Rockwell Sabreliner Civil Aircraft Model Details

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General Information of Rockwell Sabreliner

First Flight : September 16, 1958[1]

Introduction : 1962

Manufacturer : North American Aviation; Rockwell International

Number Built : 800+[2]

Primary Users : United States Air Force; United States Navy; United States Marine Corps

Produced : 1959–1982

Role : Trainer aircraft; Business jet

Status : In active service

General characteristics of Rockwell Sabreliner

Capacity : 5–7 passengers

Crew : 4–5

Empty Weight : 9,257 lb (4,199 kg)

Height : 16 ft (4.88 m)

Length : 44 ft (13.41 m)

Loaded_Weight : 16,340 lb (7,412 kg)

Max Takeoff Weight : 17,760 lb (8,056 kg)

Powerplant : 2 × Pratt & Whitney J60-P-3 turbojet, 3,000 lbf (13.3 kN) each

Wing Area : 342.1 ft² (31.79 m²)

Wingspan : 44 ft 6 in (13.56 m)

Performance of Rockwell Sabreliner

Cruise Speed : 435 knots (500 mph, 800 km/h)

Maximum Speed : 478 knots (550 mph, 885 km/h)

Range : 2,170 nm (2,500 mi, 4,020 km)

Service Ceiling : 40,000+ ft (12,200+ m)

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