• Model : Bombardier Challenger 605
  • Part Number :
Product Details

Type


CHALLENGER 605


CAPACITY


Passengers


LOPA 1


Crew:2+1 Passenger:Up to 12


LOPA 2


seats: 9


LOPA 3


seats: 11


Dimension


Exterior
(Meter)


Length(m)

20.85


Wingspan(m)

19.61


Height(m)

6.3


Interior
( Meter)


Cabin Length(m)

8.66


Cabin Width (m)

2.49/2.19


Cabin Ceiling Height(m)

1.85


Floor Area(Cockpit Not Included)(m2)

18.8


Luggage capacity: ( m3)

3.3


Performanc


Weight
( Kg)


Maximum Takeoff Weight (Standard)(kg)

21,863


Maximum Payload(kg)

2,275


Payload with Full Fuel(km)

522


Range
( KM)


Maximum Range(CAAC Requirement
Full Payload, NBAA IFR (km)

7,408


Eg:Direct fly to from Beijing


Darwin, Mumbai


Eg:Direct fly to from Shanghai


Delhi


Eg:Direct fly to from Guangzhou


Perth


Speed
( Mach)


Maximum Cruise Speed

0.82


Typical Cruise Speed

0.8


Altitude
( Meter)


Maximum Cruise Altitude(m)

12,479


Typical Cruise Altitude(m)

 


Other


Takeoff Distance (Sea level, International 
Standard Atmosphere,MTOW)(m)

1,780


Landing Distance (Sea level, International 
Standard Atmosphere, Typical Landing Weight)(m)

846


Landing Distance (Sea level, International 
Standard Atmosphere, Typical Landing Weight)(m)


YES


Equipment


Engine


Engine Vendor


General Electric


Engine Quantity

2


Engine Type

CF34-3B


Engine Thrust


8,729 lb


Avionicsw


Avionicsw


Rockwell Collins


Type

Pro Line 21


Operation 
Cost


Direct 
Operation 
Cost


Engine Maintenance Service Plan Price per 
Hour(US$)

455


APU Maintenance Service Plan Price per 
Hour(US$)

/


Direct Operation Cost per Hour(US$)

2,095


Fuel Cost per Hour(US$)

1,443


Maintenance 
Cost


Routine Maintenance Cost per Hour(US$)

343


Fixed Inspection Interval(eg, 
A/B/C/D/E/F/G CHECK)

/

Remarks


NBAA IFR Fuel conditions: 200-mile

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