["Ae270 Commercial Flight-Ready", "Aviation Week & Space Technology", January 8 2007.] .]pecifications (Ae 270)
aircraft specifications
plane or copter?= plane
jet or prop?= prop
ref= [http://www.ae270.com/Collateral/specifications.html Ae270 Propjet Specifications]
crew= One or two
capacity= Up to 10 passengers, but typically 6.
length main= 12.23 m
length alt= 40 ft 1 in
span main= 13.82 m
span alt= 45 ft 4 in
height main= 4.78 m
height alt= 15 ft 8 in
area main= 21 m²
area alt= 226 ft²
airfoil=NASA MS(1)-0316.7 (root), NASA MS(1)-0312 (tip) [ [http://www.ae.uiuc.edu/m-selig/ads/aircraft.html The Incomplete Guide to Airfoil Usage] ]
empty weight main= 2,564 kg
empty weight alt= 5,653 lb
useful load main= 1,136 kg
useful load alt= 2,504 lb
max takeoff weight main= 4,000 kg
max takeoff weight alt= 8,818 lb
more general=
* Maximum landing weight: 3,800 kg (8,377 lb)
engine (prop)=Pratt & Whitney Canada PT6A-66A-42A
type of prop=turboprop engine
number of props=1
power main= 634 kW
power alt= 850 shp
power original=
max speed main= 500 km/h
max speed alt= 270 knots, 311 mph
max speed more= at 7,600 m (25,000 ft)
cruise speed main=
cruise speed alt=
never exceed speed main=
never exceed speed alt=
stall speed main= 162 km/h
stall speed alt= 87.7 KEAS, 100 mph
stall speed more= with flaps up
range main= 2,859 km
range alt= 1,544 nm, 1,777 mi
range more= at 30,000 ft with 30-minute VFR reserve
ceiling main= 9,144 m
ceiling alt= 30,000 ft
climb rate main= 8.0 m/s
climb rate alt= 1.581 ft/m
loading main= 190 kg/m²
loading alt= 38.9 lb/ft²
power/mass main=
power/mass alt=
avionics=
References
External links
* [http://www.ae270.com/ www.ae270.com] – Official website
* [http://www.flugzeuginfo.net/acdata_php/acdata_ae270_en.php Specs & Photo at Flugzeuginfo.net]
ee also
aircontent
related=
similar aircraft=
* Myasichtchev 101
* Pilatus PC-12
* Piper Meridian
* Socata TBM 700
lists=
* List of civil aircraft
see also=