Mirage
The New Piper Aircraft, Inc.
![](/content/rus/mnu/422/mirage.jpg)
фотография с сайта www.newpiper.com
STANDARD EQUIPPED LIST PRICE $1,100,000 ENGINE Manufacturer Lycoming Model TI0-540-AE2A Horsepower 350 hp Number of Cylinders 6 PROPELLER Manufacturer Hartzell Number of Blades 3 Type Composite Constant Speed WEIGHTS Maximum Take-off Weight 4,340 lbs/1,969 kg Maximum Ramp Weight 4,358 lbs/1,977 kg Standard Equipped Weight 3,113 lbs/1,412 kg Standard Useful Load (a and b) 1,245 lbs/565 kg a. Standard useful load is max ramp weight minus standard equipped weight. b. Useful load is indicated for a standard equipped aircraft. DIMENSIONS Wing Span 43 ft/13.1 m Length 28.9 ft/8.8 m Height 11.3 ft/3.4 m Cabin Length 148 in/375.9 cm Instrument Panel to Rear Bulkhead Cabin Width 49.5 in/125.7 cm Cabin Height 47 in/119.4 cm Headroom (Seat to Ceiling) 38in/96.5 cm 38in/96.5 cm 37in/94.0cm WING AREA Wing Area 175 ft2/16.25 m2 FUEL AND OIL CAPACITY Usable Fuel 120 gal/454 l Oil Capacity 12 qts/11.4 l MAXIMUM SPEED TAS TAS at Mid Cruise weight 220 kts/408 km/h CRUISING SPEEDS TAS High-speed cruise power 213 kts 394km/h CRUISING RANGE TAS Long Range Cruise Power 1,345 nm/2,491 km Cruising range includes 45 minute fuel reserve at long range cruise power plus allowance for fuel used during taxi, take-off, climb at maximum climb power, cruise at optimum altitude and stated mixture plus descent STALL SPEED IAS Flaps Extended 36º 59 kias/109 km/h 60 kcas/111 kn/h SERVICE CEILING 25,000 ft+/7,620+ m 25,000 feet is the maximum approved altitude for the Mirage MAX DIFFERENTIAL PRESSURE 5.5 psid BAGGAGE Volume Forward Compartment 13 ft3/0.37 m3 Aft Compartment 20 ft3/0.57 m3 Capacity Forward Compartment 100 lbs/45.4 kg Aft Compartment 100 lbs/45.4 kg TAKE-OFF DISTANCE Ground Roll 1,087 ft/331 m Total over 50 ft Obstacle 2,090 ft/637 m Flaps 20º, Gross Weight LANDING DISTANCE Ground Roll 1,020 ft/311 m Total over 50 ft Obstacle 1,968 ft/600 m
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