A/C

Manufacturer

Bombardier

Sources:

Aircraft type

CRJ200

CRJ700

CRJ900

[1]

https://www.flightglobal.com/download?ac=73559

Total number of operating A/C

601

[1]

291

[1]

471

[1]

[2]

https://customer.aero.bombardier.com/webd/BAG/CustSite/BRAD/RACSDocument.nsf/51aae8b2b3bfdf6685256c300045ff31/ec63f8639ff3ab9d85257c1500635bd8/$FILE/ATTQF1EY.pdf/CRJ900APMR11.pdf

Option/Variant

[9]

[6]

CL-6002D24

[3]

https://www.easa.europa.eu/downloads/8355/en

Engine

No. of Engines

[9]

[6]

[2]

[4]

http://mhirj-preview-files.s3-us-west-2.amazonaws.com/mhirj/2020-12/MHIRJ_CRJ900_Factsheet_FR_V1_web.pdf

Model

CF34-3B1

[9]

CF34-8C1

[6]

CF34-8C5

[2]

[5]

https://web.archive.org/web/20210828020119/https:/commercialaircraft.bombardier.com/themes/bca/pdf/Bombardier_CRJ_Series_Brochure.pdf

Max. Rated Takeoff Thrust, T_TO [kN]

41,01

[12]

61,34

[7]

64,54

[7]

[6]

https://customer.aero.bombardier.com/webd/BAG/CustSite/BRAD/RACSDocument.nsf/51aae8b2b3bfdf6685256c300045ff31/ec63f8639ff3ab9d85257c1500635bd8/$FILE/ATTE8Q23.pdf/CRJ700APMR15.pdf

Equivalent Power, P [kW]

[7]

https://www.easa.europa.eu/downloads/18525/en

Propeller

[8]

http://mhirj-preview-files.s3-us-west-2.amazonaws.com/mhirj/2020-12/MHIRJ_CRJ700_Factsheet_FR_V1_web.pdf

Cabin

Length, l_CABIN [m]

12,42

[11]

17,25

[8]

21,13

[5]

[9]

https://customer.aero.bombardier.com/webd/BAG/CustSite/BRAD/RACSDocument.nsf/51aae8b2b3bfdf6685256c300045ff31/ec63f8639ff3ab9d85257c1500635bd8/$FILE/ATT1ES4H.pdf/CRJ200APMR8.pdf

Max. Height, h_CABIN [m]

1,84

[9]

1,89

[5]

1,89

[5]

[10]

https://www.easa.europa.eu/sites/default/files/dfu/TCDS_EASA%20IM%20A%20673_%28CRJ%29_Issue%201_EASA.PDF

Max. Width, d_F,I [m]

2,48

[9]

2,55

[5]

2,55

[5]

[11]

https://www.fzt.haw-hamburg.de/pers/Scholz/arbeiten/DataMorichon.xls

Passenger Compartment Volume, V_CABIN [m³]

N/A

68,81

[8]

84,21

[5]

[12]

https://www.easa.europa.eu/downloads/65434/en

Fuselage

Height, h_F [m]

2,64

[11]

2,69

[6]

2,69

[2]

Comments:

Width, w_F [m]

2,69

[9]

2,69

[6]

2,69

[2]

¹ Still Air, ISA conditions, zero wind, fuel reserves: 10 min taxi, gold 30 min cruise altitude, contingency of 5% of trip fuel

Total

Length, l_A/C [m]

26,77

[9]

32,3

[6]

36,24

[2]

² ISA, 138 lb taxi and APU, 280 lb take-off, 140 lb approach, reserves fuel: 100 nm alternate, 45 min holding at diversion altitude

Span, b_W [m]

21,23

[9]

23,25

[6]

23,24

[2]

³ ISA, 340 lb taxi and APU, 160 lb take-off, 100 lb approach, reserves fuel: 100 nm alternate, 45 min holding at diversion altitude

Height, h_A/C [m]

6,3

[9]

7,51

[6]

7,35

[2]

Landing Gear

Track, l_T [m]

3,14

[9]

4,12

[6]

4,07

[2]

Wheelbase, l_WB [m]

11,4

[9]

15,01

[6]

17,3

[2]

Wing

Area, S_W [m²]

54,54

[11]

70,61

[6]

71,07

[2]

Taper ratio, λ_W

0,32

[11]

0,26

[6]

0,25

[2]

1/4 Chord Sweep, φ_25,W [°]

24,5

[11]

26,5

[6]

[2]

Vertical Tail

Area, S_V [m²]

N/A

11,09

[6]

11,09

[2]

Height, b_V [m]

3,46

[9]

3,61

[6]

3,28

[2]

Taper ratio, λ_V

0,67

[11]

0,67

[6]

0,66

[2]

1/4 Chord Sweep, φ_25,V [°]

[11]

[6]

38,5

[2]

Horizontal Tail

Area, S_H [m²]

N/A

15,91

[6]

15,91

[2]

Span, b_H [m]

6,2

[9]

8,54

[6]

8,54

[2]

Taper Ratio, λ_H

0,46

[11]

0,42

[6]

0,47

[2]

1/4 Chord Sweep, φ_25,H [°]

[11]

[6]

28,5

[2]

Cruise

V_MO [kt]

507

[10]

507

[3]

507

[3]

M_MO [Mach]

0,85

[10]

0,85

[3]

0,85

[3]

Cruise Speed, M_CR [Mach]

0,8

[9]

0,7

[6]

0,7

[2]

Max. Certified Flight Level, h_MCR [FL]

410

[10]

410

[3]

410

[3]

Cruise Altitude, h_CR [FL]

370

[10]

N/A

Fuel

Unusable Fuel [l]

[10]

[3]

128

[2]

Optional Fuel [l]

Max usable fuel [l]

8082

[10]

10989

[3]

10861

[2]

Range

Max. Payload, R_MPL [nm]

1130

¹[9]

1230

²[6]

1320

³[2]

Max. Pax, R_M,pax [nm]

1830

¹[9]

1980

²[6]

1986

³[2]

Max. Range, R_PLMR [nm]

2070

¹[9]

2280

²[6]

1980

³[2]

Mass

Max. Ramp, m_MR (MRM) [kg]

21319

[9]

34133

[6]

38555

[2]

Max. Take-Off, m_MTO (MTOM) [kg]

24041

[9]

34019

[6]

38329

[2]

Max. Landing, m_ML (MLM) [kg]

21319

[9]

30391

[6]

33340

[2]

Max. Zero Fuel, m_MZF (MZFM) [kg]

19958

[9]

28260

[6]

32092

[2]

Operating Empty, m_OE (OEM) (MZFM-MPL) [kg]

13835

[9]

20070

[6]

21845

[2]

Max. Payload, m_MPL (MPL) [kg]

6124

[9]

8190

[5]

10247

[5]

Payload at Max. Range, m_PLMR [kg]

4300

[9]

5580

[6]

7800

[2]

Cargo

Volume, V_CARGO [m³]

8,89

[9]

12,39

[6]

12,39

[2]

Cargo Capacity

Max. Pallet Underfloor

Seats

Max. Seats, n_M,SEAT

[9]

[3]

[2]

Std. Layout, n_SEAT

[9]

[6]

[2]