N444SE
Bombardier Challenger 601-3A (CL-600-2B16) (601-3A)
Canadair / Bombardier
8 Hours
Duration of Flight
3291 NM
Range
459 MPH
Max Speed
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Gallery
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Basic Information
Airframe
Data valid as of 2024-05-31No flight history available
Flight records for this aircraft have not been tracked yet.
AI Summary
Bombardier Challenger 601-3A (CL-600-2B16) (601-3A)
Overview
Registered to ENCORE ENTERPRISES INC (co-ownership listed with Base Capital Funding LLC). 1987 CL-600-2B16 Challenger 601-3A, MSN 5008. Standard/Transport airworthiness. 22 seats; weight class over 20,000 lbs.
Specifications
- Engines: 2× General Electric CF34-3A (9220 lbf each)
- Range: 3291 nm
- Cruise: 424 kts
- Seats: 22
- Ceiling: 41000 ft
Operations & Cabin
Typical executive layout: 10–12 passenger club seating with forward galley and aft lavatory (certificated for up to 22 seats). Stand-up cabin ~28 ft long, ~8.2 ft wide, ~6.1 ft high; forward galley, aft lavatory, baggage ~115 ft³ (model-typical figures). Avionics: Collins Pro Line II (typical for 601-3A installations / upgrades vary by airframe)
Model & Market Context
The airframe bearing tail number N444SE is a 1987-built Bombardier Challenger 601-3A (CL-600-2B16), constructor serial 5008, manufactured by Canadair / Bombardier. The aircraft is registered in the US and is owned by the corporation ENCORE ENTERPRISES INC, based in Dallas, TX, US. This entry reflects the current single-owner status on record and the basic registry identifiers for this specific Challenger 601-3A airframe. No additional ownership transfers, valuation events, or notable registry actions are recorded within the provided data set.
The airframe is typically outfitted in a standard executive configuration: a forward galley, aft lavatory and a club seating arrangement for 10–12 passengers while being certificated for up to 22 seats, matching the listed seating certification. Avionics fit for this model is commonly the Collins Pro Line II, noted as typical for 601-3A installations though specific upgrades can vary by individual airframe. With a cruise speed of 424 knots and a maximum range of 3,291 nautical miles, this aircraft is suited to medium- to long-range executive transport missions from its operator base in Dallas, TX, US, accommodating transcontinental and regionally extended routings within one flight sector. Maintenance and cabin configuration considerations follow standard corporate-jet practice for a Challenger 601-3A type.
The Bombardier Challenger 601-3A (CL-600-2B16) occupies a mid-size long-range business jet niche, combining twin General Electric CF34-3A turbofan performance with a high-cabin comfort layout certificated for up to 22 seats and a service ceiling of 41,000 ft. Its range and cruise profile position it competitively against contemporary midsize and large-cabin business jets for charter and corporate transport. Typical buyer and charter demand considerations include operating economics tied to twin CF34 engines, maintenance status and avionics fit—frequently Pro Line II—plus interior condition and certification for high-density seating when resale or reconfiguration is contemplated.
Aircraft Comparison
| Parameter | N444SE | N111CC | N243JP |
|---|---|---|---|
| Serial Number (MSN) | 5008 | 5192 | 5101 |
| Year Manufactured | 1987 | 1996 | 1991 |
| Duration of Flight | 8 Hours | 8 Hours | 8 Hours |
| Range | 3291 NM | 3430 NM | 3430 NM |
| Max Speed | 459 MPH | 459 MPH | 459 MPH |
| Aircraft Class | Over 20,000lbs | Over 20,000lbs | Over 20,000lbs |
| Service Ceiling | 41000 ft | 41000 ft | 41000 ft |
| Max Passengers | 22 | 22 | 22 |
| Cabin Comfort | No items found. | No items found. | No items found. |