Overview
The Douglas B-66 Destroyer was developed in the 1950s as a tactical bomber and reconnaissance aircraft for the U.S. Air Force. Derived from the Navy’s A-3 Skywarrior, it was adapted for land-based operations. The aircraft served extensively during the Cold War, particularly in Southeast Asia.
Live Fleet Activity (B66)
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Specifications
Units
- Engine
- 2 × Allison J71-A-11
- Engine type
- Jet
- Thrust
- 2 × 10,200 lbf · 45 kN
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 3
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- 75 ft 2 in · 22.90 m
- Tail height
- 23 ft 7 in · 7.19 m
- Fuselage diameter
- 6 ft 7 in · 2.00 m
- Wing span
- 72 ft 6 in · 22.10 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 83,000 lb · 37,700 kg
- Max landing weight
- 56,000 lb · 25,500 kg
- Max payload
- 15,400 lb · 7,000 kg
- Fuel capacity
- 4,650 gal · 17,600 L · 14,100 kg (Jet A)
- Max cruise speed
- 550 kt · 633 mph · 1,019 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- 116 kt · 133 mph · 215 km/h
- Range
- 1,564 nm · 1,800 mi · 2,900 km
- Fuel burn
- —
- Ceiling
- 43,000 ft · 13,100 m
- Rate of climb
- 5,000 ft/min · 25 m/s
- Takeoff distance
- —
- Landing distance
- —
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Live fleet activity details
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