TBM 900 IN FIGURES POWERPLANT Type: P&W Canada PT6A-66D turboprop Thermodynamic power Nominal power Usable fuel capacity 1825 hp. 850 shp. 291 US gal. 1,100 liters EXTERNAL DIMENSIONS Wingspan Height Length Wheel base Tailplane span 42.10 ft. 14.29 ft. 35.22 ft. 9.56 ft. 16.36 ft. 12.833 m. 4.355 m. 10.736 m. 2.914 m. 4.988 m. INTERNAL DIMENSIONS Maximum cabin width Maximum cabin length Maximum cabin height Maximum volume in cabin 3 ft. 11.64 in. 13 ft. 3.45 in. 4 ft. 123 cu. ft. 1.21 m. 4.05 m. 1.22 m. 3.5 cu. m. LOADING Basic empty weight Maximum ramp weight (MRW) Maximum takeoff weight Maximum zero fuel weight Maximum payload Maximum payload with full fuel: Maximum luggage in storage areas (4 seats): Maximum luggage in storage areas (6 seats): Maximum luggage volume (large net): 4,629 lb. 7,430 lb. 7,394 lb. 6,032 lb. 1,410 lb. 891 lb. 507 lb. 330 lb. 30¼ cu. ft. 2,097 kg. 3,370 kg. 3,354 kg. 2,736 kg. 639 kg. 404 kg. 230 kg. 135 kg. 0.989 cu. m. PERFORMANCE (ISA conditions, MTOW, no wind,) Maximum cruise speed at long-range settings 252 KTAS 467 km/h Maximum cruise speed at 28,000 ft. 330 KTAS 611 km/h Time-to climb to 31,000 ft. 18 min. 45 sec. Certified ceiling 31,000 ft. 9,449 m. RUNWAY DISTANCES (ISA conditions, MTOW, no wind, 50 ft. obstacle clearance) Takeoff 2,380 ft. 726 m. Landing 2,430 ft. 741 m. Maximum range with maximum fuel (ISA conditions, MTOW, no wind, one pilot, 45 min fuel reserve) @ 31,000 ft. 252 KTAS cruise speed 1,730 NM 3,304 km 290 KTAS cruise speed 1,585 NM 2,935 km 326 KTAS cruise speed 1,440 NM 2,666 km TBM 900 ADVANTAGES Improved performance • Provides excellent short-field performance • Combines light jet performance with single-engine turboprop operating costs • Achieves maximum cruise speed at easily-available cruise altitudes • Delivers excellent useful load and range • Provides rapid climb and a 31,000 ft. service ceiling, Improved efficiency • Range increased to over 1,730 naut. mi. with five adults on board • Noise level reduced • Ensures low operating costs Improved environment for pilots • Reduced workload • Enhanced ergonomics • Intuitive human machine interface • Increased ease of handling Improved comfort • Lower cabin noise • Automatic pressurization • New seat design • More capable electrical systems • Weather radar overlay offers pilots the option to avoid weather Ownership advantages • Combines a proven airframe and engine combination • Supported by customer service on all five continents • Built by DAHER-SOCATA, a major aerospace company that listens to its customers • Eases the insurance coverage for owner/pilots • Offers a straightforward step-up for pilots qualified on piston-engine aircraft S Payload range with NBAA reserve (100 naut. mi. alternate + fuel reserve) TBM 900 DIMENSIONS
© Copyright 2024 ExpyDoc