Rockwell 500 accident near Pembroke Park, Florida, August 28, 2020
On August 28, 2020 at about 1:02 pm local time, a 1969 Rockwell 500, registered N900DT, was destroyed in an accident during enroute (cruise) near Pembroke Park, Florida. It was an instructional 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 total loss of engine power due to fuel exhaustion. Contributing to the fuel exhaustion was the fatigue fracture of an electrical wire in the tank unit or fuel transmitter, which likely resulted in an inaccurate fuel quantity indication.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- August 28, 2020 · about 1:02 pm local time
- Place
- Pembroke Park, Florida · map
- Type
- Accident
- Injuries
- 2 people were killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Rockwell 500 S, built 1969
- Registration
- N900DT · no longer on the register · serial 3056
- Damage
- Destroyed
- Flight
- Instructional flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The pilot-in-command seated in the right seat was providing familiarization in the multi-engine airplane to the left seat pilot during a flight to a nearby airport for fuel. Shortly after takeoff, one of the pilots reported an engine problem and advised that they were diverting to a nearby airport. A witness along the route of flight reported hearing the engines accelerating and decelerating and then popping sounds; several witnesses near the accident site reported hearing no engine sounds. The airplane impacted a building and terrain about 10 minutes after takeoff. Very minimal fuel leakage on the ground was noted and only 23 ounces of aviation fuel were collected from the airplane’s five fuel tanks. No evidence of preimpact failure or malfunction was noted for either engine or propeller; the damage to both propellers was consistent with low-to-no power at impact. Since the pilot could not have visually verified the fuel level in the center fuel tank because of the low quantity of fuel prior to the flight, he would have had to rely on fuel consumption calculations since fueling based on flight time and the airplane’s fuel quantity indicating system. Although the fuel quantity indications at engine start and impact could not be determined postaccident from the available evidence, if the fuel quantity reading at the start of the flight was accurate based on the amount of fuel required for engine start, taxi, run-up, takeoff, and then only to fly the accident flight duration of 10 minutes, it would have been reading between 8 and 10 gallons. It is unlikely that the pilot, who was a chief pilot of a cargo operation and tasked with familiarizing company pilots in the airplane, would have knowingly initiated the flight with an insufficient fuel load for the intended flight or with the fuel gauge accurately registering the actual fuel load that was on-board. Examination of the tank unit, or fuel quantity transmitter, revealed that the resistance between pins A and B, which were the ends of the resistor element inside the housing, fell within specification. When monitoring the potentiometer pin C, there was no resistance, indicating an open circuit between the wiper and the resistor element. X-ray imaging revealed that the conductor of electrical wire was fractured between the end of the lugs at the wiper and for pin C. Bypassing the fractured conductor, the resistive readings followed the position of the float arm consistent with normal operation. Visual examination of the wire insulation revealed no evidence of shorting, burning or damage. Examination of the fractured electrical conductor by the NTSB Materials Laboratory revealed that many of the individual wires exhibited intergranular fracture surface features with fatigue striations in various directions on some individual grains. It is likely that the many fatigue fractured conductor strands of the electrical wire inside the accident tank unit or fuel transmitter resulted in the fuel gauge indicating that the tanks contained more fuel than the amount that was actually on board, which resulted in inadequate fuel for the intended flight and a subsequent total loss of engine power due to fuel exhaustion. The inaccurate fuel indication would also be consistent with the pilot’s decision to decline additional fuel before departing on the accident flight. While the estimated fuel remaining since fueling (between 15 and 51 gallons) was substantially more than the actual amount on board at the start of the accident flight (between 8 and 10 gallons), the difference could have been caused by either not allowing the fuel to settle during fueling, and/or the operational use of the airplane. Ultimately, the fuel supply was likely completely exhausted during the flight, which resulted in the subsequent loss of power to both engines. Given the circumstances of the accident, the effects from the right seat pilot’s use of cetirizine and the identified ethanol in the left seat pilot, which was likely from sources other than ingestion, did not contribute to this accident.
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
- Off-field or emergency landing during emergency descent
- Fuel exhaustion during enroute (cruise) defining event
- Collision with terrain or object (not controlled flight into terrain) during landing
The NTSB's findings
- Aircraft › Fluids/misc hardware › Fluids › Fuel › Fluid level
- Aircraft › Aircraft systems › Fuel system › Fuel quantity sensor › Fatigue/wear/corrosion
Other crew
- Certificate: commercial pilot
- Ratings: multi-engine land; single-engine land; instrument: airplane
- Flight time: 27,780 hours in all; 300 in this make and model; 249 in the last 90 days; 52 in the last 30 days; 18,700 as pilot in command; 9,080 on instruments
- Last flight review: July 7, 2020
- Medical certificate: Class 2 (with waivers/limitations)
- Seat: rgt
- Injury: fatal
Other crew
- Certificate: airline transport pilot
- Ratings: multi-engine land; instrument: airplane
- Flight time: 8,029 hours in all; 209 in the last 90 days; 46 in the last 30 days; 3,793 as pilot in command
- Last flight review: September 18, 2019
- Medical certificate: Class 1 (without waivers/limitations)
- Seat: left
- Injury: fatal
The aircraft
- Airframe total time: 10,300.9 hours
- Last inspection: annual inspection, August 14, 2020
- Maximum gross weight: 6,750 lb
- Seats: 7
- Landing gear: retractable
- Engine 1: Lycoming IO-540-E1B5 (piston); 5,371 hours total
- Engine 2: Lycoming IO-540-E1B5 (piston); 5,371 hours total
- Operator: Conquest Air
The flight
- Departed from: PMP Pompano Beach FL at 12:52 pm
- Destination: OPF Miami FL
- Flight plan: none
- A second pilot was aboard
Weather at the time
- Light: daylight
- Wind: from 140° at 8 knots
- Visibility: 10 statute miles
- Sky: broken clouds at 12,000 ft; scat at 3,000 ft
- Temperature: 88°F (31°C), dew point 81°F (27°C)
- Altimeter: 30.09 inHg
- Observation at 12:53 pm from HWO, 4 miles away
Weather report (METAR): KHWO 281253Z 14008KT 10SM SCT030 BKN120 31/27 A3009 RMK AO2 SLP188 T03060267
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 | |||
| Passengers | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
45 documents, released by the NTSB on September 13, 2022. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.
The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.
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.
