Saab 2000
Saab 2000
Turboprop Airplanes
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Operational Photo
Basic Information
Name
Saab 2000
Designation
Saab 2000
Alternate Designation
—
Equipment Type
Turboprop Airplanes
Manufacturer
Saab
Date of Introduction
1994
Description
Saab 2000 is a twin-engine turboprop aircraft featuring a comfortable, quiet and spacious cabin for up to 50 business class seats and low fuel consumption. Saab 2000 airplane covers regional routes cruising at 370 knots (680+ kph or 400+ mph). All Saab 2000 versions are powered by two Rolls Royce Allison AE 2100A turboprop engines rated at 4,152-shp each. Saab is offering Saab 2000 turboprop aircraft to commercial customers in three configurations: airliner, corporate shuttle and flight inspection.
Air & Air Defense Specifications
Crew
2
Max Speed
680.0 km/h
Range
2164.0 km
Service Ceiling
9450 m
Wingspan
24.80 m
Overview (Deagel)
Group
Turboprop Airplanes
Status
Active
Origin
Sweden
Contractor
Saab
Initial Operational Capability (IOC)
1994
Total Production
?
Specifications (Deagel)
Crew
2
Number of Engines
2
Passengers
50
Dimensions — Height
7.7 meter
Dimensions — Length
27.3 meter
Dimensions — Wingspan
24.8 meter
Mass — Empty Weight
14,500 kilogram
Mass — Max Takeoff Weight
23,000 kilogram
Mass — Payload
5,500 kilogram
Performance — Ceiling
9,450 meter
Performance — Max Range
2,164 kilometer
Power — Max Power at TakeOff
8,304 shp
Speed — Cruise Speed
191 mps
Gear (Deagel)
Item 1
Turboprop Engines: AE 2100A (2)
Variants
Variant 1
Saab 2000
Variant 2
Saab 2000 AEW&C
Details
Country of Origin
Sweden
Sources
deagel.com: https://www.deagel.com/x/x/a000063 Wikidata (https://www.wikidata.org/wiki/Q1136382)
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
27.3 m
Width
24.8 m
Height
7.7 m
Weight
23000 kg
Related Equipment (1)
Variant
Operators (10)
United States
France
Germany
United Kingdom
Sweden
Finland
Marshall Islands
Portugal
Romania
Switzerland
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