COMMERCIAL AVIATION
Used in roles serving the commercial aviation market, ferrying both passengers and goods over range.
73.0 ft
(22.25 meters)
Length
84.9 ft
(25.89 meters)
Width/Span
24.6 ft
(7.50 meters)
Height
23,126 lb
(10,490 kilograms)
Empty Weight
36,376 lb
(16,500 kilograms)
Maximum Take-Off Weight
+13,250 lb
(+6,010 kg)
Weight Difference
monoplane / high-mounted / straight
Mainplane Arrangement
Monoplane
Design utilizes a single primary wing mainplane; this represents the most popular modern mainplane arrangement.
High-Mounted
Mainplanes are mounted at the upper-most position allowable along the dorsal line of the fuselage.
Straight
The planform involves use of basic, straight mainplane members.
2 x Pratt & Whitney PW120A/PW121 turboprop engines developing 2,000 horsepower each driving six-bladed propeller units.
Propulsion
317 mph
(510 kph | 275 knots)
Max Speed
25,000 ft
(7,620 m | 5 miles)
Ceiling
1,181 miles
(1,900 km | 1,026 nm)
Range
MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030