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747SP ✕ Douglas 1211-J ✕
Manufacturer Boeing Douglas Aircraft Corporation
Description The Boeing 747SP (for Special Performance) is a shortened version of the Boeing 747 wide-body airliner, designed for a longer range. The Douglas 1211-J was a bomber aircraft design developed by American aircraft manufacturer Douglas to compete with the Boeing B-52 design for a major United States Air Force contract between 1946 and 1954.
ICAO Code B74S
EASA TCDSN EASA.IM.A.196
First Flight 1975-07-04
Entry Into service 1976-04-25
Production End 1982-01-01
Designer Douglas Aircraft Corporation
Type Wide-body jet airliner
Length (m) 55.85 48.768
Height (m) 20.06 13.4112
Cockpit Crew 3 9
Max Seating 331
Max Speed (km/h) 833.3993
Max Ceiling (m) 13746.48 15240
Rate of Climb (m/s) 2.54
Armament 2x 20 mm cannon; 2x 2000 lb bombs; 2x TV-guided bombs
Capacity Description 331 or 343 passengers (three-class), 3,900 cu ft (110 m3) of cargo, 83,730 lb (37,970 kg) total payload
Max Mach (Mach) 0.92
National Origin United States of America
Number Built 45
Powerplant Description 4 × Pratt & Whitney JT9D-7J high bypass turbofan
Primary Users Pan Am (historical), United Airlines (historical), South African Airways (historical), Iran Air (historical) United States Air Force
Status Two in service with Pratt & Whitney Canada Design only
Wikipedia Article (URL) en.wikipedia.org/wiki/Boeing_747SP en.wikipedia.org/wiki/Douglas_1211-J
Flat Wing Span (m) 59.64 69.1896
Wake Category H
Aircraft Engine Pratt & Whitney JT9D
Number of Engines 4 4