N200PR
Raytheon 390 Premier I (Premier I)
Raytheon Aircraft Company
3 Hours
Duration of Flight
1360 NM
Range
451 MPH
Max Speed

Gallery




Basic Information
Airframe
Data valid as of 2006-09-21| Date | From | To | Flight Time | Status |
|---|---|---|---|---|
| 2004-04-07 | N/A | N/A | N/A | ✓ Landed |
AI Summary
Raytheon 390 Premier I (Premier I)
Overview
N200PR listed on FAA-derived records with registrant Dodson International Parts Inc; last action 2006-09-21; Mode S hex A19358.
Specifications
- Engines: 2× Williams International FJ44-2A (2300 lbf each)
- Range: 1360 nm
- Cruise: 450 kts
- Seats: 8
- Ceiling: 41000 ft
Operations & Cabin
Typical 6-place executive club (many examples); some registry entries list 8 seats for this mark. Executive seating, aft lavatory and refreshment center are common configurations for Premier I interiors. Avionics: Collins Pro Line 21 (common fit / common retrofit package on Premier I examples)
Model & Market Context
The airframe bearing registration N200PR is a 2001-built Raytheon 390 Premier I, serial number RB-79, recorded in U.S. civil registry. Ownership is held by the corporate entity Dodson International Parts Inc, based in Rantoul, KS, US, which appears as the on-record operator/home base for this airframe. Some registry entries for the Premier I mark note an alternate seating declaration, and the file for this specific airframe reflects that variability in interior configuration. The aircraft retains a common retrofit avionics fit encountered on Premier I examples and shows no public record here of major airframe-status anomalies.
The cabin for this Premier I airframe is typically arranged as a 6-place executive club in many examples, though registry entries for this mark including this airframe list 8 seats in certain configurations. Avionics commonly fitted or retrofitted on Premier I examples are the Collins Pro Line 21 suites, and this airframe is recorded with that common fit/retrofit package. Operationally the airframe’s performance—cruise near 450 kts, a 1,360 nm mission radius and a 41,000 ft ceiling—suits short- to mid-range corporate missions, charter hops, and owner-flown transport from its base in Rantoul, KS. Maintenance considerations align with twin–engine light-jet practice for Williams FJ44-series propulsion and Pro Line 21 avionics lifecycle items.
The Raytheon 390 Premier I occupies a light business jet performance niche defined by relatively high cruise speeds and transregional ranges out to roughly 1,360 nm, with eight-seat certification available in some entries. Buyers and charter operators typically value the model for fast point-to-point regional missions and compact cabin ergonomics; resale and maintenance considerations commonly center on Williams FJ44 supportability and avionics upgrade paths such as Pro Line 21 retrofits. The platform’s combination of speed, ceiling, and two-engine simplicity informs its continued demand among owners seeking efficient short- to mid-range transport.
Aircraft Comparison
| Parameter | N200PR | N100HL | N100WE |
|---|---|---|---|
| Serial Number (MSN) | RB-79 | 258345 | RB-45 |
| Year Manufactured | 2001 | 1997 | 2002 |
| Duration of Flight | 3 Hours | 6 Hours | 3 Hours |
| Range | 1360 NM | 2470 NM | 1460 NM |
| Max Speed | 451 MPH | 447 MPH | 454 MPH |
| Aircraft Class | 12,500 to 20,000lbs | Over 20,000lbs | 12,500-19,999lbs |
| Service Ceiling | 41000 ft | 41000 ft | 41000 ft |
| Max Passengers | 8 | 8 | 8 |
| Cabin Comfort | No items found. | No items found. | No items found. |