Commercial Aircraft Corporation of China Ltd (COMAC) - China
Manufacturer(s)
China; United States (GE Capital Aviation)
Operators
2023
Service Year
China
National Origin
Active
Project Status
2
Crew
10
Units
COMMERCIAL AVIATION
Used in roles serving the commercial aviation market, ferrying both passengers and goods over range.
127.6 ft
(38.90 meters)
Length
117.5 ft
(35.80 meters)
Width/Span
39.2 ft
(11.95 meters)
Height
170,417 lb
(77,300 kilograms)
Maximum Take-Off Weight
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 CFM International LEAP-1C non-afterburning turbofan engines developing 25,000-to-30,000lb of thrust each.
Propulsion
559 mph
(900 kph | 486 knots)
Max Speed
364 mph
(585 kph | 316 knots)
Cruise Speed
+196 mph
(+315 kph | 170 knots)
Speed Difference
39,698 ft
(12,100 m | 8 miles)
Ceiling
2,485 mi
(4,000 km | 2,160 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 (559mph).
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).
>>>>