Heavy Jet Charter
Refining the wide-body formula for global range.
Why Charter This Aircraft
Fly nonstop across the U.S. or the Atlantic with ease.
A spacious wide-body cabin.
CF34 turbofans deliver a smooth, quiet ride.
Over 160 aircraft delivered across three variants.
Development & Background
The Challenger 601's story begins in 1983, when Canadair (soon to be acquired by Bombardier) sought to correct the reliability and efficiency limitations of the early Challenger 600 while retaining its wide-body comfort and long-range performance.
The first iteration, the 601-1A, introduced General Electric CF34-1A engines, replacing the Lycoming ALF 502Ls used in the 600. The new high-bypass engines dramatically improved thrust and fuel efficiency, while enhancing climb performance and cruise stability. Canadair also strengthened the wing and incorporated drag-reducing winglets — a first for the series — improving range by nearly 300 nautical miles. This model was also the first Challenger to feature a glass cockpit architecture and upgraded avionics, allowing Category II ILS approaches. Certification was achieved in September 1983.
In 1987, Bombardier took over Canadair and immediately began refining the program. The 601-3A replaced the engines with GE CF34-3A powerplants with digital controls and improved compressor stages, alongside a Collins EFIS flight deck, dual FMS systems, and increased MTOW. Cabin pressurization systems were upgraded, allowing smoother climbs to 41,000 feet. The 601-3A became Bombardier's first truly global business jet, operating comfortably on routes such as New York to London or Los Angeles to Honolulu.
The 601-3R, introduced in 1993, brought further refinements focused on increased fuel capacity and extended range. Bombardier integrated auxiliary center fuel tanks, boosting range to nearly 3,800 nautical miles, and standardized EFIS and autopilot systems from the upcoming Challenger 604. By the time the 601-3R ended production in 1996, more than 160 aircraft had been delivered — many still flying today under private, charter, and government operation.
Specifications
| Metric | Challenger 601-1A | Challenger 601-3A | Challenger 601-3R |
|---|---|---|---|
| Passenger Capacity | 9–12 | 9–12 | 9–12 |
| Range | ~3,200 nm | ~3,500 nm | ~3,800 nm |
| Max Cruise Speed | Mach 0.80 (460 KTAS) | Mach 0.82 (470 KTAS) | Mach 0.82 (470 KTAS) |
| Service Ceiling | 41,000 ft | 41,000 ft | 41,000 ft |
| Takeoff Distance (MTOW) | ~5,400 ft | ~5,400 ft | ~5,500 ft |
| Landing Distance | ~2,600 ft | ~2,600 ft | ~2,600 ft |
| Cabin Dimensions | 28 ft × 8.2 ft × 6.1 ft | Same | Same |
| Engines | 2 × GE CF34-1A | 2 × GE CF34-3A | 2 × GE CF34-3R |
| Thrust per Engine | 8,650 lbf | 8,850 lbf | 8,850 lbf |
| MTOW | 43,000 lb | 43,000 lb | 44,000 lb |
Cabin & Interior Experience
The Challenger 601 preserved the wide, flat-floor cabin layout that defined the series, measuring 8.2 feet wide, 6.1 feet high, and 28 feet long. Most configurations feature double-club seating, a three-person divan, a forward galley, and a fully enclosed lavatory.
Noise suppression improved significantly from the 600 series, thanks to better insulation and redesigned engine pylons. Today, modernized interiors often feature Wi-Fi, touch-screen cabin management systems, and leather-appointed seating rivaling more recent jets.
Capabilities & Performance
The Challenger 601 is equipped with two General Electric CF34 engines producing between 8,650 and 8,850 lbs of thrust. Depending on variant, it has a range between 3,200 and 3,800 nm, a max cruise speed of Mach 0.82 (470 KTAS), a service ceiling of 41,000 ft, and a fuel burn of roughly 320 gallons per hour. Takeoff distance runs about 5,400 ft, with a landing distance of 2,600 ft, making it accessible at most regional airports.
Pilots are given Honeywell SPZ-8000 avionics with dual EFIS and FMS on earlier variants, while later aircraft host the standard Collins Pro Line 4 suite. As a two-pilot aircraft, captains are typically hired around 4,000 total flight hours, with first officers around 2,000.
Charter Pricing
| Direct Operating Cost | $5,200 – $5,800/hr |
| Charter Rate | $9,000 – $10,500/hr |
| Fuel Burn | ~320 GPH |
| Maintenance Programs | SmartParts, JSSI |
| Average Used Value (2025) | $2.5M – $3.4M |
Estimates only — actual pricing varies by operator availability, seasonality, and routing. Request a quote for an exact rate.
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