Diamond Aircraft Ind INC DA 40 NG accident near Sanford, North Carolina, May 7, 2025
On May 7, 2025 at about 8:00 pm local time, a 2018 Diamond Aircraft Ind INC DA 40 NG, registered N499BW, was substantially damaged in an accident during initial climb near Sanford, North Carolina (Raleigh Exec Jetport At Sanfor airport). It was a personal flight under general aviation rules (Part 91). 2 people were seriously injured. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The mechanic’s re-use of worm drive clamps, which resulted in a separation of the turbocharger air discharge duct and a partial loss of engine power during initial climb.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- May 7, 2025 · about 8:00 pm local time
- Place
- Sanford, North Carolina · Raleigh Exec Jetport At Sanfor · map
- Type
- Accident
- Injuries
- 2 people were seriously injured.
- Weather
- visual conditions (good weather)
- Aircraft
- Diamond Aircraft Ind INC DA 40 NG, built 2018
- Registration
- N499BW · registry record · serial 40.NC020
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The purpose of the accident flight was for the pilot and the mechanic, who was the passenger on the accident flight, to go on a short test flight after the airplane’s most recent annual inspection. The pilot reported that he performed one circuit of the airport traffic pattern, which was uneventful. During the second circuit, he decided to perform a touch-and-go landing, but the airplane bounced, so he decided to abort the landing. During the initial climb the mechanic heard a “pop,” and shortly thereafter the pilot noticed the engine speed decreased and the airplane lost partial engine power. To avoid trees, the pilot attempted to return to another runway and land, but the airplane descended and impacted a field short of the runway. Postaccident examination of the airplane revealed that the turbocharger air discharge duct had separated from the engine (this duct provided turbocharged intake air to the diesel engine). One of the two worm drive clamps that would have secured the duct to its mating hose was found separated and unsecured. The worm drive’s screw was worn and loose in the clamp housing, consistent with reuse. No evidence of any other preaccident mechanical malfunctions or failures of the engine were found during the examination. Data recovered from the engine control unit (ECU) revealed that the engine boost pressure dropped to ambient pressure during the initial climb, about the same time that the mechanic reported hearing the “pop.” Because the diesel engine relied on turbocharged intake air for power, disconnection of the turbocharger air discharge duct would have resulted in a significant loss of engine power consistent with the partial loss of engine power described by the pilot. The mechanic stated that during the airplane’s most recent annual inspection, he had removed the turbocharger air discharge ductwork, and that when he reinstalled it, he reused the worm drive clamps (rather than using new clamps as prescribed by the airplane’s maintenance manual). Given the worn and loose condition of the unsecured clamp’s worm drive found during the wreckage examination, it is likely that the reused clamp loosened during the accident flight, resulting in the turbocharger air discharge duct’s separation and the partial loss of engine power during the initial climb.
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
- Powerplant sys/comp malf/fail during initial climb defining event
- Loss of control in flight during initial climb
- Aerodynamic stall/spin during initial climb
- Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent
The NTSB's findings
- Personnel issues › Task performance › Maintenance › Scheduled/routine maintenance › Maintenance personnel
- Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
- Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Angle of attack › Capability exceeded
- Aircraft › Aircraft power plant › Turbocharging (recip only) › (general) › Incorrect service/maintenance
Pilot
- Certificate: private
- Ratings: single-engine land
- Flight time: 1,830 hours in all; 1,830 in this make and model; 30 in the last 90 days
- Last flight review: August 13, 2024
- Medical certificate: Class 2 (without waivers/limitations)
- Seat: left
- Injury: serious injuries
The aircraft
- Airframe total time: 1,025.4 hours
- Last inspection: annual inspection, April 25, 2025
- Maximum gross weight: 2,897 lb
- Seats: 4
- Landing gear: fixed
- Engine: Austro E4-A (piston); 969 hours total
The flight
- Flight plan: none
- Runway 21, 6,501 ft by 100 ft
Weather at the time
- Light: daylight
- Wind: from 270° at 4 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 77°F (25°C), dew point 54°F (12°C)
- Altimeter: 30.04 inHg
- Observation at 4:05 pm from TTA, 1 miles away
Weather report (METAR): KTTA 072005Z AUTO 27004KT 10SM CLR 25/12 A3004 RMK AO2 T02450121
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 | |||
| Passengers | 1 |
Photographs from the investigation 3 pictures from the NTSB's docket, as the NTSB released them
Photograph 1 – main wreckage
Photograph 2 – Main wreckage
Photograph 3 – Engine, note: Air discharge duct missing.The NTSB's photographs with the NTSB's captions, at screen size. Open a picture to see it full size or to report one that should not be shown.
Documents from the investigation the NTSB's docket: the evidence folder behind the report
14 documents, released by the NTSB on September 18, 2026. 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.
