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In aviation a flameout refers to the run-down of a jet engine caused by the extinction of the flame in the combustion chamber. It can be caused by a number of factors, including fuel starvation, compressor stall, insufficient oxygen (at high altitudes), foreign object damage (such as caused by birds, hail or volcanic ash), severe inclement weather, mechanical failure and very cold ambient temperatures.[1][2]


A flameout is believed to be most likely to occur when flying through certain weather conditions at a low power setting such as flight idle (e.g. during the descent). These conditions include flight through moderate to heavy turbulence, rain, hail or sleet. The potentially hazardous circumstances are highlighted in the flight manual with a requirement to select continuous ignition. Alternatively, the FADEC engine controller will select ignition automatically if it detects specific changes in engine parameters. It will also perform a relight if necessary. A manual re-light attempt is made by following the procedure in the Flight Operations Manual.[3]

Early jet engines, such as Junkers Jumo 004 used in early German jets, including the Messerschmitt Me 262, were at relatively high risk of flameout. Fast acceleration or inappropriate throttle settings could impoverish the fuel/air mixture causing a flameout. If this happened at low altitude, it would often lead to the total loss of the aircraft. However, jet engines were developed to be controlled with a governor, a centrifugal feedback valve for controlling the speed of the engine - sometimes referred to as FCU (Fuel Control Unit) or HMU (Hydro-Mechanical Unit) - allowing controlled fuel metering proportional to the engine's rotational speed. Current modern engines are engineered to a higher degree of technical quality controlled by digital electronic systems (FADEC) that constantly fine-tune their performance; thus such flameouts are not as common as they were in the early days of jet-powered aviation.

It is common practice for pilots to be taught and to practice flameout landings.[4]

Windmill restart[edit]

In-flight restarts are designated as either windmill or starter-assisted, depending where in the flight envelope the restart is attempted. The re-light envelope occupies the lower part of the flight envelope below about 30,000 ft (28,000 ft in the case of a Boeing 747, which experienced flameouts at 37,000 ft[5]). When an appropriate initial altitude and forward speed are available, the mass airflow through the compressor blades can maintain sufficient rotational velocity for enough time to permit restart. If the aircraft's operating conditions are not sufficient for a windmill start, the engine's starter motor must be operated to increase the turbine velocity to the minimum required speed.[6]

Notable incidents of flameout[edit]

Engine flameout due to inclement weather and volcanic activity[edit]

Engine flameout due to fuel starvation[edit]

  • On July 23, 1983, Air Canada Flight 143, a Boeing 767, ran out of fuel, causing both of its engines to flameout. The pilot was able to glide the plane to safety, landing it on an auto racing track which was previously the RCAF Station Gimli. Hence the aircraft involved is known as the Gimli Glider.
  • On August 24, 2001, Air Transat Flight 236, operated by an Airbus A330, experienced a flame out on both of its engines due to fuel starvation. The plane continued to glide until it landed safely in Azores. All 306 passengers and crew on board the plane were unharmed.
  • On 29 November 2013, a Police Scotland Eurocopter EC135-T2+ experienced a double engine flameout and crashed into a Glasgow pub, the Clutha Vaults. Three persons in the aircraft and seven on the ground were killed; an additional 32 were injured. Both engines flamed out about 32 seconds apart due to fuel starvation.[7]

Engine flameout due to mechanical problems[edit]

  • On 19 February 1985, China Airlines Flight 006, a Boeing 747SP, operating from Taipei to Los Angeles plunged 30,000 ft (9,100m) after the plane's fourth engine flamed out. The pilots managed to recover the plane in the nick of time and the flight was diverted to San Francisco International Airport without further incident. Two passengers were seriously injured as a result of the plunge. The airplane was significantly damaged after the incident, including the loss of parts of its horizontal stabilizers.
  • On 4 February 2015, TransAsia Flight 235, operated by an ATR 72-600, crashed soon after takeoff in Taipei. Approximately one minute before the crash the pilot reported an engine flameout which had been caused by an engine failure. Combined with the mistaken shut down of the working engine this caused the aircraft to strike a viaduct and crash into a river, killing 43 out of the 58 people on board.

Other examples[edit]


  1. ^ "''Turbo Jet Flame Out'' by Ask a Scientist". Newton.dep.anl.gov. Retrieved 2012-03-25. 
  2. ^ "''Flameout - Why the fire in a perfectly healthy jet engine can die.'' by Peter Garrison, Air & Space Magazine, September 01, 2006". Airspacemag.com. Retrieved 2012-03-25. 
  3. ^ "''Airplane Turbofan Engine Operation and Malfunctions'', FAA Manual". Webcache.googleusercontent.com. Retrieved 2012-03-25. 
  4. ^ [1]
  5. ^ Flightglobal archive flight International 10 July 1982 p59
  6. ^ "Gas Turbine Performance" 2nd edition P.P.Walsh P. Fletcher ISBN 0-632-06434-X p484
  7. ^ "AAIB Bulletin 12/2015" (PDF). Air Accidents Investigation Branch, Department for Transport. Retrieved 10/12/2015.  Check date values in: |access-date= (help)
  8. ^ [2]