BOMBARDIER Challenger 600

Aircraft
Name: 
Challenger 600
Manufacturer: 
Body: 
Narrow
Wing: 
Fixed Wing
Position: 
Low wing (winglets)
Tail: 
T-tail
WTC
M
APC
C
Type Code: 
L2J
Aerodrome Reference Code: 
3A
Engine: 
Jet
Engine Count: 
Multi
Position: 
Both sides of rear fuselage
Landing gear: 
Tricycle retractable
Manufacturered as
CANADAIR C-143 Challenger 604
CANADAIR CC-144 Challenger 600
CANADAIR CC-144B Challenger 601
CANADAIR CE-144A Challenger 600
CANADAIR Challenger 600
CANADAIR Challenger 601
CANADAIR Challenger 604
CANADAIR Challenger 605
CANADAIR Challenger 650
CANADAIR CL-600 Challenger 600
CANADAIR CL-600 Challenger 601
CANADAIR CL-600 Challenger 604
CANADAIR CL-600 Challenger 605

CL60

The Bombardier Challenger 600 series (600/601/604/605) is a family of business jets designed by Bill Lear and produced first by Canadair until that company was bought by Bombardier Aerospace in 1986. The Challenger was one of the first business jets designed with a supercritical wing.

Technical Data
Wing span: 
19.60 m
Length: 
20.85 m
Height: 
6.30 m
Powerplant: 

2 x General Electric CF34-3A

Engine Model: 
General Electric CF34
Indicative Performance Data
Take-Off
V2: 
n/a
Distance: 
1730 m
MTOW: 
19500 kg
Initial Climb (to 5000 ft)
IAS: 
n/a
ROC: 
n/a
Initial Climb (to FL150)
IAS: 
n/a
ROC: 
n/a
Initial Climb (to FL240)
IAS: 
n/a
ROC: 
n/a
MACH Climb
MACH: 
n/a
ROC: 
n/a
Cruise
TAS: 
432 kts
MACH: 
0.75
Ceiling: 
450
Range: 
3400 NM
Initial Descent (to FL240)
MACH: 
n/a
ROD: 
n/a
Descent (to FL100)
IAS: 
n/a
ROD: 
n/a
Descent (FL100 & below)
IAS: 
n/a
MCS: 
n/a
ROD: 
n/a
Approach
Vapp (IAS): 
n/a
Distance: 
1000 m

SKYbrary Partners:

Safety knowledge contributed by: