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Embraer EMB-314 Super Tucano (A-29) vs Sukhoi Su-25 Grach (Frogfoot) Comparison


Aviation | Utilities | Side-by-Side Comparison

Direct side-by-side comparison of two aircraft.

Your selected aircraft are compared in side-by-side arrangement below. You can always go back and Compare any two aircraft in our database. Some entries contain '0', 'not available', or an 'NA' value. This is more common with conceptual, experimental, and x-plane designs. Rotary-wing system (i.e. helicopters) values include main rotor diameter as part of width/wingspan measurement. UAV entries may display crew values as '0', not taking into account ground-based controllers.
Subjects
Embraer EMB-314 Super Tucano
Trainer / Counter-Insurgency / Light Attack / Armed Reconnaissance Aircraft
Sukhoi Su-25TM (Frogfoot)
Close-Air Support (CAS) / Ground Attack Aircraft
Basics
ORIGIN
Brazil
ORIGIN
Soviet Union
YEAR
2003 [Diff.+22 yrs]
YEAR
1981 [Diff.-22 yrs]
CREW
2
CREW
1
PRODUCTION
205 units [Diff.-819]
PRODUCTION
1,024 units [Diff.+819]
Dimensions
LENGTH
37.2 ft (11.3 m) [Diff.-13.1 ft]
LENGTH
50.3 ft (15.3 m) [Diff.+13.1 ft]
WIDTH/SPAN
36.5 ft (11.1 m) [Diff.-10.6 ft]
WIDTH/SPAN
47.1 ft (14.4 m) [Diff.+10.6 ft]
HEIGHT
13.0 ft (4.0 m) [Diff.-2.7 ft]
HEIGHT
15.7 ft (4.8 m) [Diff.+2.7 ft]
Relative Size Comparison
Shapes below depict aircraft from wingtip-to-wingtip / nose-to-tail assuming aircraft are being viewed from overhead perspective (the nose pointing towards the top of the screen). Helicopter widths include main rotor diameter. If any dimensional values are "NA" in the database then the presented shapes may appear skewed.
Compare aircraft size graphic
Embraer EMB-314 Super Tucano
Compare aircraft size graphic
Sukhoi Su-25TM (Frogfoot)
Weights
EMPTY WT.
6,658 lb (3,020 kg) [Diff.-17,020 lb]
EMPTY WT.
23,678 lb (10,740 kg) [Diff.+17,020 lb]
M.T.O.W.
11,464 lb (5,200 kg) [Diff.-33,731 lb]
M.T.O.W.
45,195 lb (20,500 kg) [Diff.+33,731 lb]
Installed Power
1 x Pratt & Whitney Canada PT6A-68C turboprop engine developing 1,600 horsepower and driving a five-bladed propeller unit at the nose.
2 x Soyuz / Tumansky R-195 turbojet engines developing 9,480 pounds of thrust each.
Performance
SPEED
367 mph (590 kph) [Diff.-224 mph]
SPEED
590 mph (950 kph) [Diff.+224 mph]
RANGE
1,774 miles (2,855 km) [Diff.+221 miles]
RANGE
1,553 miles (2,500 km) [Diff.-221 miles]
CEILING
35,007 ft (10,670 m) [Diff.+12,041 feet]
CEILING
22,966 ft (7,000 m) [Diff.-12,041 feet]
RATE-OF-CLIMB
3,242 ft/min [Diff.-8,158 feet]
RATE-OF-CLIMB
11,400 ft/min [Diff.+8,158 feet]
Armament
STANDARD:
1 x 20mm cannon in under-fuselage pod.
2 x 12.7mm FN Herstal M3P Heavy Machine Guns (HMGs).

AIR-TO-AIR ORDNANCE:
2 x AIM-9 "Sidewinder" short-range air-to-air missiles.
2 x MAA-1 "Piranha" air-to-air missiles.
2 x "Python" Mark 3/ Mark 4 air-to-air missiles.

AIR-TO-GROUND ORDNANCE:
4 x 70mm rocket launcher pods.
Conventional Drop Bombs.
Precision-Guided / Laser-Guided Bombs.

Also gun pods, cannon pods, and jettisonable fuel tanks.
STANDARD:
1 x 30mm GSh-30-2 / AO-17A internal cannon.

OPTIONAL:
Up to 9,700 lb of external ordnance including rocket pods, guided munitions, conventional dumb bombs, laser-guided air-to-surface missiles/bombs, cluster bombs and air-to-air missiles. Also jettisonable fuel tanks as needed.
Going Further
View Entry
(Embraer EMB-314 Super Tucano (A-29))
View Entry
(Sukhoi Su-25 Grach (Frogfoot))
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