter remained outside in temperatures ranging from 16 degrees Fahrenheit (F) to 34 degrees F for the next 19 hours. The video also revealed that at no time did anybody look at the exhaust stack, right side engine intake, or open any access panels prior to the operation of the helicopter. An examination of the recorded Engine Control Unit (ECU) data revealed that during the flight, the helicopter’s engine experienced a momentary flameout followed by a successful relight. Although the engine power was increasing, due to the helicopter’s close proximity to the ground, the pilot was unable to recover main rotor rpm before ground impact. As part of the postaccident examination, the engine was removed from the airframe and an engine run was performed. There were no anomalies found with the airframe or engine that would have contributed to the loss of engine power. The operator’s procedure manual stated that the pilot must ensure that all ice, snow, and frost is removed from the engine inlet area. The helicopter manufacture’s flight manual stated that as part of the preflight inspection, the pilot must check that the engine inlet area is cleaned of all debris, accumulated snow and ice. The engine manufacturer’s Operation and Maintenance Manual gave a precaution that the accumulation of snow or ice may result in the engine experiencing a flameout.
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
- Aircraft inspection event during prior to flight
- Loss of engine power (total) during takeoff defining event
- Autorotation Loss of engine power (total)
- Hard landing during landing
The NTSB's findings
- cause Aircraft › Aircraft power plant › Engine (turbine/turboprop) › (general) › Inadequate inspection
- cause Environmental issues › Conditions/weather/phenomena › Ceiling/visibility/precip › Snow › Effect on equipment
Pilot
- Certificate: commercial pilot
- Ratings: instrument: helicopter; rotorcraft: helicopter
- Flight time: 3,191 hours in all; 997 in this make and model; 21 in the last 90 days; 4 in the last 30 days; 3,044 as pilot in command
- Last flight review: February 5, 2009
- Medical certificate: Class 2 (without waivers/limitations)
- Seat: frt
- Injury: serious injuries
The aircraft
- Airframe total time: 4,500 hours
- Last inspection: approved inspection programme, December 17, 2009
- Maximum gross weight: 5,250 lb
- Seats: 5
- Landing gear: fixed
- Engine: Allison 250-C47B (turboshaft); 0 hours total
- Operator: Air Evac Ems INC
The flight
- Departed from: XA57 Decatur TX at 6:58 pm
- Destination: Wichita Falls TX
Weather at the time
- Light: daylight
- Wind: from 250° at 6 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 34°F (1°C), dew point 32°F (0°C)
- Altimeter: 30.02 inHg
- Observation at 6:46 pm from LUD, 2 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 2 | 1 |
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.
