The Saab 2000
Country of origin
Sweden
Type
50 seat twin turboprop regional airliner
History
The Saab 2000 was a stretched 50 seat, faster development of the successful 340.
Charter a Saab 2000 Aircraft
The SAAB 2000 IS a twin-ENGINE 50 seat regional turboprop airliner produced BY SAAB AB, which IS
headquartered IN Stockholm, Sweden. The SAAB 2000 IS an improved development of the 30 seat SAAB 340,
WITH its major improvements being more powerful Rolls-Royce Allison AE 2100A ENGINES (THEN built BY
Allison) rated AT 4591 shp, a modified wingspan, AND a 24 ft 9 IN (7.55 m) fuselage stretch over the baseline of the
SAAB 340, allowing seating FOR 20 more passengers. WHEN compared TO other turboprop airliners, the SAAB
2000 IS ONE of the fastest ones developed, being able TO cruise AT a maximum speed of 368 knots (682 km/h) AT
25,000 ft. The SAAB 2000 delivers high-speed performance combined WITH turboprop economy. The SAAB 2000
can operate FROM high altitude airfields, taking off WITH maximum load AND fuel even AT very hot temperatures,
WHILE offering rapid rates of climb AND a service ceiling of 31,000 ft.
The Saab 2000, with a cruise speed of over 665km/h (360kt), is one of the fastest turboprop airliners developed.
It combines near jet speeds, including near jet climb and descent rates, with turboprop economy. Saab launched
development of the 2000 in mid December 1988 with a launch order from Crossair for 25 (plus a further 25 on option)
following definition and design studies that revealed a market for a high speed regional turboprop.
The initial Saab 2000 development plan would have seen the 2000 in service in the second half of 1993, but delays
pushed this back until the second half of 1994. The Saab 2000's first flight took place on March 26 1992, and
certification from Europe's Joint Airworthiness Authorities and the USA's FAA was granted in March and April 1994
respectively. Service entry with Crossair occurred a few months later.
While retaining the same cross section as the Saab 340, the 2000 is 7.55m (24ft 9in) longer (seating 15 more
passengers), while the same wing section was retained but the 2000's wing span is 15% greater than the 340's,
and the engines are positioned further outboard.
The 2000 was the first civil application of the advanced Allison (now Rolls-Royce) AE-2100 turboshaft (derived
from the military T406 developed for the revolutionary V-22 Osprey tiltrotor), driving slow turning six blade props.
The flightdeck features a Collins Pro Line 4 EFIS avionics suite with six colour CRT displays. Cabin noise is reduced
by an active noise control system comprising 72 microphones and 36 speakers which generate anti phase noise.
Several European aerospace firms participated in the Saab 2000 manufacturing program including CASA which
designed and built the wing, Westland, which manufactured the rear fuselage, and Valmet of Finland which built the
tail.
Lack of sales and profitability forced Saab to cease 340 and 2000 production, with the lines winding up in 1998.
The last 2000 was delivered to Crossair in April 1999.
Powerplants
Two 3096kW (4152shp) Allison AE-2100A turboprops driving six blade constant speed Dowty propellers.
Performance
Max cruising speed 682km/h (368kt) at 25,000ft, long range cruising speed 594km/h (321kt). Initial rate of climb
2250ft/min. Service ceiling 31,000ft. High speed range with 50 passengers and reserves 2185km (1180nm), range at
long range cruising speed 2868km (1549nm).
Weights
Operating empty 13,800kg (30,423lb), max takeoff 22,800kg (50,265lb).
Dimensions
Wing span 24.76m (81ft 3in), length 27.28m (89ft 6in), height 7.73m (25ft 4in). Wing area 55.7m2 (600.0sq ft).
Capacity
Flightcrew of two. Normal passenger accommodation for 50 at three abreast and 81cm (32in) pitch.
Max seating for 58 at three abreast and 76cm (30in) pitch, with repositioned galley and wardrobe.
Production
63 built.
In 2000, 54 were in airline service with three used as corporate transports.
Saab 2000 Exterior
Performance Specifications
Jet Type SAAB-2000
Category Turboprop Airliner
Max Pax 50
Cruise Speed 424 mph
Range 1783 miles
Min Runway 6086 ft
Interior Specifications
Cabin Length 54.80 ft
Cabin Width 7.10 ft
Cabin Height 6.00 ft
Lavatory Full
Bag Capacity 930 cubic ft
Ankita Verma MBA[HR]
Management Trainee
Gtalk : AnneV.AeroSoft@gmail.com
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Rediff Bol : AnneV.AeroSoft@rediffmail.com
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