(Showcased structural values pertain to the Boeing KC-767A production variant)
monoplane / low-mounted / swept-back
Design utilizes a single primary wing mainplane; this represent the most popular mainplane arrangement.
Mainplanes are low-mounted along the sides of the fuselage.
The planform features wing sweep back along the leading edges of the mainplane, promoting higher operating speeds.
(Structural descriptors pertains to the Boeing KC-767A production variant)
2 x General Electric GE CF6-80C2 non-afterburning turbofan engines developing 60,200 lb of thrust each.
(915 kph | 494 kts)
(12,200 m | 8 mi)
(12,200 km | 22,594 nm)
♦ MACH Regime (Sonic)
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 (569mph).
Graph average of 563 miles-per-hour.
Boeing KC-767A operational range when compared to distances between major cities (in KM).
Max Altitude Visualization
The 3 qualities we look at for a balanced aircraft design are altitude, speed, and range.
Showcasing era cross-over of this aircraft design.
This entry's total production compared against the most-produced military and civilian aircraft types in history (Ilyushin IL-2 and Cessna 172, respectively).
Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.