CL60

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 Challenger 650
CANADAIR Challenger 605
CANADAIR Challenger 604
CANADAIR Challenger 601
CANADAIR Challenger 600
CANADAIR CE-144A Challenger 600
CANADAIR CC-144B Challenger 601
CANADAIR CC-144 Challenger 600
CANADAIR C-143 Challenger 604
CANADAIR CL-600 Challenger 604
CANADAIR CL-600 Challenger 601
CANADAIR CL-600 Challenger 600
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 (metric)
19.60 m
Length (metric)
20.85 m
Height (metric)
6.30 m
Powerplant

2 x General Electric CF34-3A

Engine Model(s)
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

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