1. Sri Lanka
  2. Aircraft
  3. IA-58A Pucara

Basic Information

Category Fixed Wing Type Attack
Year Commissioned 1992 Year Decommissioned 1997
Agility 1.5 Damage Points (DP) 5
Empty Weight 4020 kg Max Weight 6800 kg
Runway Information 250-450m (STOL) TOD/LAD Physical Size Medium Aircraft (12.1-18m)
Cost 0 Hypothetical No
Payload Weight 1500 kg Crew 2 people

Aircraft Capabilities

Bombsight - Ballistic Computing

Sensor Parameters

Model Purpose Range Scan Interval Generation

Sensor Coverage Diagram
Model Detection Angle Omnidirectional

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius
125kg GPB   x 12
125kg GPB   x 6
HYDRA 70mm Rocket   x 38
125kg GPB   x 6
HYDRA 70mm Rocket   x 38
125kg GPB   x 12

Signatures

Type Front Side Rear
Visual Detection Range 2.9 nm 5.62 nm 2.9 nm
Visual Classification Range 1.6 nm 3.22 nm 2.66 nm
Infrared Detection Range 2.9 nm 7.47 nm 12.97 nm
Infrared Classification Range 1.6 nm 3.22 nm 1.6 nm
Radar, A-D Band (30-2000 MHz) 6.3 dBsm (4.27 m²) 8.6 dBsm (7.24 m²) 6.3 dBsm (4.27 m²)
Radar, E-M Band (2-100 GHz) 6.3 dBsm (4.27 m²) 8.6 dBsm (7.24 m²) 6.3 dBsm (4.27 m²)

Default Configuration

Model Comments
20mm Hispano HS.804 x 2 [280 rnds x 2] Aircraft, AI-58 Pucara
7.62mm MG x 4 [750 rnds x 4] Aircraft, IA-58 Pucara

Datalink

Type Model Range Channels
Radio UHF/VHF Radio [Unsecure] 100 nm 0

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
2x Astazou XVIG Turboprop 2 978 - 0.5 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 1040