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Accidents · NTSB CEN09FA012 · Final report

Bell 206 accident near Conroe, Texas, October 13, 2008

On October 13, 2008 at about 4:09 pm local time, a Bell 206 (helicopter), registered N6ZV, was destroyed in an accident during maneuvering near Conroe, Texas. It was an aerial observation flight under general aviation rules (Part 91). 2 people were killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

A loss of control for undetermined reasons.

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

What the record shows

Date
October 13, 2008 · about 4:09 pm local time
Place
Conroe, Texas · map
Type
Accident
Injuries
2 people were killed.
Weather
visual conditions (good weather)
Aircraft
Bell 206 L-4 · all 206s on the register
Registration
N6ZV · no longer on the register · serial 52046
Damage
Destroyed
Flight
Aerial observation flight · general aviation rules (Part 91)

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

**This report was modified on June 28, 2010, and May 11, 2015. Please see the public docket for this accident to view the original report.** The news helicopter was en route to cover a breaking news story. Witnesses saw the helicopter flying approximately 350 feet above the ground when it nosed over and entered a sharp 70-degree bank and dove towards the ground. The helicopter was equipped with a video camera. Analysis of the video revealed a "small perturbation in yaw (nose towards the left) followed by a return back to the right of equal magnitude." The perturbation was "no larger or faster" than other yaw motions seen previously during the flight. About two seconds later, the helicopter began a slow, smooth roll to the right and the ground was no longer visible. The helicopter came down through trees at a 72-degree impact angle. The right skid was embedded in the ground at a 25-degree angle. Both main rotor blades bore evidence of tree strikes. The clevis ends of the pitch change tubes remained attached to their respective horns. The pitch and collective control rods remained attached to their linkages, and the linkages were attached to their respective servos. Flight control continuity was established between the control rods and the servos but could not be established beyond the servos because of impact forces and a postcrash fire. One tail rotor blade was straight and the other blade was bent 90 degrees to the plane of rotation. There was no evidence of a main rotor blade strike against the horizontal stabilizer, synchronized elevator, or finlets or tail boom. Tail rotor continuity was established. Examination of the engine revealed the Pg line was only finger tight. Later pressure testing of the Pg line disclosed no leaks. The transmission, main drive shaft, and freewheeling unit were disassembled and inspected. No anomalies were noted. The autopsy of the pilot identified areas of moderate to severe (up to 85 to 90 percent) occlusion of the coronary arteries and a small area of scar in the cardiac muscle, but the significance of these findings to the accident could not be conclusively determined. Although it is clear that the pilot had significant coronary disease, which placed him at risk for an acute coronary event, there is no way to determine, on the basis of the available evidence, whether the pilot actually suffered such an event during the accident flight.  The observations from witnesses, analysis of the wreckage and impact evidence, and test results indicated a loss of control occurred. However, the investigation could not determine the reason for the loss of control.

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 control in flight during maneuvering defining event
  2. Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent

The NTSB's findings

  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Lateral/bank control › Not attained/maintained
  • cause Not determined › Not determined › (general) › (general) › Unknown/Not determined
  • Personnel issues › Physical › Health/Fitness › Predisposing condition › Pilot

Pilot

  • Certificate: commercial pilot
  • Ratings: multi-engine land; single-engine land; instrument: airplane; instrument: helicopter; rotorcraft: helicopter
  • Flight time: 6,105 hours in all; 2,450 in this make and model; 240 in the last 90 days; 90 in the last 30 days
  • Last flight review: May 28, 2008
  • Medical certificate: Class 2
  • Seat: rgt
  • Injury: fatal

The aircraft

  • Airframe total time: 7,992 hours
  • Last inspection: 100-hour inspection, October 6, 2008; 14 hours since
  • Maximum gross weight: 4,150 lb
  • Seats: 5
  • Landing gear: fixed
  • Engine: Rolls Royce 250-C30P (turboshaft); 0 hours total
  • Fire on the ground
  • Operator: Helicopters, Inc.

The flight

  • Departed from: HOU Houston TX at 3:40 pm
  • Destination: HOU Houston TX
  • Flight plan: none

Weather at the time

  • Light: daylight
  • Wind: from 130° at 7 knots
  • Visibility: 10 statute miles
  • Sky: scat at 2,600 ft
  • Temperature: 81°F (27°C), dew point 72°F (22°C)
  • Altimeter: 30.12 inHg
  • Observation at 4:48 pm from IAH

Injuries

FatalSeriousMinorNone
Flight 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.