Credit
Daniel VA · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
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At a glance
Measured figures
AT-802 · Length
Single source35 ft 11 in (10.95 m)[source]
MC-130J Commando II · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Lockheed MC-130 |
|---|---|---|
| Crew | One or Two (AT-802A – single-seat)[source] | Two pilots, one Combat Systems Officer (officers), and two Loadmasters (enlisted)[source] |
| Type | Agricultural / Fire-fighting aircraft[source] | STOL Special operations military transport aircraft[source] |
| National origin | United States[source] | — |
| Manufacturer | Air Tractor[source] | Lockheed Corporation[source] |
97 ft 9 in (29.79 m)[source]
AT-802 · 1 × Pratt & Whitney PT6A -67AG turboprop , 1,350 shp (
Single source1 × Pratt & Whitney PT6A -67AG turboprop , 1,350 shp (1,010 kW)[source]
MC-130J Commando II · 4 × Rolls-Royce AE 2100D3 turboprop engines, 4,591 shp ( ) each
Single source4 × Rolls-Royce AE 2100D3 turboprop engines, 4,591 shp (3,424 kW) each[source]
AT-802 · Wing area
Single source401.0 sq ft (37.25 m 2 )[source]
AT-802 · 850 ft/min (
Single source850 ft/min (4.3 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status | Active[source] | Active[source] |
|---|
| Manufactured | 1990–present[source] | — |
|---|
| First flight | 1990[source] | MC-130J: April 2011[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | — |
|---|
| Aspect ratio | 8.8:1[source] | — |
|---|
| Airfoil | NACA 4415[source] | — |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | — |
|---|
| Primary user | — | United States Air Force[source] |
|---|
| Number built | — | MC-130E: 18 MC-130H: 24 MC-130P: 28 MC-130W: 12 MC-130J: 64[source] |
|---|
| Introduction date | — | MC-130E: 1966 MC-130P: 1986 MC-130H: 1991 MC-130W: 2006 MC-130J: 2012[source] |
|---|
| Retired | — | MC-130E: April 15, 2013 MC-130P: May 15, 2015 MC-130H: April 2, 2023[source] |
|---|
| Developed from | — | C-130 Hercules C-130J Super Hercules[source] |
|---|
| Propellers | — | 6-bladed fully feathering reversible propellers[source] |
|---|
| Country of origin | — | United States[source] United States[source] |
|---|