Mirage

The New Piper Aircraft, Inc.

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

Сайт разработчика: www.newpiper.com