Basic Information

Category Fixed Wing Type Transport
Year Commissioned 1983 Year Decommissioned 1998
Agility 0.5 Damage Points (DP) 20
Empty Weight 66406 kg Max Weight 151320 kg
Runway Information 2001-2600m TOD/LAD Physical Size Very Large Aircraft (26.1-75m)
Cost 0 Hypothetical No
Payload Weight 0 kg Crew 5 people

Aircraft Capabilities

Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles)

Sensor Parameters

Model Purpose Range Scan Interval Generation
Generic Doppler Navigation/Weather Radar, Weather and Navigation 0.20 - 35.00 nm 2 sec Early 1970s
AN/ALQ-204 Matador IRCM 0.00 - 0.00 nm 0 sec Early 2000s

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
Generic Doppler Navigation/Weather SB1, SB2, SMF1, PB1, PB2, PMF2
AN/ALQ-204 Matador SB1, SB2, SMF1, SMF2, SMA1, SMA2, SS1, SS2, PB1, PB2, PMF1, PMF2, PMA1, PMA2, PS1, PS2

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius
Passenger   x 100

Signatures

Type Front Side Rear
Visual Detection Range 12 nm 22.12 nm 12 nm
Visual Classification Range 4.49 nm 8.64 nm 8.8 nm
Infrared Detection Range 8 nm 14.21 nm 19.25 nm
Infrared Classification Range 3.74 nm 7.2 nm 3.74 nm
Radar, A-D Band (30-2000 MHz) 18.6 dBsm (72.44 m²) 20.4 dBsm (109.65 m²) 18.6 dBsm (72.44 m²)
Radar, E-M Band (2-100 GHz) 18.6 dBsm (72.44 m²) 20.4 dBsm (109.65 m²) 18.6 dBsm (72.44 m²)

Default Configuration

Model Comments

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
4x JT3D-3 Turbojet 4 8172 - 0.535 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 72460