Specifications |
DIMENSIONS: | Span: 38.13 feet (11.6 meters)
Length: 38.70 feet (11.8 meters)
Height: 14.80 feet (4.5 meters) |
WEIGHT: | Empty: 8,115 pounds (3,681 kilograms)
Take-off gross weight: 13,179 pounds (5,978 kilograms) |
MAXIMUM SPEED AT SEA LEVEL: | 465 knots (862 kilometers/hour) |
SERVICE CEILING: | 45,200 feet (13,777 meters) |
CREW: | Instructor pilot, student pilot |
FUEL: | Fuselage tank: 387 gallons (1,465 liters)
Wing tip tanks: 102 gallons (386 liters) each tank
Wing leading edge: 50 gallons (189 liters) each wing |
RANGE: | 930 nmi (1,723 kilometers) (10% reserve) |
EQUIPMENT: | - LS-1A Election Seats Speed Brakes
- Duplicate controls and instruments in each cockpit
- Variety of communications and navigation systems
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POWER PLANTS: | Two J85-GE-4 engines; each rated at 2,950 pounds (1,338 kilograms) maximum thrust (standard day at sea level) |
ARMAMENT: | - Two 320-pound (145 kilograms) capacity underwing store stations
- 50-caliber gun package
- Bomb racks
- Rocket packs
- Tow target containers
- Fire control package (baggage compartment)
- An armament accessory kit was available that provided six store stations.
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LANDING GEAR: | Tricycle; hydraulic retracted; conventional air/oil shock strut |
MAINTAINABILITY: | - Workstands or ladders not required for servicing or maintenance
- Large quick-open access doors for equipment, accessories, and engines
- System components grouped together in spacious compartments
- Engines accessible and easily removed from ground level
- Battery starting
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