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Concorde's pressurisation was set to an altitude at the lower end of this range, 6,000 feet (1,800 m). [129] Concorde's maximum cruising altitude was 60,000 feet (18,000 m); subsonic airliners typically cruise below 44,000 feet (13,000 m). [130] A sudden reduction in cabin pressure is hazardous to all passengers and crew. [131]
The additional weight of the extra fuel in tank 11, the rearmost tank, plus the additional luggage shifted the aircraft's centre of gravity rearwards, to beyond the safe operating limit of 54 per cent, set by the Concorde test pilots. Once the damaged forward tank 5 began to lose fuel, the centre of gravity moved even further rearward.
This is often important when traveling with hand baggage only as some airlines have very restrictive weight limits, even in business or first class with limits as low as 10kg.
Type MTOW [kg] MLW [tonnes] TOR [m] LR [m] ICAO category FAA category; Antonov An-225: 640,000: 591.7: 3,500: Super: Super Scaled Composites Model 351 Stratolaunch
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The Rolls-Royce/Snecma Olympus 593 was an Anglo-French turbojet with reheat, which powered the supersonic airliner Concorde.It was initially a joint project between Bristol Siddeley Engines Limited (BSEL) and Snecma, derived from the Bristol Siddeley Olympus 22R engine.