* Specifications *

Manufacturer: Grumman Aircraft Corporation

Power plant: Two Pratt & Whitney J52-P408 turbofan engines

Thrust: 11,200 pounds (4,767 kilograms) per engine

Length: 59 feet (17.98 meters)

Height: 15 feet (4.57 meters)

Wing span: 53 feet (16.15 meters)

Speed: Maximum .99 mach; cruise .72 mach

Ceiling: 40,000 feet - maximum (12,186 meters)
37,600 feet - Service ceiling

Performance 2,750 ft - Minimum take-off distance
2,185 ft - Minimum landing distance
Weight: 33,600 lbs - Empty
61,500 lbs - Maximum TOGW (27,921 kilograms)
15,422 lbs - Internal fuel
10,000 lbs - External fuel
4,000 lbs - External fuel (typical)

Range: Unrefueled in combat configuration: 850 nautical miles (977.5 miles)
Ferry range (5 drop tanks) 1,747 nm
Refueled: unlimited (crew fatigue factor - approximately 8 hours)

Armament: ALQ-99 Tactical Jamming System (TJS);
High Speed Anti-Radiation Missile (HARM)

Sensors: ALQ-99 On-board System (OBS)

Crew: 4

Introduction date: ICAP configuration, 1977; current ICAP II configuration, 1984

Unit Replacement Cost: $52,000,000

Inventory: 100 PAA
120 total