1. Malaysia
  2. Aircraft
  3. A-4PTM Skyhawk

Basic Information

Category Fixed Wing Type Attack
Year Commissioned 1986 Year Decommissioned 1999
Agility 3 Damage Points (DP) 5
Empty Weight 4460 kg Max Weight 10215 kg
Runway Information 901-1400m TOD/LAD Physical Size Medium Aircraft (12.1-18m)
Cost 0 Hypothetical No
Payload Weight 8318 kg Crew 1 people

Aircraft Capabilities

Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles) Bombsight - Ballistic Computing Probe Refueling

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

Signatures

Type Front Side Rear
Visual Detection Range 2.23 nm 5.11 nm 2.23 nm
Visual Classification Range 1.29 nm 2.98 nm 2.04 nm
Infrared Detection Range 2.23 nm 7.01 nm 11.71 nm
Infrared Classification Range 1.29 nm 2.98 nm 1.29 nm
Radar, A-D Band (30-2000 MHz) 3.1 dBsm (2.04 m²) 5.5 dBsm (3.55 m²) 3.1 dBsm (2.04 m²)
Radar, E-M Band (2-100 GHz) 3.1 dBsm (2.04 m²) 5.5 dBsm (3.55 m²) 3.1 dBsm (2.04 m²)

Default Configuration

Model Comments
20mm Mk12 x 2 [100 rnds x 2] Aircraft, A-4

Datalink

Type Model Range Channels
Radio UHF/VHF Radio [Unsecure] 100 nm 0
Bullpup Weapon Link AGM-12 Command Datalink 10 nm 1

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
1x J65-W-16A Turbojet 1 3495 - 0.9 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 2360