Socata TBM 700 accident near Hollywood, Florida, October 12, 2011
On October 12, 2011 at about 5:34 pm local time, a 2008 Socata TBM 700, registered N37SV, was substantially damaged in an accident during approach (VFR pattern final) near Hollywood, Florida (North Perry Airport). It was a flight test under general aviation rules (Part 91). 2 people had minor injuries. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot’s failure to terminate the flight after observing multiple conflicting errors associated with the inaccurate right fuel quantity indication. Contributing to the accident were the total loss of engine power due to fuel starvation from the right tank, the inadequate manufacturing of the right fuel gauge electrical harness, and failure of maintenance personnel to recognize and evaluate the reason for the changing fuel level in the right fuel tank.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- October 12, 2011 · about 5:34 pm local time
- Place
- Hollywood, Florida · North Perry Airport · map
- Type
- Accident
- Injuries
- 2 people had minor injuries.
- Weather
- visual conditions (good weather)
- Aircraft
- Socata TBM 700, built 2008 · all TBM 700s on the register
- Registration
- N37SV · no longer on the register · serial 441
- Damage
- Substantial damage
- Flight
- Flight test · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
In anticipation of the maintenance test flight, a about 72 gallons of fuel was added to the left fuel tank to balance the fuel load. During the preflight, the pilot noted that the left tank had 105 gallons and that the right tank had 108 gallons. Because of the fuel level indications, the pilot did not visually inspect the tanks; even if he had done so the wing dihedral would have prevented him from seeing the fuel level. About 20 minutes after takeoff, the pilot received the first annunciation of "Fuel Low R," which lasted for about 10 seconds then went out. This indicates the fuel quantity is less than or equal to 9 gallons of usable fuel in the right tank. The pilot attributed this to a malfunction of the low fuel level sensor, since the fuel gauge showed about 98 gallons of fuel. He instructed the right front seat occupant (the mechanic) to make a note so the sensor would be replaced after the flight. Shortly thereafter, the amber "Fuel Unbalance" illuminated, and indicated that the right fuel quantity was greater than the left; as a result the pilot switched the fuel selector to the right tank. He then initiated a descent to 10,000 feet to perform system checks, and after levelling off at that altitude for about 15 minutes, received a second "Fuel Low R" annunciation; he verified that the fuel selector automatically switched to the left tank and noted that the message went out after about 10 seconds. Either before or during a descent to 4,000 feet, the second "Fuel Unbalance" annunciation occurred. The right tank again depicted a greater quantity of fuel, so the pilot again switched the fuel selector to the right tank. The flight continued to a nearby airport, where the pilot terminated an instrument approach with a low approach. The flight then proceeded to the destination airport and entered the traffic pattern on a left downwind leg.. While on the downwind leg, the pilot received the third "Fuel Unbalance" annunciation and at this time the left fuel gauge indicated 55 gallons while the right fuel gauge indicated 74 gallons. Because he intended to land within a few minutes, the pilot manually selected the fullest (right) tank, then turned to base then final. While at 800 feet on final approach, the red warning message "Fuel Press" illuminated and the engine lost all power. Attempts to restore engine power were unsuccessful. Unable to reach the airport, the pilot landed on a nearby turnpike. Both fuel tanks were breached, and fuel leakage, likely from the left fuel tank, was noted at the site. Inspection of the fuel outlet filter on the engine and the fuel sequencer reservoir considered an airframe item revealed both contained minimal fuel consistent with fuel starvation from the right fuel tank that actually did not contain an adequate supply of fuel. Postaccident operational testing of the engine revealed no evidence of preimpact failure or malfunction that would have resulted in the loss of power. Examination and testing of the right fuel gauge harness revealed that a high impedance shielded cable was not correctly soldered to the shielding braid when the airplane was manufactured, which resulted in erroneous high readings of the fuel quantity in the right tank. Several opportunities existed to detect the fuel quantity errors in the right tank during the airplane's 600-hour and annual inspection, which was signed off the day before. Several times during the inspection, electrical power was applied and different fuel quantities for the right tank were displayed, yet nothing was done to determine the reason for the different fuel indications. For example, 41 gallons was displayed, yet 70 gallons was drained; the fuel was returned to the tank after maintenance, yet the gauge showed 51 gallons, and after a post-maintenance run was performed, the gauge showed over 140 gallons even though it hadn't been fueled. Maintenance personnel incorrectly attributed the difference to fuel migration. Further, the pilot had the opportunity to terminate the test flight after multiple conflicting indications from the right tank, yet he continued the test flight, which resulted in fuel starvation.
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
- Loss of engine power (total) during approach (VFR pattern final) defining event
- Off-field or emergency landing during emergency descent
- Hard landing during landing (flare/touchdown)
- Collision with terrain or object (not controlled flight into terrain) during landing (flare/touchdown)
The NTSB's findings
- cause Personnel issues › Action/decision › Info processing/decision › Understanding/comprehension › Pilot
- cause Personnel issues › Task performance › Use of equip/info › Use of available resources › Pilot
- cause Aircraft › Aircraft systems › Fuel system › Fuel indication system › Malfunction
- factor Aircraft › Fluids/misc hardware › Fluids › Fuel › Fluid level
- factor Organizational issues › Development › Manufacture/production › Equipment manufacture › Manufacturer
- factor Personnel issues › Action/decision › Info processing/decision › Understanding/comprehension › Maintenance personnel
- factor Aircraft › Aircraft systems › Fuel system › Fuel indication system › Incorrect service/maintenance
- factor Aircraft › Aircraft systems › Fuel system › Fuel indication system › Design
- Environmental issues › Physical environment › Terrain › (general) › Contributed to outcome
Pilot
- Certificate: airline transport pilot
- Ratings: single-engine land; instrument: airplane
- Flight time: 11,071 hours in all; 4,053 in this make and model; 102 in the last 90 days; 61 in the last 30 days; 10,415 as pilot in command; 3,267 on instruments
- Last flight review: February 1, 2010
- Medical certificate: Class 1 (without waivers/limitations)
- Seat: left
- Injury: minor injuries
Other crew
- Certificate: commercial pilot, flight engineer
- Ratings: multi-engine land; single-engine land; instrument: airplane
- Flight time: 2,500 hours in all; 5 in this make and model; 2,400 as pilot in command
- Medical certificate: Class 2 (without waivers/limitations)
- Seat: rgt
- Injury: minor injuries
The aircraft
- Airframe total time: 593 hours
- Last inspection: annual inspection, October 12, 2011; 2 hours since
- Maximum gross weight: 7,400 lb
- Seats: 6
- Landing gear: retractable
- Engine: P&W PT6A-66D (turboprop); 595 hours total
- Operator: Socata North America, Inc.
The flight
- Departed from: HWO Hollywood FL at 4:16 pm
- Destination: HWO Hollywood FL
- Flight plan: IFR
- Runway 27L, 3,255 ft by 100 ft
- A second pilot was aboard
Weather at the time
- Light: daylight
- Wind: from 230° at 6 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 86°F (30°C), dew point 68°F (20°C)
- Altimeter: 29.85 inHg
- Observation at 5:35 pm from HWO, 1 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 2 |
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.
