Credit
US Navy · Public domain · Resized · Public domain · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
Length
Single source110 ft 4 in (33.63 m)[source]
SR20-G3 · Length
Single sourceConfiguration
| Specification | Boeing C-40 | Cirrus SR20 |
|---|---|---|
| Type | Military transport aircraft[source] | Light aircraft[source] |
| National origin | United States[source] | United States[source] |
| Manufacturer | Boeing[source] | Cirrus Aircraft[source] |
| Status | In service[source] | — |
| Primary users |
26 ft 0 in (7.92 m)[source]
C-40A
Single sourceC-40B/C
Single source3,200 nmi (3,700 mi, 5,900 km) (C-40A), 4,500–5,000 nmi (5,200–5,800 mi; 8,300–9,300 km) (C-40B/C)[source]
SR20-G3 · 1 × Continental IO-360-ES six cylinder, horizontally-opposed piston aircraft engine
Single source1 × Continental IO-360-ES six cylinder, horizontally-opposed piston aircraft engine , 200 hp (150 kW)[source]
2 × CFM International CFM56-7B turbofan engines thrust each
Single source2 × CFM International CFM56-7B turbofan engines, 27,300 lbf (121 kN) thrust each[source]
Payload
Single source40,000 lb (18,144 kg)[source]
SR20-G3 · 828 ft/min (
Single source828 ft/min (4.21 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
United States Navy United States Air Force United States Marine Corps[source]
| — |
| Number built | 28[source] | 2,084 (through 2025)[source] |
|---|
| Manufactured | 2001–2019[source] | 1999–present[source] |
|---|
| Introduction date | 21 April 2001[source] | — |
|---|
| First flight | April 2000[source] | 21 March 1995[source] |
|---|
| Developed from | Boeing 737 Next Generation[source] | — |
|---|
| Capacity | C-40A passenger configuration: 121 passengers C-40A cargo configuration: 8 pallets C-40A combination configuration: 3 pallets, 70 passengers C-40B: 26 to 32 passengers C-40C: 42 to 111 passengers Payload: 40,000 lb (18,144 kg)[source] | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
|---|
| Fuel capacity | 6,875 US gal (26,020 L; 5,725 imp gal)[source] | — |
|---|
| Airfoil | root: BAC 449/450/451; tip: BAC 442 mod[source] | — |
|---|
| Thrust/weight | 0.407[source] | — |
|---|
| Developed into | — | Cirrus SR22[source] |
|---|
| Propellers | — | 3-bladed[source] |
|---|
| Stall speed | — | 56 kn (64 mph, 104 km/h) CAS[source] |
|---|