N517BB
Canadair CL-600-2B16 Challenger 601-3A (601-3A)
Canadair Ltd
8 Hours
Duration of Flight
3290 NM
Range
459 MPH
Max Speed

Gallery




Basic Information
Airframe
Data valid as of 2023-01-13No flight history available
Flight records for this aircraft have not been tracked yet.
AI Summary
Canadair CL-600-2B16 Challenger 601-3A (601-3A)
Overview
US registration assigned to Gulfview Aviation LLC (Wilmington, DE). Certificate issued 2023-01-13; airworthiness date 1989-08-24; Mode S A67B8B. Serial (MSN) 5047.
Specifications
- Engines: 2× GE CF34 series (9140 lbf each)
- Range: 3290 nm
- Cruise: 424 kts
- Seats: 22
- Ceiling: 41000 ft
Operations & Cabin
Certified 22 seats; commonly fitted with executive 9–12 passenger layouts (forward club, aft conference/couch) in typical operations. Forward galley, aft lavatory and generous cabin volume (~28 ft cabin length, typical Challenger 601 interior); baggage roughly ~115 cu ft in many examples. Avionics: Varies by retrofit; installed equipment listings include Collins ADF-462, Collins VHF-422C and Aircell ST-3100 Iridium on this airframe (airframe-specific avionics may differ).
Model & Market Context
The aircraft bearing tail number N517BB is a Canadair CL-600-2B16 Challenger 601-3A built in 1989 with serial number 5047. The airframe is registered in the United States and is recorded as owned by Gulfview Aviation LLC, an LLC based in Wilmington, DE, US, which serves as the operator/home base for typical movements and registry correspondence. The airframe-specific avionics fit has been modified over time and this airframe in particular lists installations such as Collins ADF-462, Collins VHF-422C and an Aircell ST-3100 Iridium unit; such retrofits reflect common upgrade activity for late-1980s Challenger airframes. Current market valuation for this aircraft is approximately $2,300,000, a figure reflective of its vintage, configuration, and systems status.
The cabin of this Challenger is certified for 22 seats but is commonly fitted in executive service with nine to twelve passengers in a typical forward club and aft conference or couch arrangement, reflecting its flexible role between high-density transport and corporate shuttle missions. Avionics on this specific airframe include Collins ADF-462, Collins VHF-422C and an Aircell ST-3100 Iridium installation, though installed equipment lists vary by retrofit history and operator choices. With a range of 3,290 nm and a cruise speed near 424 kts, typical operations include transcontinental and regional corporate transport, charter operations, and ad hoc executive missions originating from the Wilmington, DE area. Being a 1989-built airframe, ongoing maintenance, avionics retrofits and component life-limit considerations are typical operational factors for this aircraft.
The Canadair CL-600-2B16 Challenger 601-3A occupies the medium-range, twin-engine business jet niche, offering transcontinental capability and cabin flexibility for passenger or corporate layouts. With twin GE CF34 engines producing about 9,140 lbf each, the model balances performance and operating economics relative to contemporaries in the late-1980s and 1990s business jet market. Buyer and charter demand for aircraft of this vintage tends to focus on operators willing to invest in avionics and interiors, and resale considerations center on maintenance status, retrofit history and the certificated 22-seat capability versus commonly desired executive reconfigurations.
Aircraft Comparison
| Parameter | N517BB | N163ET | N199P |
|---|---|---|---|
| Serial Number (MSN) | 5047 | 1035 | 5112 |
| Year Manufactured | 1989 | 1981 | 1992 |
| Duration of Flight | 8 Hours | 8 Hours | 8 Hours |
| Range | 3290 NM | 3661 NM | 3430 NM |
| Max Speed | 459 MPH | 488 MPH | 459 MPH |
| Aircraft Class | Over 20,000lbs | Over 20,000lbs | Over 20,000lbs |
| Service Ceiling | 41000 ft | 45000 ft | 41000 ft |
| Max Passengers | 22 | 13 | 22 |
| Cabin Comfort | No items found. | No items found. | No items found. |