- Year
- 2028
- Location
- Boca Raton, United States
Specifications
Performance (across variants)
- Range ·
- 3,400 nm
- Cruise ·
- 432 kt
- Service ceiling ·
- 45,000 ft
- MTOW ·
- 19,500 kg
- Passengers ·
- 12 as configured (up to 19 across variants)
Avionics equipment
- Proline 21
- Rockwell Collins
Avionics
Rockwell Collins, Proline 21
Description
Challenger 650 – Delivery Position 1st Quarter 2028 Download Pdf Maximum Range 4000 nm Maximum speed .85 mach High Speed cruise .82 mach Typical cruise Speed .80 mach Takeoff distance 5,640 ft (SL, ISA, MTOW) Landing Distance 2,402 ft (SL, ISA) Maximum operating altitude 41,000 ft Initial cruise altitude 37,000 ft (MTOW) Cabin layout can be configured for up to 12 passengers AVIONICS: Rockwell Collins Proline 21 Advanced Suite with 4-large displays Dual Flight Management Systems with LPV and RNP approach capabilities Synthetic Vision System (SVS) MultiScan weather radar Dual Inertial Reference System (IRS) Dual SBAS and WAAS GPS Photo Gallery Aircraft Specification Floor Plan Challenger 650 Maximum Range 4000 nm Maximum speed .85 mach High Speed cruise .82 mach Typical cruise Speed .80 mach Takeoff distance 5,640 ft (SL, ISA, MTOW) Landing Distance 2,402 ft (SL, ISA) Maximum operating altitude 41,000 ft Initial cruise altitude 37,000 ft (MTOW) Cabin layout can be configured for up to 12 passengers AVIONICS: Rockwell Collins Proline 21 Advanced Suite with 4-large displays Dual Flight Management Systems with LPV and RNP approach capabilities Synthetic Vision System (SVS) MultiScan weather radar Dual Inertial Reference System (IRS) Dual SBAS and WAAS GPS Standard Cabin Layout
