Bombardier Challenger 600 series

Airplanes

Length

20.7264 m

Flat Wing Span

19.5072 m

Height

6.096 m

Flat Wing Area

45.4296 m²

Flat Wing Aspect Ratio

8.46

Max Seating

Max Mach

0.85 Mach

Max Ceiling

12496.8 m

Number of Engines

Aircraft Engine

First Flight

1978-11-08

Number Built

1066

Maximum Take-Off Weight

21.8632 t (paragliders: kg)

Maximum Range

7408 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Bombardier Challenger 600 series	21.8632	7408

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Beriev R-1	Klimov VK-1	19.9	20		Compare
Martin B-57 Canberra	Wright J65	20	19.5		Compare
English Electric Canberra		19.812	19.5072		Compare
VFW-Fokker 614		20.6	21.5	44	Compare
Bombardier Challenger 300		20.9184	19.2024	19	Compare
Falcon 2000		20.23	21.38	10	Compare

All data (21 fields)

Name: Bombardier Challenger 600 series
Manufacturer: Bombardier
Description: The Bombardier Challenger 600 series is a family of business jets developed by Canadair after a Bill Lear concept, and then produced from 1986 by its new owner, Bombardier Aerospace.
First Flight: 1978-11-08
Designer: Bombardier
Type: Business jet
Length (m): 20.7264
Height (m): 6.096
Max Seating: 19
Max Ceiling (m): 12496.8
Capacity Description: 2,200 kg (4,850 lb) and up to 19 passengers
Max Mach (Mach): 0.85
Number Built: 1066
Powerplant Description: 2 × General Electric CF34-3B turbofans
Status: In production
Wikipedia Article (URL): en.wikipedia.org/wiki/Bombardier_Challenger_600_series
Flat Wing Span (m): 19.5072
Flat Wing Area (m²): 45.4296
Flat Wing Aspect Ratio: 8.46
Aircraft Engine: General Electric CF34
Number of Engines: 2