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is the density altitude at which flying in a clean configuration, at the best rate of climb airspeed for that altitude with one engine producing maximum continuous power and the other engine shut down (and if it has a propeller, the propeller is feathered), will produce a given rate of climb, usually
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which can be sustained: although the true airspeed at an altitude is typically greater than indicated airspeed (IAS), the difference is not enough to compensate for the fact that IAS at which minimum drag is achieved is usually low, so a flight at an absolute ceiling altitude results in a low TAS as
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for that altitude and with all engines operating and producing maximum continuous power, will produce a given rate of climb. A typical value might be 100 ft/min (0.51 m/s) climb, or on the order of 500 ft/min (2.5 m/s) climb for jet aircraft.
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or other devices temporarily increasing thrust. Another factor that makes it impossible for some aircraft to reach their absolute ceiling, even with temporary increases in thrust, is the aircraft reaching the
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However, some performance charts will define the service ceiling as the pressure altitude at which the aircraft will have the capability of climbing at 50 ft/min (0.25 m/s) with one
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well, and therefore in a high fuel burn rate per distance traveled. The absolute ceiling varies with the air temperature and, overall, the aircraft weight (usually calculated at
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Compared to service ceiling, the absolute ceiling of commercial aircraft is much higher than for standard operational purposes. In the
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is the highest altitude at which an aircraft can sustain level flight. Due to the thin air at higher altitudes, a much higher
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Service ceiling is the density altitude at which the rate of climb drops below a prescribed value.
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is the maximum altitude of an aircraft during normal operations. Specifically, it is the
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before it was retired) routinely flew at 60,000 ft (18.3 km; 11.4 mi).
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about 51,000 ft (15.5 km; 9.7 mi). Before its retirement, the
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have a service (or certified) ceiling of under 45,000 ft (13,700 m) and some
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an aircraft can reach under a set of conditions, as determined by its
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The one-engine inoperative (OEI) service ceiling of a twin-engine,
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This article is about aircraft performance. For cloud base, see
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The absolute ceiling and service ceiling diagram of an aircraft
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Pilot's
Handbook of Aeronautical Knowledge (FAA-H-8083-25A)
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186:at which flying in a
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