Credit
Tomás Del Coro from Las Vegas, Nevada, USA · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
SR20-G3 · Length
Single source26 ft 0 in (7.92 m)[source]
Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Qods Mohajer-6 |
|---|---|---|
| Type | Light aircraft[source] | Multirole, including ISR and air-to-ground strike[source] |
| Manufacturer | Cirrus Aircraft[source] | Qods Aviation Industry Company[source] |
| Number built | 2,084 (through 2025)[source] | Not known[source] |
| Manufactured | 1999–present[source] | February 2018 |
7.5 m (24 ft 7 in)[source]
SR20-G3 · Height
Single source8 ft 11 in (2.72 m)[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]
1 × water-cooled 4-stroke engine ( Rotax 914 or HESA indigenous equivalent)
Single source1 × 115 hp water-cooled 4-stroke engine ( Rotax 914 or HESA indigenous equivalent)[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.
| First flight | 21 March 1995[source] | — |
|---|
| Developed into | Cirrus SR22[source] | — |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | — |
|---|
| Propellers | 3-bladed[source] | — |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | — |
|---|
| National origin | United States[source] | Iran[source] |
|---|
| Designer | — | Qods Aviation Industry Company[source] |
|---|
| Status | — | In service[source] |
|---|
| Primary user | — | Iran[source] |
|---|
| Max Takeoff Weight (MTOW) | — | 600 kg - 670 kg (1,323 Ibs - 1,477 lbs)[source] |
|---|
| Payload Capacity | — | 100 kg - 150 kg (220 Ibs - 330 lbs)[source] |
|---|
| Propeller & Fuel | — | 3-bladed propeller; standard gasoline (petrol)[source] |
|---|
| Max speed | — | 200 km/h (110 knots)[source] |
|---|
| Operational Range ( Radius of action ) | — | 2,000 km - 2400 km (1,080 nmi - 1,300 nmi)[source] |
|---|
| Direct Line-of-Sight Data Link | — | 200 km - 500 km (130 mi - 312 mi)[source] |
|---|
| Operational altitude | — | 16,000 ft - 18,000 ft (4,876 m - 5,486 m)[source] |
|---|
| Flight Endurance | — | Up to 12 hours[source] |
|---|
| Precision Munitions | — | Air-to-ground missiles , air-to-air missiles , guided rockets , and precision-guided mortar rounds.[source] |
|---|
| Payload Pods | — | Electronic Countermeasure (ECM), electronic intelligence , and radar detection/warning systems.[source] |
|---|
| Reported operators | — |
|
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