CL-600 Challenger vs DC-3
Overview
The CL-600 Challenger and the DC-3 are both Military Transport Aircraft, manufactured by Bombardier and Douglas respectively.
The CL-600 Challenger reaches 882 km/h — 2.1x the DC-3's 413 km/h. The CL-600 Challenger has an operational range of 7,400 km vs 2,540 km for the DC-3. The CL-600 Challenger operates at altitudes up to 12,497 m compared to 7,071 m for the DC-3.
The CL-600 Challenger has been produced in 1,066 units vs 10,174 for the DC-3. Unit cost is $14M for the CL-600 Challenger vs $0.08M for the DC-3. The DC-3 first flew 37 years before the CL-600 Challenger (1941 vs 1978).
| Canadian business jet, introduced in the 1980s, extensively deployed for VIP and corporate travel worldwide. | |
|
|
| Origin country | 🇨🇦 Canada |
| Category | Military Transport Aircraft |
| Manufacturer | Bombardier |
| First flight | 8 November 1978 |
| Year introduced | 1980 |
| Number produced | 1066 units |
| Average unit price | $14 million |
| American commercial airliner, renowned for significant contributions to World War II airlift operations, frequently used for cargo and passenger transport. | |
|
|
| Origin country | 🇺🇸 United States |
| Category | Military Transport Aircraft |
| Manufacturer | Douglas |
| First flight | 23 December 1941 |
| Year introduced | 1936 |
| Number produced | 10174 units |
| Average unit price | $80K |
| Wing area | 48.3 m² ◉ |
| Wingspan | 19.6 m ◉ |
| Height | 6.3 m ◉ |
| Length | 20.9 m ◉ |
| Maximum speed | 882 km/h ◉ |
| Operational range | 7,400 km ◉ |
| Service ceiling | 12,497 m ◉ |
| Max. takeoff weight | 19,550 kg ◉ |
| Empty weight | 9,292 kg ◉ |
| Total thrust | 2 x 2,073 kgf ◉ |
| Wing area | 91.7 m² ◉ |
| Wingspan | 29.0 m ◉ |
| Height | 5.6 m ◉ |
| Length | 22.7 m ◉ |
| Maximum speed | 413 km/h ◉ |
| Operational range | 2,540 km ◉ |
| Service ceiling | 7,071 m ◉ |
| Max. takeoff weight | 13,154 kg ◉ |
| Empty weight | 6,450 kg ◉ |
| Total thrust | 3 x 292 kW ◉ |
Performance Radar Chart
Detailed Comparison
Loading analysis...
Generating comparison analysis...
Unable to generate comparison at this time.
Frequently Asked Questions
Which is faster, the CL-600 Challenger or DC-3?
The CL-600 Challenger is faster with a maximum speed of 882 km/h compared to the DC-3's 413 km/h, a difference of 469 km/h.
Which has longer range, the CL-600 Challenger or DC-3?
The CL-600 Challenger has a longer range at 7,400 km compared to the DC-3's 2,540 km.
Which can fly higher, the CL-600 Challenger or DC-3?
The CL-600 Challenger has a higher service ceiling at 12,497 meters (41,000 ft) compared to the DC-3's 7,071 meters (23,198 ft).
Which is heavier, the CL-600 Challenger or DC-3?
The CL-600 Challenger has a higher maximum takeoff weight at 19,550 kg compared to the DC-3's 13,154 kg.
Which is larger, the CL-600 Challenger or DC-3?
The DC-3 is longer at 22.7 meters compared to the CL-600 Challenger's 20.9 meters.
Which is more expensive, the CL-600 Challenger or DC-3?
The CL-600 Challenger is more expensive at approximately $14 million per unit compared to the DC-3 at $0.1 million.
Which entered service first, the CL-600 Challenger or DC-3?
The DC-3 entered service first in 1936, 44 years before the CL-600 Challenger which entered service in 1980.
Which has been built in greater numbers, the CL-600 Challenger or DC-3?
The DC-3 has been produced in greater numbers with 10,174 units compared to 1,066 units of the CL-600 Challenger.