AT-802U Dimensional Drawings
AT-802U Specifications
| Engine Type | Pratt & Whitney PT6A-67F |
|---|---|
| Engine takeoff SHP –uninstalled | 1,600 @ 40.3° C, 1,700 rpm |
| Engine maximum continuous shaft horsepower –uninstalled | 1,600 @ 27.5° C, 1,700 rpm |
| Propeller | 118 in (300 cm) diameter, aluminum Hartzell |
| Propeller ground clearance | 39 in (0.99 m) |
| Gross weight –landing & takeoff | 16,000 lbs (7,257 kg) |
| Empty weight, with armor, no weapons | 7,836 lbs (3,703 kg) |
| Useful load with ballistic armor | 8,164 lbs (4,000 kg) |
| Fuel capacity – wings | 380 US gal (1,438 L) |
| Auxiliary fuel capacity – fuselage | 360 US gal (1,363 L) |
| Wingspan | 59.2 ft (18.04 m) |
| Wing area | 401 ft2 (37.25 m2) |
AT-802U Performance
| Maximum speed, no weapons, at 10,000 ft. (3048 m) | 213 knots (394 kph) |
|---|---|
| Patrolling speed – 10,000 ft.; 71 US gal per hour (3,048 m; 268 L per hour) | 180 knots (333 kph) |
| Stall speed – flaps down, at max gross weight | 91 knots (169 kph) |
| Stall speed, at 12,500 lbs. (5,670 kg) | 70 knots (130 kph) |
| Range with auxiliary fuselage fuel, economy cruise at 8,000 ft (2,438 m) | 1,303 nm (2,414 km) |
| Landing run | 1200 ft (366 m) |
| Gross Weight | Takeoff Roll | Rate of Climb |
|---|---|---|
| Full fuel load, 10,000 lbs (4,500 kg) | 680 ft (207 m) | 3,000 fpm (914 mpm) |
| Surveillance Load, 12,500 lbs (5,700 kg) | 1,100 ft (335 m) | 2,200 fm (670 mpm) |
| Surveillance & weapons load, 14,500 lbs (6,600 kg) | 1,400 ft (426 m) | 1,700 fpm (518 mpm) |
AT-802U Standard Features
- Wing and Center Line Structural External Stores Locations
- 8 wing hard points to carry 500 lb. class weapons
- 2 centerline hard points to carry 1,000 lb. class weapons
- Innermost wing station optimized for guns (.50 cal to 20mm)
- Pratt & Whitney PT6A-67F Turboprop Engine
- Titanium Dome 5-Blade Propeller
- Tandem Seat Cockpit with Dual Flight Controls, Power and Instruments
- 380 Gallon Wing Fuel Tanks
- 360 Gallon Fuselage Fuel Tank, with Fuel Jettison
- Self-Sealing Fuel System (Wing Tanks, Fuselage Tanks and Fuel Hoses)
- Fuel Tank Shutoff Control System
- Cockpit and Engine Armor (Panels, Glass, Split Doors and Footwell enclosure)
- Vertical Speed Indicator (Front Cockpit)
- Lightning Protection
- AmSafe Inflatable Restraints, (Front and Rear Cockpit)
- Minimum VFR Flight Instruments
- ESC Electrical Bus
- Forward Mission Equipment Bay
- NVG Compatible Cockpit Lighting
- Emergency Locator Transmitter (ELT)
- Two-Place Diluter Extended Demand Oxygen System
- Avionics (Air Speed Indicator, Turn Coordinator, Altimeter, Altitude Indicator, Clock)