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Bombardier CRJ-100
The CRJ100 is the first Canadair Regional Jet, a 50-seat airliner developed from the Challenger business jet and certified in Canada on July 31, 1992. On its type certificate it is a CL-600-2B19, the same model as the later CRJ200, and the only difference the certificate names is the engine: the CRJ100 has General Electric CF34-3A1 turbofans where the CRJ200 has CF34-3B1s. It shares the CRJ200's size, 87 ft 10 in long with a wingspan of 69 ft 8 in, its T-tail and its 8,082 liters of usable fuel. The heaviest option takes off at 23,995 kg, and it is certified to 41,000 feet. A few still fly in US airspace.
- Engines
- Two General Electric CF34-3A1 turbofans at the tail
- Max takeoff weight
- 52,900 lb (23,995 kg)
Photos from members
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Specifications
| Length | 87 ft 10 in (26.77 m) |
|---|---|
| Wingspan | 69 ft 8 in (21.23 m) |
| Height | 20 ft 9 in (6.32 m) |
| Fuselage width | 8 ft 10 in (2.69 m) |
| Ceiling | 41,000 ft (12,500 m) |
| Fuel capacity | 2,140 US gal (8,082 L) |
| Status | Still flying with a few operators |
| Type codes | ICAO CRJ1 |
Who flies it now
20 flights by other operators
From flights seen in US airspace in the last 14 days (public flight data).
In the air now
No aircraft of this type in the air right now
Flights of this type in the air now, from public flight data.