N80CK
CL-600-1A11 (Challenger 600)
Canadair (Bombardier)
7 Hours
Duration of Flight
2909 NM
Range
458 MPH
Max Speed

Gallery




Basic Information
Airframe
Data valid as of 2023-09-09No flight history available
Flight records for this aircraft have not been tracked yet.
AI Summary
CL-600-1A11 (Challenger 600)
Overview
United States registration (type: corporation). Certificate issue 2010-10-08; last FAA action 2023-09-09; expiration 2029-10-31.
Specifications
- Engines: 2× ALF-502 (series) (7500 lbf each)
- Range: 2909 nm
- Cruise: 442 kts
- Seats: 21
- Ceiling: 41000 ft
Operations & Cabin
Typical executive layout (commonly 8–12 executive seats); FAA record for this registration lists 21 seats (corporate/commercial configuration possible). Varies by installation; Challenger 600-series wide cabin supports private lavatory, forward galley and multiple seating zones when fitted as an executive transport. Avionics: Original fit typically Sperry/Collins analog flight guidance (SPZ-600 / Collins Pro Line 1); many aircraft have aftermarket avionics retrofits.
Model & Market Context
The airframe bearing tail number N80CK is a 1982-built Canadair/Bombardier CL-600-1A11 (Challenger 600), serial number 1069. Ownership is recorded to BANK OF UTAH TRUSTEE, a corporate trustee based in Salt Lake City, Utah, United States, which places the aircraft's operator/home base interests in the Salt Lake City area. The US-registered Challenger has an FAA record that notably lists 21 seats, indicating a corporate or commercial configuration rather than the more common lower-density executive fit. Valuation and condition details are not published in the available data.
The cabin for this specific Challenger is described as a typical executive layout in the family—commonly fitted with 8–12 executive seats—however, the FAA registration for N80CK lists 21 seats, which signals a corporate/commercial configuration is installed or certificated for this airframe. Original avionics fit for the CL-600-1A11 generally included Sperry/Collins analog flight guidance equipment (SPZ-600 / Collins Pro Line 1), though many airframes in the type have undergone aftermarket avionics retrofits; the exact retrofit status for N80CK is not specified in the record. Typical mission profiles for the type and this airframe would include medium-range executive transport or corporate shuttle missions from its Salt Lake City trustee/operator base, with attention to maintenance of older analog systems if not modernized.
The CL-600-1A11 variant of the Challenger 600 family occupies a medium-range, high-comfort executive jet niche with transcontinental capability reflected by the 2,909 nm range and 41,000 ft ceiling of this airframe. Competing models in its era and secondary market tend to include other large-cabin business jets offering similar range and passenger counts. Market considerations for this airframe include potential avionics modernization, maintenance sourcing for ALF-502 engines, and the resale implications of a 1982 serial 1069 airframe carrying a 21-seat certification versus a conventional executive seating layout.
Aircraft Comparison
| Parameter | N80CK | N2105 | N236N |
|---|---|---|---|
| Serial Number (MSN) | 1069 | 1010 | 5108 |
| Year Manufactured | 1982 | 1986 | 1992 |
| Duration of Flight | 7 Hours | 7 Hours | 8 Hours |
| Range | 2909 NM | 2909 NM | 3430 NM |
| Max Speed | 458 MPH | 480 MPH | 459 MPH |
| Aircraft Class | Over 20,000lbs | Over 20,000lbs | Over 20,000lbs |
| Service Ceiling | 41000 ft | 41000 ft | 41000 ft |
| Max Passengers | 21 | 13 | 22 |
| Cabin Comfort | No items found. | No items found. | No items found. |