Time Period: Post-WW2
Country of Origin: Canada
Type: Airliners
Manufacturer: Bombardier, Inc.
Bombardier Challenger 600 Series Aircraft Overview
The Bombardier Challenger 600 is a family of business jets produced by Bombardier Aerospace, a Canadian aircraft manufacturer. It was the company’s first foray into the business jet market and has paved the way for the highly successful Challenger series.
The Challenger 600 was initially developed by Canadair in the late 1970s as a larger and more capable follow-up to their successful CL-41 Tutor military trainer aircraft. It was designed to meet the growing demand for long-range, high-performance business jets.
The aircraft features a spacious and comfortable cabin, offering luxurious accommodations for passengers. It has a typical seating capacity of 8 to 12 passengers, depending on the specific model and interior configuration. The cabin can be customized to include various amenities and configurations to suit the needs and preferences of the owners.
The Challenger 600 series is known for its exceptional performance, capable of flying at high speeds and long distances. It is powered by two turbofan engines, providing excellent thrust and fuel efficiency. The aircraft offers a range of approximately 5,700 kilometers (3,000 nautical miles), allowing for non-stop transcontinental flights.
Over the years, Bombardier has introduced several variants of the Challenger 600, including the Challenger 601, Challenger 604, Challenger 605, and the latest model, the Challenger 650. Each variant incorporates improvements in avionics, systems, and performance to enhance the overall flying experience.
The Challenger 600 series has been widely adopted by corporate and private jet operators around the world, renowned for its reliability, comfort, and versatility. It has set the standard for business aviation and continues to be a popular choice among discerning travelers seeking luxurious and efficient transportation.
Bombardier Challanger 650 Specifications
- Crew: 2 (pilot and co-pilot)
- Passenger Capacity: Up to 19 passengers with a total payload of 2,200 kg (4,850 lb)
- Length: 20.85 meters (68 feet 5 inches)
- Wingspan: 19.61 meters (64 feet 4 inches)
- Height: 6.30 meters (20 feet 8 inches)
- Wing Area: 45.4 square meters (489 square feet)
- Aspect Ratio: 8.46
- Empty Weight: 12,315 kilograms (27,150 pounds)
- Maximum Takeoff Weight: 21,863 kilograms (48,200 pounds)
- Fuel Capacity: 9,072 kilograms (20,000 pounds)
- Cabin Dimensions: 1.83 meters (6 feet) high, 2.41 meters (7 feet 11 inches) wide
- Engines: 2 × General Electric CF34-3B turbofan engines, each providing 41.0 kN (9,220 lbf) of thrust
Bombardier Challanger 650 Performance
- Maximum Speed: Mach 0.85
- Range: 7,400 kilometers (4,600 miles, 4,000 nautical miles)
- Service Ceiling: 12,000 meters (41,000 feet)
- Thrust-to-Weight Ratio: 0.38
- Takeoff Distance: 1,720 meters (5,640 feet) at sea level, ISA conditions, maximum takeoff weight
- Landing Distance: 732 meters (2,402 feet) at sea level, ISA conditions, typical landing weight