The
Bombardier CRJ100 and
CRJ200
are a family of regional airliners
manufactured by Bombardier, and based on the
Canadair Challenger business jet, which was
purchaced from Bill Lear in 1976.
The wide fuselage of the Challenger which
seats 2 passengers on each side of the aisle
suggested early on to Canadair officials
that it would be straightforward to stretch
the aircraft to accomomodate more seats, and
there was a plan for a
Challenger 610E,
which would have had seating for 24
passengers. That lengthening did not occur,
the effort being canceled in 1981, but the
idea did not disappear.
In 1987, studies began for a much more
ambitious stretched configuration, leading
to the formal launch of the
Canadair
Regional Jet program in the spring of
1989. The "Canadair" name was retained
despite the fact that Bombardier had bought
out the company. The first of three
development machines for the initial
CRJ100 performed its first flight on 10
May 1991, though the first prototype
(C-FCRJ) was lost in a spin mishap on July
26, 1993 near Wichita, Kansas. The type
obtained certification in late 1992, with
initial delivery to customers late in that
year.
As of August 2006 a total of 938 CRJ100
and CRJ200 aircraft (all variants) are in
airline service, with 8 further firm orders.
CRJ100
The CL-600 design was stretched 5.92
meters (19 feet 5 inches) to create the
CRJ100, with fuselage plugs fore and aft of
the wing, two more emergency exit doors,
plus a reinforced and modified wing. Typical
seating was 50 passengers, the maximum load
being 52 passengers. The CRJ100 featured a
Collins ProLine 4 avionics suite, Collins
weather radar, GE CF34-3A1 turbofans with
41.0 kN (4,180 kgp / 9,220 lbf), new wings
with extended span, more fuel capacity, and
improved landing gear to handle the higher
weights. It was followed by the
CRJ100 ER
subvariant with 20% more range, and the
CRJ100 LR
subvariant with 40% more range
than the standard CRJ100. The
CRJ 100 SE
sub-variant was produced to more closely
meet the needs of corporate and executive
operators.
CRJ200
The CRJ200 is identical to the 100 model
except for more efficient engines.
Pinnacle Airlines had operated some with
44 seats, designated as
CRJ440, with
closets in the forward areas of the
passenger cabin though these were converted
to 50 seat airplanes. These modifications
were designed to allow operations under
their major airline contract "scope clause"
which restricts major airlines' connection
carriers from operating equipment carrying
50 or more passengers to guard against
usurpation of Air Line Pilots Association
and Allied Pilots Association pilots' union
contract. Similarly, Comair's fleet of
40-seat CRJ200s were sold at a discounted
price to discourage Comair from purchasing
the less expensive and smaller Embraer 135.
There is also a CRJ200 freighter version
which is designated
CRJ200 PF (Package
Freighter) which was developed in
cooperation with Cascade Aerospace on the
request of West Air Sweden.
Source:
Wikipedia
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Specifications
Variant |
CRJ100 ER/LR |
CRJ200 ER/LR |
Crew |
3-4 (2 pilots + 1-2 cabin crew) |
Seating capacity |
50 |
Length
Wing span
Height |
26.77 m (87 ft 10 in)
21.21 m
(69 ft 7 in)
6.22 m (20 ft 5 in) |
Wing area
(net)
Fuselage maximum diameter
Turning circle |
48.35 m2 (520.4 sq ft)
2.69 m (8 ft 10 in)
22.86 m
(75 ft 0 in) |
Engines
(2x)
Takeoff thrust (2x)
Thrust APR (2x) |
GE CF34-3A1
38.83 kN (8,729 lbf)
41.01 kN
(9,220 lbf) |
GE CF34-3B1
38.83 kN (8,729 lbf)
41.01 kN
(9,220 lbf) |
Max Zero
Fuel Weight (ZFW) |
19,958 kg (44,000 lb) |
Max payload
weight |
6,124 kg (13,500 lb) |
Max Take
Off Weight (MTOW) |
24,041 kg (53,000 lb) |
Maximum
range |
ER:
3,000 km (1,864 mi, 1,620 nmi)
LR: 3,710 km (2,305 mi, 2,003 nmi) |
ER:
3,045 km (1,895 mi, 1,644 nmi)
LR: 3,713 km (2,307 mi, 2,004 nmi) |
Basic
cruising speed |
Mach .78 [503 mph, 437 knots]
(593.74 mph ground, 516 knots
ground) |
Flight
ceiling |
12,496 m (41,000 ft) |
Number of
Orders |
1054 |
Certification Date |
unknown |
July 1992 |
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