N313SJ

Raytheon 390 Premier I (Premier I)

Raytheon Aircraft Company

3 Hours

Duration of Flight

1360 NM

Range

461 MPH

Max Speed

N313SJ

Gallery

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Aircraft Class
Aircraft Class
12,500-19,999lbs
Max passengers
Max passengers
6
Range
Range
1360 NM
Service Ceiling
Service Ceiling
41000 ft
Duration of Flight
Duration of Flight
3 Hours
Max Speed
Max Speed
461 MPH

Basic Information

Year Manufactured2002
Registration NumberN313SJ
Serial NumberRB-30

Airframe

Data valid as of 2025-11-26
AFTT (hrs)
Current
N/A
Flight
N/A
Est.
N/A
Landings/Cycles
Current
N/A
Flight
N/A
Est.
N/A
Nautical Miles
Current
N/A
Flight
N/A
Est.
N/A
No flights

No flight history available

Flight records for this aircraft have not been tracked yet.

AI Summary

Fact-checked by AI

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

ParameterN313SJN100HLN100WE
Serial Number (MSN)RB-30258345RB-45
Year Manufactured200219972002
Duration of Flight3 Hours6 Hours3 Hours
Range1360 NM2470 NM1460 NM
Max Speed461 MPH447 MPH454 MPH
Aircraft Class12,500-19,999lbsOver 20,000lbs12,500-19,999lbs
Service Ceiling41000 ft41000 ft41000 ft
Max Passengers688
Cabin ComfortNo items found.No items found.No items found.

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