Skip Ribbon Commands
Skip to main content
Full Narrative

Quick Launch
NTSB Identification: ENG04IA021
HISTORY OF FLIGHT

On July 12, 2004, about 1210 eastern daylight time, a Raytheon Beechjet 400A airplane, N455CW, operated by Flight Options of Cleveland Ohio, experienced a dual-engine flameout of the Pratt & Whitney Canada (PWC) JT15D-5 engines while descending through flight level (FL) 390 over the Gulf of Mexico about 100 miles west of Sarasota, Florida. The pilots, after several attempts, were able to get the right engine restarted as they descended through 10,000 feet and diverted to Sarasota for landing without further incident. Daytime instrument meteorological conditions (IMC) prevailed at the time the engines lost power. The airplane was operating on an instrument flight rules flight plan under 14 CFR Part 135 from Duncan, Oklahoma to Fort Myers, Florida. The two pilots and seven passengers on board were not injured.

The pilots stated that they were cruising at FL 410 in IMC and air traffic control (ATC) cleared the airplane to descend to FL 330. As the airplane was passing through FL 390, the pilots felt a jolt and heard a bang and about 30 seconds later, they realized the airplane was losing cabin pressure. They donned their oxygen masks, declared an emergency, and went through the emergency descent checklist that included confirming the passengers' oxygen masks had been released and were being used. The pilots stated that as the airplane was passing through FL 350, they noticed that every warning light in the cockpit was illuminated and that the engines were not operating. After several unsuccessful attempts to restart the engines, the pilots were able to get the right engine restarted as the airplane descended through 10,000 feet.

TESTS AND RESEARCH

Following the incident, the airplane and engines were tested and no discrepancies were noted. Fuel from the airplane underwent tests at a petrochemical laboratory that revealed the fuel conformed to the requirements for Jet A. But the tests also revealed the concentration of the fuel system icing inhibitor (FSII) was 0.02 percent. Although FSII is not a requirement for Jet A, the Beechjet 400A airplane flight manual (AFM) specifies that the airplane's fuel must have an FSII in concentrations of 0.1 to 0.15 percent.

At the time the engines flamed out, the airplane was in IMC. Weather satellite imagery revealed there were convective weather cells in the area where the airplane's engines flamed out. According to the Federal Aviation Administration's (FAA) engine icing expert, convective weather can lift significant amounts of moisture into the upper atmosphere and the blow off from the tops of these convective storms can contain significant amounts of ice crystals.

PWC did a study to determine if high altitude ice crystals could adhere to the inside of a JT15D-5 engine to the point that it would flame out. The study revealed that it was possible for ice crystals to partially melt passing through the fan and with the anti-ice turned off, to accrete on the leading edges of the front inner compressor stator vanes. Any change in engine speed would change the airflow's angle of incidence over the stators causing any accreted ice to be blown off of the stator vane. The study showed that if a significant amount of ice had accreted on the stator vanes and was blown off, it could result in the engine surging and possibly flaming out. In addition, any ice that may have accreted within the engine would degrade the engine's compressor efficiency, surge margin, and relight capability. Additionally, the ice that was blown off of the stator vanes would melt passing through the high pressure compressor that could be then picked up by the P3 (compressor discharge pressure) line that goes to the fuel control.

Raytheon conducted a flight test of a Beechjet 400A airplane that had thermocouples installed on the P3 line adjacent to the fuel control on one engine. The testing revealed that the temperature of the line would go below freezing at low power settings when the engine was operated in ambient conditions like those when the airplane's engines flamed out. PWC developed a rig test to simulate the effect of a blocked P3 line. The testing revealed that if the line was blocked when the power lever was retarded, the electronic engine control would reduce the fuel flow even though the pressure was maintained in the fuel control P3 bellows. When the line became unblocked, either by the pressure differential or the melting of an ice blockage, the sudden drop in the P3 bellows pressure resulted in the fuel flow dropping faster than in a normal rapid engine deceleration that could result in the engine flaming out.

The Safety Board issued Urgent Safety Recommendation A-06-56 that requested the FAA to Beechjet 400 pilots to activate the engine anti-ice at high altitudes whenever they were in or near visible moisture or convective storm activity. On September 15, 2006, Raytheon issued a temporary change to the Beechjet 400 AFM that provided guidelines for turning on the engine anti-ice at high altitudes when in the vicinity of visible moisture and convective storm activity. The FAA issued Airworthiness Directive 2006-21-02 that required operators of Beechjet 400 airplanes to incorporate the temporary revision into their airplanes AFM.