 - ENGINE AND FUEL
- F404 GE 100 18,000 Pound Thrust Turbofan Engine
- Pneumatic/Cartridge Starter or Optional Jet Fuel Starter
- 5,050 Pound Internal Fuel Capacity
- 330 Gallon Pylon Tank Capability--Three Stations
- Provisions for Air Refueling
- Halon Fuel lnerting System
- AVIONICS
- Digital Avionics with Built in Test (BIT)
- MIL STD 1553B Multiplexed Stores Management
- MIL STD 1750A Mission Computer
- Head Up Display (HUD)
- Hands on Stick and Throttle Controls
- ASN-144 Ring Laser Gyro Inertial Navigation Set
- AN/APG-67(V) Multimode Coherent Radar
- APX-101 Identification Friend or Foe (IFF)
- ARC-182 VHF/UHF Radio
- Radar Warning Receiver (RWR)
- ALE-40 Flush Mounted Countermeasures Dispenser System
- ARN-118 TACAN
- AIRFRAME
- 9G 8,000 Hour Airframe
- Dual Digital Flight Control System with 3 Axis Control Augmentation, plus Full Time Mechanical Backup System
- Autopilot
- Automatic High Rate Continuous Maneuvering Flap System
- Zero Altitude/Airspeed Ejection Seat
- Antiskid Carbon Brakes
- Onboard Oxygen Generating System (OBOGS)
- Graphite Composite Tail Skins
- Reduced Detectability, Increased Survivability
Back to the F-20A Tigershark Home Page
© Mark Wade, 1997 - 2006 except where otherwise noted.
Please contact us with any corrections, additions, or comments.
|
|
|
