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CRJ700
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Specifications

 

General
Flight Crew 2
Cabin Crew 2
Passengers Up to 78


Engines
Number Two General Electric CF34-8C5 turbofans
Thrust 12,670 pounds (56.4 kN) thrust at take-off
Flat rating 13,790 pounds (61.3 kN) thrust APR*
86° F (ISA+15°C)
* Uninstalled


Avionics
Collins Pro Line 4 six-tube EFIS/EICAS
Dual attitude heading reference systems (AHRS)
Traffic alert and collision avoidance system (TCAS)
Collins digital weather radar
 
 

 
 
Dimensions


External:
Length overall 106 ft 8 in 32.51 m
Wingspan 76 ft 3 in 23.24 m
Wing area (net) 760 ft2 70.61 m2
Height overall 24 ft 10 in 7.57 m
Fuselage maximum diameter 8 ft 10 in 2.69 m
Turning Circle 75 ft 22.86 m


Internal:

Cabin length (excluding cockpit) 56 ft 8.5 in 17.28 m
Cabin maximum width (centreline) 8 ft 5 in 2.57 m
Cabin width (floor level) 7 ft 0 in 2.13 m
Maximum height 6 ft 2.25 in 1.89 m
Floor area (excluding cockpit) 396.95 ft2 36.88 m2
Cabin volume 2,430 ft3 68.81 m3
Baggage volume (checked and on-board) 812.7 ft3 23.01 m3


Doors and exits:

Passenger door (LH, fwd)
  Height 5 ft 10 in 1.78 m
  Width 3 ft 0.91 m
  Height to sill 5 ft 8 in 1.73 m
Aft cargo door (LH, aft)
  Height 2 ft 9 in 0.84 m
  Width 3 ft 7 in 1.09 m
  Height to sill 7 ft 7 in 2.31 m
Forward underfloor cargo door (LH, fwd)
  Height 1 ft 8 in 0.51 m
  Width 3 ft 6 in 1.07 m
  Height to sill 4 ft 2.5 in 1.28 m
Service door (RH, fwd)
  Height 4 ft 1.22 m
  Width 2 ft 0.61 m
  Height to sill 5 ft 8 in 1.73 m
 
 

 
 
Weights
Maximum ramp weight (Series 701) 73,000 lb 33,131 kg
Maximum ramp weight (Series 701 ER) 75,250 lb 34,133 kg
Maximum ramp weight (Series 701 LR) 77,500 lb 35,153 kg
Maximum take-off weight (Series 701) 72,750 lb 32,995 kg
Maximum take-off weight (Series 701 ER) 75,000 lb 34,019 kg
Maximum take-off weight (Series 701 LR) 77,000 lb 34,926 kg
Maximum landing weight
(Series 701 / 701 ER)		 67,000 lb 30,390 kg
Maximum landing weight (Series 701 LR) 67,600 lb 30,662 kg
Maximum zero fuel weight
(Series 701 / 701 ER)		 62,300 lb 28,259 kg
Maximum zero fuel weight (Series 701 LR) 63,495 lb 28,801 kg
Operating weight empty 43,500 lb 19,731 kg
Maximum fuel load 19,450 lb 8,823 kg
Maximum payload
(Series 701 / 701 ER)		 18,800 lb 8,527 kg
Maximum payload (Series 701 LR) 19,995 lb 9,070 kg
Payload with full fuel (Series 701) 10,050 lb 4,559 kg
Payload with full fuel (Series 701 ER) 12,300 lb 5,579 kg
Payload with full fuel (Series 701 LR) 14,550 lb 6,600 kg
 
 

 
 
Performance

Range:
Maximum range at LRC, FAA 121, 220 lb. pax (100 kg. pax) NM SM KM
CRJ700 Series 701 (70 pax) 1,434 1,690 2,655
CRJ700 Series 701ER (70 pax) 1,732 1,993 3,209
CRJ700 Series 701LR (70 pax) 2,002 2,304 3,708

Speeds:
  Mach kts. mph km/h
High cruise speed 0.825 473 544 876
Normal cruise speed 0.78 447 515 829


Airfield Performance:

CRJ700 Series 701
FAR take-off field length (SL, ISA) at MTOW 5,130 ft 1,564 m
FAR landing field length (SL) at MLW 5,090 ft 1,551 m

CRJ700 Series 701 ER
FAR take-off field length (SL, ISA) at MTOW 5,500 ft 1,676 m
FAR landing field length (SL) at MLW 5,090 ft 1,531 m

CRJ700 Series 701 LR
FAR take-off field length (SL, ISA) at MTOW 6,072 ft 1,851 m
FAR landing field length (SL) at MLW 5,119 ft 1,560 m
     
Fuel consumption per hour
(cruise average)		 444 U.S. gal 1,680 L

Ceiling:
Maximum operating altitude 41,000 ft  12,496 m

Noise Level:		  


Take-off
EPNdB
82.7		 FAR 36
EPNdB
89
Approach 92.6 98
Sideline 89.4 94
 
Avionics
Dimensions
Weights and fuel capacity
Performance
Bombardier CRJ700 nacelle
Bombardier CRJ700 Cockpit

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