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BSupport aircraft
Airborne early warning and control (AEW&C) (E-99) Remote sensing (R-99) Maritime patrol (P-99)
Measured figures
L-59E · Length
Single source12.20 m (40 ft 0 in)[source]
Configuration
| Specification | Aero L-59 Super Albatros | Embraer R-99 |
|---|---|---|
| Type | Military trainer aircraft COIN[source] | Airborne early warning and control (AEW&C) (E-99) Remote sensing (R-99) Maritime patrol (P-99)[source] |
| Manufacturer | Aero Vodochody[source] | Embraer[source] |
| Status | Out of production, in service[source] | Active in service[source] |
| Primary users | Czech Air Force Egyptian Air Force Tunisian Air Force[source] |
L-59E · including tip tanks
Single source9.54 m (31 ft 4 in) (including tip tanks)[source]
L-59E · Height
Single source4.77 m (15 ft 8 in)[source]
Maximum; L-59E · at 5,000 m (16,000 ft)
Single source865 km/h (537 mph, 467 kn) at 5,000 m (16,000 ft)[source]
L-59E · at 7,000 m (23,000 ft) (with maximum internal and external fuel)
Single source2,000 km (1,200 mi, 1,100 nmi) at 7,000 m (23,000 ft) (with maximum internal and external fuel)[source]
L-59E · 1 × Lotarev DV-2 turbofan thrust
Single source1 × Lotarev DV-2 turbofan , 21.57 kN (4,850 lbf) thrust[source]
L-59E · Wing area
Single source18.80 m 2 (202.4 sq ft)[source]
L-59E · Service ceiling
Single source11,800 m (38,700 ft)[source]
L-59E · 5,510 ft/min
Single source28.0 m/s (5,510 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Brazilian Air Force (E-99M/R-99) Hellenic Air Force (R-99A) Mexican Air Force (R-99A/P-99) Indian Air Force ( Netra AEW&C )[source] |
| Number built | 80[source] | 6 (EMB-145-SA) 3 (EMB-145-RS) 2 (EMB-145-MP) 4 (EMB-145-H) 3 (EMB-145-I)[source] |
|---|
| Manufactured | 1986–1996[source] | 1999–present[source] |
|---|
| First flight | 30 September 1986[source] | 1999[source] |
|---|
| Developed from | Aero L-39 Albatros[source] | Embraer ERJ-145[source] |
|---|
| Variant | Aero L-159 ALCA[source] | — |
|---|
| Fuel capacity | 1,537 L (406 US gal; 338 imp gal) including tip tanks[source] | — |
|---|
| Stall speed | 185 km/h (115 mph, 100 kn) (flaps down)[source] | — |
|---|
| Guns | one GSh-23L cannon in under-fuselage pod[source] | — |
|---|
| Hardpoints | four underwing hardpoints with a capacity of inner hardpoints 500 kg (1,100 lb)capacity, outer hardpoints 250 kg (550 lb)[source] | — |
|---|
| Country of origin | Czechoslovakia[source]Inventory Origin column; table 1, row 26, cell 2; revision 1374778711; retrieved 2026-10-01 | — |
|---|
| National origin | — | Brazil[source] |
|---|
| Introduction date | — | 2001[source] |
|---|