Tbm 900 For Sale4/25/2021
The aircraft has a maximum operating altitude of 31,000, a normal cruise speed of 318 KTS366 MPH, and a 1,274 NM1,468 SM seats-full range.The SOCATA TBM 900 has a 3,000 balanced field length and 3,500 landing distance.It has a total baggage capacity of 33.00 ft3; 24.00 ft3 being internal and 09.00 ft3 being external.
Based on 450 annual owner-operated hours and 4.25-per-gallon fuel cost, the SOCATA TBM 900 has total variable costs of 355,387.50, total fixed costs of 143,464.00, and an annual budget of 498,851.50. This breaks down to 1,108.56 per hour. The cabin measures 10.0 feet long by 4.0 feet wide by 4.1 feet tall giving it a total cabin volume of 163.3 cubic feet making it comfortable for up to 5 passengers. The baggage compartment can hold up to 0.0 bags assuming your average piece of luggage is less than 5 cubic feet. The EADS Socata TBM 900 has a maximum range (not including headwinds, high altitude, hot temperatures, or higher capacity) of 1,597 miles and a maximum speed of 345 mph. Common names and abbreviations: TBM-900, Socata TBM 900, EADS Socata TBM 900, TBM-900. Internal baggage capacity is the amount of available baggage which can be stowed inside the aircraft where there will be pressurization and temperature control. External baggage capacity is the amount of baggage space accessed from outside the aircraft and may not have pressurization or temperature control. Tbm 900 For Sale Plus 2 CubicTotal number of bags is the total number of bags, using an average 5 cubic feet per bags plus 2 cubic feet of space between bags (unusable space) that you could expect to fit in the aircraft. Seats full range is the maximum range the jet will fly at long range cruise speed at optimal altitude with the maximum payload. The higher the altitude, the thinner the air which allows the jet to fly faster and more efficiently since the thinner air produces less friction. Balanced field length is effected by many factors such as altitude, temperature, humidity and the condition of the runway which is effected by rain and snow. This calculation is performed by the pilot in command prior to every flight to ensure an adequate margin of safety in the event a take-off has to be aborted. Landing distance is the amount of runway required to land the aircraft at an average weight and air density and will vary greatly for each mission. Operational weight It is the basic weight of the aircraft including the the crew, all fluids necessary for operation such as engine oil, engine coolant, water, unusable fuel and all operator items and equipment required for flight but excluding usable fuel and the payload. Maximum take off weight is the maximum total weight of the aircraft fully packed with passengers, crew, baggage and fuel able to take off. Maximum landing weight is the maximum weight of the aircraft can be at landing.
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