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Accidents · NTSB ENG06IA020 · Final report

Raytheon Corporate Jets Beechjet 400A incident near Norfolk, Virginia, June 14, 2006

On June 14, 2006 at about 8:15 pm local time, a Raytheon Corporate Jets Beechjet 400A, registered N440DS, was involved in an incident near Norfolk, Virginia. It was a positioning flight under general aviation rules (Part 91). No one was hurt; 2 people were on board or involved.

The NTSB's probable cause their words, unchanged

High-altitude ice crystals that had accreted on the compressor vanes and were ingested into the engine high pressure compressor when the pilots retarded the power levers causing compressor surges and the flameouts of both engines. Contributing factors were the lack of training on the hazards of high-altitude ice crystals to gas turbine engines and guidance to the pilots to activate the engine anti-ice system in conditions where high-altitude ice crystals may exist.

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

What the record shows

Date
June 14, 2006 · about 8:15 pm local time
Place
Norfolk, Virginia · map
Type
Incident
Injuries
No one was hurt; 2 people were on board or involved.
Weather
not recorded
Aircraft
Raytheon Corporate Jets Beechjet 400A
Registration
N440DS · no longer on the register · serial RK-8
Damage
Not recorded
Flight
Positioning flight · general aviation rules (Part 91)

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

The Raytheon Beechjet 400A was cruising at flight level 380 when both of the engines flamed out after the pilots had reduced power prior to turning on the engine anti-ice systems. The airplane was in visual meteorological conditions (VMC), but were approaching clouds that were known to remnants of a tropical storm. The pilots were unsure if they could remain in VMC and had decided to turn on the engine anti-ice. In accordance with the airplane flight manual (AFM) procedures, the pilots reduced the power to 89.5 percent N1 and both engines flamed out. The left and right engines restarted on their own as the airplane descended through FL 300 and 240, respectively. Testing of the airplane and engines immediately after the incident revealed that they were operating correctly. Testing of the fuel revealed that it conformed to the specifications for Jet A and the concentration of the fuel system icing inhibitor was within limits. Weather satellite imagery showed that there were convective weather cells in the area where the airplane's engines flamed out. Convective weather can lift significant amounts of water into the upper atmosphere that then form ice crystals. Research indicates that the ice crystals can partially melt passing through the JT15D-5 engine fan that can then accrete to an internal compressor stator. When any accreted ice was shed from the stator vanes, it would pass through the high pressure compressor and could be picked up by the pressure sense line to the fuel control. Flight tests confirmed that sense line could go below freezing at low power settings at high altitude. Tests also show that if the sense line was blocked and the power levers were retarded, the electronic engine control would reduce the fuel flow to reduce the power, but the sense pressure within the fuel control would be maintained. But when the blockage was cleared, the sudden reduction in the sense pressure in the fuel control would result in a reduction of the fuel flow at a rate that was much faster than a normal rapid power reduction and could result in the engine flaming out.

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

Pilot

  • Certificate: airline transport pilot
  • Ratings: multi-engine land
  • Seat: left
  • Injury: no injuries

Crew member

  • Seat: rgt

The aircraft

  • Maximum gross weight: 16,300 lb
  • Seats: 10
  • Landing gear: fixed
  • Engine 1: Pratt & Whitney Canada JT15D-5 (turbofan); 0 hours total
  • Engine 2: Pratt & Whitney Canada JT15D-5 (turbofan); 0 hours total
  • Operator: Southern Air Systems

The flight

  • Departed from: OQU Quonset Point RI
  • Destination: CHS Charleston SC
  • Flight plan: IFR
  • A second pilot was aboard

Weather at the time

  • Temperature: 0°F (-18°C), dew point 0°F (-18°C)

Injuries

FatalSeriousMinorNone
Crew2

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.