Bombardier Challenger 601-1A
CL60The Bombardier Challenger 601-1A is a large jet produced between 1983 and 1987. It has up to 19 passengers.
Source: RAB-ANAC (data as of 11/7/2026) and Jet Tracker catalog (spec sheet reviewed on 11/7/2026).
Temporal identity
The Challenger 601-1A (CL-600-2A12) is the Challenger 600 version with General Electric CF34-1A engines, certificated in Canada on 25 February 1983. The TCDS lists serial numbers 1003 and 3001 to 3066; JETNET counts 65 aircraft built up to 1987. This page covers the Challenger 601 before the 601-3A, with a maximum takeoff weight of 43,100 lb (19,550 kg) in the TCDS.
Detailed specs
Performance
- Engine
- 2x General Electric CF34-1A, 8,650 lbf (some with CF34-3A or CF34-3A2)
Cabin and comfort
- Wi-Fi
- Optional Iridium / SwiftBroadband retrofit
- Lavatory
- Aft fully enclosed externally serviced + full-service forward galley
- Configuration
- 9-12 passengers in double-club + divan or club + conference layout
- Cabin length (alternate source)
- 8.61 m
- Typical configuration
- Double Club 8 + Divan
- Stand-up cabin
- Yes
- Cabin volume
- 32.56 m³
- Differential pressurization
- 8.8 psi
- Baggage capacity
- 115 cu ft
Avionics and engines
- Engines
- 2× General Electric CF34-1A (8,650 lbf)
Operating costs
Detailed specs pending
External dimensions
- Overall length
- 20.8 m
- Wingspan
- 19.59 m
- Height
- 6.27 m
- Wing area
- 45.4 m²
Weights & fuel
- Maximum takeoff weight (MTOW)
- 19,550 kg
Cabin
Typical factory configuration (curated data). The drawing below is schematic and at approximate scale; the actual layout varies by interior and year.
History
Lineage
Curiosities and highlights
Frequently asked questions
How many passengers does the Bombardier Challenger 601-1A seat?
The Bombardier Challenger 601-1A seats up to 19 passengers, crew not included.