Bombardier Challenger 601-1A Performance Specs

Aircraft Performance

Weights (lb) Challenger 601-1A, CL-600-2A12
Max Ramp 43,250
Max Takeoff 43,100
Max Landing 36,000
Zero Fuel 31,000c
BOW 24,585
Max Payload 6,415
Useful Load 18,665
Executive Payload 1,800
Max Fuel 16,665
Max Fuel 16,665
Avail Payload Max Fuel 2,000
Avail Fuel Max Payload 12,250
Avail Fuel Exec Payload 16,665
Limits Challenger 601-1A, CL-600-2A12
MMO 0.850
Transition Altitude FL/VMO N/A
Cabin Pressurization (PSI) 8.8
Airport Performance Challenger 601-1A, CL-600-2A12
TO (Sea Level, ISA Temp) 5,400
TO (5000′, @25C) 10,100
Hot/High WAT 43,100
NBAA IFR Ranges
V2 @ SL ISA, MTOW
3,440
144
VREF 134
Landing Distance with 4 Passengers 2,925
Climb Challenger 601-1A, CL-600-2A12
Time to Climb/Alt N/A
Engine Out Rate fpm 1,048
FAR 25 Engine-Out Grad (ft/nm) 438
Ceilings (ft) Challenger 601-1A, CL-600-2A12
Certificated 41,000
All Eng Srv 38,145
Eng Out Service 19,500
Sea Level Cabin 23,200
Long Range Cruise Challenger 601-1A, CL-600-2A12
KTAS 424
Fuel Flow 1,692
Altitude FL 410
Specific Range 0.251
High Speed Cruise Challenger 601-1A, CL-600-2A12
KTAS 459
Fuel Flow 2,067
Altitude FL 390
Specific Range 0.222
Data based on latest manufactured year