COMMERCIAL AVIATION
Used in roles serving the commercial aviation market, ferrying both passengers and goods over range.
123.3 ft
(37.57 meters)
Length
117.5 ft
(35.80 meters)
Width/Span
38.5 ft
(11.75 meters)
Height
93,917 lb
(42,600 kilograms)
Empty Weight
155,999 lb
(70,760 kilograms)
Maximum Take-Off Weight
+62,082 lb
(+28,160 kg)
Weight Difference
monoplane / low-mounted / swept-back
Mainplane Arrangement
Monoplane
Design utilizes a single primary wing mainplane; this represents the most popular modern mainplane arrangement.
Low-Mounted
Mainplanes are low-mounted along the sides of the fuselage.
Swept-Back
The planform features wing sweep back along the leading edges of the mainplane, promoting higher operating speeds.
2 x CFMI CFM56-5 OR IAE V2500 turbofan engines developing between 25,400 and 27,000 lb of thrust each.
Propulsion
541 mph
(870 kph | 470 knots)
Max Speed
39,370 ft
(12,000 m | 7 miles)
Ceiling
3,542 miles
(5,700 km | 3,078 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
Values are derrived from a variety of categories related to the design, overall function, and historical influence of this aircraft in aviation history.
The overall rating takes into account over 60 individual factors related to this aircraft entry.
Rating is out of a possible 100 points.
This entry's maximum listed speed (541mph).
Graph average of 563 miles-per-hour.
Operational range when compared to distances between major cities (in KM).
Max Altitude Visualization
The three qualities reflected above are altitude, speed, and range.
Showcasing era cross-over of this aircraft design.
Compared against Ilyushin IL-2 (military) and Cessna 172 (civilian).
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