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At a glance
Measured figures
SR20-G3 · Length
Single source26 ft 0 in (7.92 m)[source]
T3J-1/T-39D · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | North American Sabreliner |
|---|---|---|
| Type | Light aircraft[source] | Trainer aircraft Business jet[source] |
| Manufacturer | Cirrus Aircraft[source] | North American Aviation Rockwell International[source] |
| Number built | 2,084 (through 2025)[source] | 800+[source] |
| Manufactured | 1999–present[source] | 1959 – 1982 |
44 ft 0 in (13.41 m)[source]
T3J-1/T-39D · Range
Single source2,170 nmi (2,500 mi, 4,020 km)[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]
T3J-1/T-39D · 2 × Pratt & Whitney J60-P-3 turbojet thrust each
Single source2 × Pratt & Whitney J60-P-3 turbojet , 3,000 lbf (13 kN) thrust each[source]
SR20-G3 · 828 ft/min (
Single source828 ft/min (4.21 m/s)[source]
T3J-1/T-39D · Wing area
Single source342.1 sq ft (31.79 m 2 )[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| First flight | 21 March 1995[source] | September 16, 1958[source] |
|---|
| Developed into | Cirrus SR22[source] | — |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | five–seven passengers[source] |
|---|
| Propellers | 3-bladed[source] | — |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | — |
|---|
| National origin | United States[source] | — |
|---|
| Status | — | In active service[source] |
|---|
| Primary users | — | United States Air Force United States Navy United States Marine Corps[source] |
|---|
| Introduction date | — | 1962[source] |
|---|
| Thrust/weight | — | 0.338[source] |
|---|
| Country of origin | — | United States[source]Inventory Origin column; table 13, row 7, cell 3; revision 1374043591; retrieved 2026-09-30 |
|---|