N80CK

CL-600-1A11 (Challenger 600)

Canadair (Bombardier)

7 Hours

Duration of Flight

2909 NM

Range

458 MPH

Max Speed

N80CK

Gallery

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Aircraft Class
Aircraft Class
Over 20,000lbs
Max passengers
Max passengers
21
Range
Range
2909 NM
Service Ceiling
Service Ceiling
41000 ft
Duration of Flight
Duration of Flight
7 Hours
Max Speed
Max Speed
458 MPH

Basic Information

Year Manufactured1982
LocationSalt Lake City, UT, US
Registration NumberN80CK
OwnershipBANK OF UTAH TRUSTEE
Serial Number1069

Airframe

Data valid as of 2023-09-09
AFTT (hrs)
Current
N/A
Flight
N/A
Est.
N/A
Landings/Cycles
Current
N/A
Flight
N/A
Est.
N/A
Nautical Miles
Current
N/A
Flight
N/A
Est.
N/A
No flights

No flight history available

Flight records for this aircraft have not been tracked yet.

AI Summary

Fact-checked by AI

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

ParameterN80CKN2105N236N
Serial Number (MSN)106910105108
Year Manufactured198219861992
Duration of Flight7 Hours7 Hours8 Hours
Range2909 NM2909 NM3430 NM
Max Speed458 MPH480 MPH459 MPH
Aircraft ClassOver 20,000lbsOver 20,000lbsOver 20,000lbs
Service Ceiling41000 ft41000 ft41000 ft
Max Passengers211322
Cabin ComfortNo items found.No items found.No items found.

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