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]
C-130H · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Lockheed C-130 Hercules |
|---|---|---|
| Type | Light aircraft[source] | Tactical airlifter[source] |
| Manufacturer | Cirrus Aircraft[source] | Lockheed Corporation Lockheed Martin[source] |
| Number built | 2,084 (through 2025)[source] | 2,700+ (as of June 2024)[source] |
| Manufactured | 1999–present[source] | 1954–present |
97 ft 9 in (29.79 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]
C-130H · 4 × Allison T56 -A-15 turboprop engines, 4,590 shp ( ) each
Single source4 × Allison T56 -A-15 turboprop engines, 4,590 shp (3,420 kW) each[source]
C-130H · Wing area
Single source1,745 sq ft (162.1 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] | August 23, 1954 ( 1954-08-23 )[source] |
|---|
| Developed into | Cirrus SR22[source] | — |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 42,000 lb (19,000 kg) payload C-130E/H/J cargo hold: length, 40 ft (12.19 m); width, 9 ft 11 in (3.02 m); height, 9 ft (2.74 m). Rear ramp: length, 123 in (3.12 m); width, 119 in (3.02 m) C-130J-30 cargo hold: length, 55 ft (16.76 m); width, 9 ft 11 in (3.02 m); height, 9 ft (2.74 m). Rear ramp: length, 123 inches (3.12 m); width, 119 in (3.02 m) 92 passengers or 64 airborne troops or 74 litter patients with 5 medical crew or 6 pallets or 2–3 Humvees or 2 M113 armored personnel carriers 1 CAESAR self-propelled howitzer[source] |
|---|
| Propellers | 3-bladed[source] | 4-bladed Hamilton Standard 54H60 constant-speed fully feathering reversible propellers, 13 ft 6 in (4.11 m) diameter[source] |
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| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | — |
|---|
| National origin | United States[source] | United States[source] |
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| Status | — | In service[source] |
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| Primary users | — | United States Air Force United States Navy United States Coast Guard United States Marine Corps[source] |
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| Introduction date | — | December 1956[source] |
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| Variants | — | Lockheed AC-130 Lockheed DC-130 Lockheed EC-130 Lockheed EC-130H Compass Call Lockheed HC-130 Lockheed Martin KC-130 Lockheed LC-130 Lockheed MC-130 Lockheed RC-130 Lockheed WC-130 Lockheed L-100 Hercules Lockheed Martin C-130J Super Hercules[source] |
|---|
| Former operator · Afghanistan | — | Afghanistan[source] |
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| Former operator · Angola | — | Angola[source] |
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| Former operator · Belgium | — | Belgium[source] |
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| Former operator · Brazil | — | Brazil[source] |
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| Former operator · Honduras | — | Honduras[source] |
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| Former operator · Rhodesia | — | Rhodesia[source] |
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| Former operator · South Vietnam | — | South Vietnam[source] |
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| Former operator · Spain | — | Spain[source] |
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| Airfoil | — | root: NACA 64A318 ; tip: NACA 64A412[source] |
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| Takeoff distance | — | 3,586 ft (1,093 m) at 155,000 lb (70,307 kg) max gross weight;[source] |
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| Alternative designation | — | C-130 Hercules[source] |
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| Reported operators | — |
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