N118MT
Canadair CL-600-2B16 Challenger 601-3A (601-3A)
Canadair Ltd (Bombardier)
8 Hours
Duration of Flight
3365 NM
Range
459 MPH
Max Speed

Gallery




Basic Information
Airframe
Data valid as of 2024-06-20No 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
Registered in the United States to ONE WORLD AVIATION 118 LLC (Atlanta, GA). Airworthiness certificate dated 1990-09-25; certificate issue action recorded 2024-06-20 with expiration 2031-06-30. Serial (MSN) 5077; certified as a transport/standard airworthiness class aircraft.
Specifications
- Engines: 2× General Electric CF34 series (CF34-3A family) (9140 lbf each)
- Range: 3365 nm
- Cruise: 442 kts
- Seats: 22
- Ceiling: 41000 ft
Operations & Cabin
Executive layout; commonly 9–12 passenger executive seating with forward galley and aft lavatory (type-cert allowed up to 22 seats). Forward galley, enclosed aft lavatory, typical club/sofa executive seating; individual fit varies by owner/modification. Avionics: Collins Pro Line II (common fit on 601-3A retrofits; fit varies by airframe)
Model & Market Context
This entry covers airframe N118MT, a 1990-built Canadair CL-600-2B16 Challenger 601-3A bearing serial number 5077. The airframe is owned by ONE WORLD AVIATION 118 LLC, an Atlanta, GA–based limited liability company, and is registered in the US. The Challenger 601-3A represented here is listed with an estimated market value of $2,300,000 and has the typical build vintage and configuration associated with early-1990 production Challengers; ownership is recorded to an Atlanta LLC, with no additional publicized operator changes in the supplied data.
The specific cabin of N118MT is configured in an executive layout and the type certification for the model allows up to 22 seats; in practice the Challenger 601-3A airframes are commonly fitted for 9–12 passenger executive seating with a forward galley and aft lavatory. Avionics fit for this airframe class frequently includes the Collins Pro Line II on 601-3A retrofit installations, although the fit varies by airframe and is not uniquely specified beyond the common retrofit compatibility. Typical mission profiles for this aircraft class include medium- to long-range executive transport and private charter missions out of its Atlanta base, leveraging a cruise speed near 442 kts and a transcontinental-capable range of 3,365 nm. Maintenance considerations follow CF34-powered regional and business-jet practices given the twin CF34-3A family engines.
The Canadair/Bombardier Challenger 601-3A occupies a mid-size corporate jet niche, offering transcontinental range and a pressurized, stand-up cabin suitable for executive transport up to the type-cert limit of 22 seats. Competing models in the era and market segment include updated Challenger variants and other late-20th-century business jets with CF34 or equivalent powerplants. Buyer and charter demand for 1990-series 601-3As is influenced by overall airframe condition, avionics retrofit status (e.g., Collins Pro Line II installations), and engine life cycles; these factors, together with the listed valuation of $2,300,000, shape resale and maintenance economics for this specific airframe.
Aircraft Comparison
| Parameter | N118MT | N141RD | N18RC |
|---|---|---|---|
| Serial Number (MSN) | 5077 | 1041 | 5315 |
| Year Manufactured | 1990 | 1982 | 1996 |
| Duration of Flight | 8 Hours | 7 Hours | 9 Hours |
| Range | 3365 NM | 2909 NM | 4033 NM |
| Max Speed | 459 MPH | 458 MPH | 468 MPH |
| Aircraft Class | Over 20,000lbs | Over 20,000lbs | Over 20,000lbs |
| Service Ceiling | 41000 ft | 41000 ft | 41000 ft |
| Max Passengers | 22 | 13 | 22 |
| Cabin Comfort | No items found. | No items found. | No items found. |