N1EG
Raytheon 390 Premier I
Raytheon Aircraft Company
3 Hours
Duration of Flight
1350 NM
Range
454 MPH
Max Speed
Gallery


Basic Information
Airframe
Data valid as of 2025-01-24No flight history available
Flight records for this aircraft have not been tracked yet.
AI Summary
Raytheon 390 Premier I
Overview
U.S. registration N1EG assigned to LEVENSON LOUIS (certificate issue 2025-01-24). Airworthiness date 2002-09-12. Status: Valid/active registration.
Specifications
- Engines: 2× Williams FJ44-2A (2300 lbf each)
- Range: 1350 nm
- Cruise: 451 kts
- Seats: 6
- Ceiling: 41000 ft
Operations & Cabin
Typical 6-place executive club layout (single‑aisle, forward galley, aft lavatory/baggage) Executive seating for 6, forward galley, enclosed lavatory; specific interior fittings vary by refurbishment (broker listings show leather seating and IFIS/IFIS-5000 options). Avionics: Collins Pro Line 21 (typical Pro Line 21 fit on Premier I)
Model & Market Context
This article covers the individual airframe bearing tail number N1EG, a 2002-built Raytheon 390 Premier I with manufacturer serial RB-43. The airframe is registered in the United States and is registered to LEVENSON LOUIS of Atlanta, GA, who is listed as the individual owner and operator/home base contact. The airplane carries a typical market valuation of $1,550,000 in the provided data and is identified as a fixed-wing multi-engine executive jet configured for six occupants. No additional registry actions or prior owners are published in the supplied dataset.
The cabin of N1EG is described as a typical six-place executive club layout with a single aisle, a forward galley, and an aft lavatory/baggage area, reflecting the standard Premier I corporate interior arrangement. Avionics aboard this airframe follow the common fit for the model with a Collins Pro Line 21 installation, supporting integrated flight management and communications for typical business-jet operations. With a maximum cruise of 451 kts and a listed range of 1,350 nm, this specific aircraft is suited to short to mid-range point-to-point executive transport missions out of its Atlanta, GA base. Maintenance and operational considerations for this airframe align with standard Premier I practices, including support for Williams FJ44-2A turbofans and Pro Line 21 avionics lifecycle items.
The Raytheon 390 Premier I occupies a light business-jet niche offering a mix of high-speed cruise and a pressurized composite-fuselage cabin compared with contemporaries. Typical competitors in this performance and capacity segment include several small-cabin light jets that target owner-operators and on-demand charter operators. Buyer demand and resale considerations for this airframe are informed by the airframe year (2002), serial (RB-43), current valuation, and the commonality of its Williams FJ44-2A engines and Pro Line 21 avionics, which influence maintenance availability and aftermarket support.
Aircraft Comparison
| Parameter | N1EG | N100HL | N100WE |
|---|---|---|---|
| Serial Number (MSN) | RB-43 | 258345 | RB-45 |
| Year Manufactured | 2002 | 1997 | 2002 |
| Duration of Flight | 3 Hours | 6 Hours | 3 Hours |
| Range | 1350 NM | 2470 NM | 1460 NM |
| Max Speed | 454 MPH | 447 MPH | 454 MPH |
| Aircraft Class | 12,500 to 19,999 lbs | Over 20,000lbs | 12,500-19,999lbs |
| Service Ceiling | 41000 ft | 41000 ft | 41000 ft |
| Max Passengers | 6 | 8 | 8 |
| Cabin Comfort | No items found. | No items found. | No items found. |