1. Brunei
  2. Aircraft
  3. S-70A-14 Blackhawk

Basic Information

Category Helicopter Type Transport
Year Commissioned 1986 Year Decommissioned 0
Agility 1 Damage Points (DP) 5
Empty Weight 4819 kg Max Weight 11113 kg
Runway Information 0m (VTOL) TOD/LAD Physical Size Medium Aircraft (12.1-18m)
Cost 0 Hypothetical No
Payload Weight 0 kg Crew 4 people

Aircraft Capabilities

Nap-of-the-Earth (NOE) Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles)

Sensor Parameters

Model Purpose Range Scan Interval Generation
AN/APN-217 Radar, Navigation 0.20 - 35.00 nm 2 sec Early 1980s

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
AN/APN-217 SB1, SB2, SMF1, PB1, PB2, PMF2 否

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius
Trooper   x 14
230 USG Drop Tank   x 2

Signatures

Type Front Side Rear
Visual Detection Range 1.87 nm 5.8 nm 1.87 nm
Visual Classification Range 1.11 nm 3.31 nm 1.71 nm
Infrared Detection Range 1.87 nm 7.63 nm 10.94 nm
Infrared Classification Range 1.11 nm 3.31 nm 1.11 nm
Radar, A-D Band (30-2000 MHz) 1 dBsm (1.26 m²) 3.5 dBsm (2.24 m²) 1 dBsm (1.26 m²)
Radar, E-M Band (2-100 GHz) 1 dBsm (1.26 m²) 3.5 dBsm (2.24 m²) 1 dBsm (1.26 m²)

Default Configuration

Model Comments
7.62mm MG [400 rnds] Helicopter
7.62mm MG [400 rnds] Helicopter

Datalink

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

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
2x T700-GE-701C Helo Turboshaft 2 1890 - 0.462 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 1095