N313SJ
Raytheon 390 Premier I (Premier I)
Raytheon Aircraft Company
3 Hours
Duration of Flight
1360 NM
Range
461 MPH
Max Speed

Gallery




Basic Information
Airframe
Data valid as of 2025-11-26No flight history available
Flight records for this aircraft have not been tracked yet.
AI Summary
Raytheon 390 Premier I (Premier I)
Overview
US-registered light business jet, Raytheon 390 Premier I, MSN RB-30. Previously carried registrations N84FM / N84ML (RB-30 trace). Photographed as N313SJ at KRDU on 2025-10-25.
Specifications
- Engines: 2× Williams FJ44-2A (2300 lbf each)
- Range: 1360 nm
- Cruise: 426 kts
- Seats: 6
- Ceiling: 41000 ft
Operations & Cabin
Six-place executive club layout (typical Premier I) Reported earlier configuration: six pedestal seats, mahogany laminate cabinetry, beige upholstery; forward refreshment/baggage cabinet and aft lavatory (details from prior RB-30 listing). Avionics: Collins Pro Line 21 (FMS-3000 reported on prior registration RB-30)
Model & Market Context
This entry covers airframe N313SJ, a 2002-built Raytheon 390 Premier I with manufacturer serial RB-30. The airframe is US-registered and carries a build year of 2002; prior registration RB-30 is documented in avionics reporting. Operator and home base details are not published in the supplied data. Notable registry actions include a reported avionics fitment change tied to the aircraft’s prior registration; valuation and current condition highlights are not published.
The airframe is outfitted in a six-place executive club layout typical for the Premier I, described here as a Six-place executive club layout (typical Premier I). Reported avionics include the Collins Pro Line 21 suite, with an FMS-3000 reported on the airframe under its prior registration. With a 1,360 nm range and a 426-knot cruise speed, this specific Premier I is suited to short to mid‑range corporate missions and on-demand charter work within the continental United States. Operator-specific amenities, maintenance history, and base of operations are not published in the supplied data; however, the avionics configuration and cabin layout indicate a standard light‑jet executive mission set for this airframe.
The airframe belongs to the Raytheon 390 Premier I family built by Raytheon Aircraft Company, positioned in the light-cabin, entry-level business jet market. With twin Williams FJ44-2A turbofans and a 41,000 ft service ceiling, the model occupies a performance niche favoring higher cruise speeds and efficient regional point-to-point missions. Competing aircraft in the light-jet segment typically draw comparable charter and owner-operator demand; resale and maintenance considerations for this 2002 airframe include age-related avionics upgrades and engine shop visit cycles consistent with Williams FJ44 powerplants.
Aircraft Comparison
| Parameter | N313SJ | N100HL | N100WE |
|---|---|---|---|
| Serial Number (MSN) | RB-30 | 258345 | RB-45 |
| Year Manufactured | 2002 | 1997 | 2002 |
| Duration of Flight | 3 Hours | 6 Hours | 3 Hours |
| Range | 1360 NM | 2470 NM | 1460 NM |
| Max Speed | 461 MPH | 447 MPH | 454 MPH |
| Aircraft Class | 12,500-19,999lbs | 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. |