Bombardier CRJ100
Overview
The Bombardier CRJ100 is a commercial aircraft manufactured by Bombardier, with the profile centered on its regional jet role. It first flew in 1991-05-10 and entered service in 1992. The current production-status field is listed as In Production. The listed configuration provides for a crew of 2 and passenger capacity of 50. Power is provided by 2 General Electric CF34-3A engines. Recorded dimensions include length 87.8 ft, wingspan 69.6 ft, height 20.7 ft. Maximum takeoff weight is listed as 47,450 lb. Listed performance includes range 1495 nautical miles, service ceiling 41000 ft. Its ICAO type designator is CRJ1. Figures shown here describe the listed type or configuration and may vary by sub-variant, certification basis, or operator fit.
Quick Facts
Specifications
| ICAO Type Code | CRJ1 |
|---|---|
| First Flight | May 10, 1991 |
| Introduction Date | 1992 |
| Crew | 2 |
| Passenger Capacity | 50 |
| Length | 87.8 ft |
| Wingspan / Rotor Diameter | 69.6 ft |
| Height | 20.7 ft |
| Max Takeoff Weight | 47,450 lb |
| Range | 1495 nm |
| Service Ceiling | 41000 ft |
| Engine Manufacturer | General Electric |
| Engine Model | CF34-3A |
| Engine Count | 2 |
Data verification status: Partially Verified