Credit
OTOMATICC · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
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At a glance
Measured figures
Atlantique 2 · Length
Single source31.62 m (103 ft 9 in)[source]
SR20-G3 · Length
Configuration
| Specification | Bréguet 1150 Atlantic | Cirrus SR20 |
|---|---|---|
| Type | Maritime patrol aircraft[source] | Light aircraft[source] |
| Manufacturer | Breguet Aviation[source] | Cirrus Aircraft[source] |
| Status | Active service[source] | — |
| Primary users | French Navy German Navy Italian Air Force Royal Netherlands Navy[source] | — |
| Number built |
26 ft 0 in (7.92 m)[source]
Empty; Atlantique 2 · Empty weight
Single sourceGross; Atlantique 2 · Gross weight
Single sourceMaximum take-off; Atlantique 2 · Max takeoff weight
Single source25,700 kg (56,659 lb)[source]
45,000 kg (99,208 lb)[source]
46,200 kg (101,854 lb)[source]
Empty; SR20-G3 · Empty weight
Single sourceGross; SR20-G3 · Gross weight
Single sourceAtlantique 2 · 2 × Rolls-Royce Tyne RTy.20 Mk 21 2-spool turboprop engines (6,100 shp) each (equivalent)
Single source2 × Rolls-Royce Tyne RTy.20 Mk 21 2-spool turboprop engines, 4,500 kW (6,100 shp) each (equivalent)[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]
Atlantique 2 · Wing area
Single source120.34 m 2 (1,295.3 sq ft)[source]
Atlantique 2 · Endurance
Single source18 hours[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
87 Atlantique 1 28 Atlantique 2[source]
2,084 (through 2025)[source] |
| Manufactured | 1961–1987[source] | 1999–present[source] |
|---|
| Introduction date | 1965[source] | — |
|---|
| First flight | 21 October 1961[source] | 21 March 1995[source] |
|---|
| Capacity | 12 passengers or relief crew[source] | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
|---|
| Stall speed | 167 km/h (104 mph, 90 kn) flaps down[source] | 56 kn (64 mph, 104 km/h) CAS[source] |
|---|
| Developed into | — | Cirrus SR22[source] |
|---|
| Propellers | — | 3-bladed[source] |
|---|
| National origin | — | United States[source] |
|---|