N605JL
CL-600-2B16 (Challenger 605) (CL-605)
Bombardier Inc
10 Hours
Duration of Flight
4045 NM
Range
470 MPH
Max Speed

Gallery

Basic Information
Airframe
Data valid as of 2023-05-30No flight history available
Flight records for this aircraft have not been tracked yet.
AI Summary
CL-600-2B16 (Challenger 605) (CL-605)
Overview
U.S. registration assigned to BANK OF UTAH TRUSTEE (Salt Lake City, UT). Certificate issue date 2023-05-30; airworthiness 2023-06-09; registration expires 2030-05-31. Mode S hex A7DAA5.
Specifications
- Engines: 2× GE CF34-3B1 (9220 lbf each)
- Range: 4045 nm
- Cruise: 424 kts
- Seats: 22
- Ceiling: 41000 ft
Operations & Cabin
Typical 2-zone executive layout (forward galley, main cabin with club and divan seating) seating commonly 10–12 passengers; type certificated up to 22 seats. Larger cabin windows versus predecessors, enclosed lavatory, forward galley and multiple club/divan seating arrangements; cabin length ~28.3 ft, width ~8.2 ft, height ~6.1 ft (model baseline). Avionics: Rockwell Collins Pro Line 21 (typical for the model)
Model & Market Context
This airframe, registered as N605JL, is a Bombardier-built CL-600-2B16 (Challenger 605) completed in 2010 with manufacturer serial number 5828. The aircraft is owned by BANK OF UTAH TRUSTEE, a corporate trustee recorded in Salt Lake City, UT, US, and is U.S.-registered as a fixed-wing multi-engine aircraft. The recorded trustee ownership marks a notable registry action for the airframe and identifies Salt Lake City as the administrative base for the owner. The aircraft’s listed market valuation is $9,500,000, reflecting its year, model and typical configuration and condition expectations for a 2010 Challenger 605.
The cabin of N605JL is fitted in the typical two-zone executive layout with a forward galley and a main cabin arranged with club seating and a divan, commonly set up to seat 10–12 passengers although the airframe is type certificated for up to 22 seats. Avionics fit for the model is commonly the Rockwell Collins Pro Line 21, a system that supports typical business-jet navigation, communication and flight-management requirements for domestic and transcontinental operations. With a cruise speed of 424 kts and range of 4,045 nm, missions for this airframe commonly include business travel, charter flights and corporate group transport linking regional and transcontinental city pairs from its administrative base in Salt Lake City, UT, US. Maintenance considerations follow Challenger 605 programmes for CF34 series engines and Pro Line avionics support.
The CL-600-2B16 (Challenger 605) occupies the mid-size long-range business jet niche, offering transcontinental capability with comfortable cabin amenities relative to its class. Competitors in similar missions include other mid-size long-range types; buyer and charter demand typically values a modern avionics fit such as Rockwell Collins Pro Line 21 and the CF34-3B1 engine type for performance and supportability. Resale and maintenance considerations for N605JL hinge on documented ownership, engine cycles and avionics condition, with the listed $9,500,000 valuation aligning with market expectations for a 2010 Challenger 605 in corporate ownership.
Aircraft Comparison
| Parameter | N605JL | N100LA | N1038S |
|---|---|---|---|
| Serial Number (MSN) | 5828 | 9321 | 5782 |
| Year Manufactured | 2010 | 2008 | 2008 |
| Duration of Flight | 10 Hours | 11 Hours | 9 Hours |
| Range | 4045 NM | 5200 NM | 4045 NM |
| Max Speed | 470 MPH | 504 MPH | 470 MPH |
| Aircraft Class | Over 20,000lbs | Over 20,000lbs | Over 20,000lbs |
| Service Ceiling | 41000 ft | 51000 ft | 41000 ft |
| Max Passengers | 22 | 8 | 22 |
| Cabin Comfort | No items found. | No items found. | No items found. |