N200PR

Raytheon 390 Premier I (Premier I)

Raytheon Aircraft Company

3 Hours

Duration of Flight

1360 NM

Range

451 MPH

Max Speed

N200PR

Gallery

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Aircraft Class
Aircraft Class
12,500 to 20,000lbs
Max passengers
Max passengers
8
Range
Range
1360 NM
Service Ceiling
Service Ceiling
41000 ft
Duration of Flight
Duration of Flight
3 Hours
Max Speed
Max Speed
451 MPH

Basic Information

Year Manufactured2001
LocationRantoul, KS, US
Registration NumberN200PR
OwnershipDodson International Parts Inc
Serial NumberRB-79

Airframe

Data valid as of 2006-09-21
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
DateFromToFlight TimeStatus
2004-04-07N/AN/AN/A✓ Landed

AI Summary

Fact-checked by AI

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

ParameterN200PRN100HLN100WE
Serial Number (MSN)RB-79258345RB-45
Year Manufactured200119972002
Duration of Flight3 Hours6 Hours3 Hours
Range1360 NM2470 NM1460 NM
Max Speed451 MPH447 MPH454 MPH
Aircraft Class12,500 to 20,000lbsOver 20,000lbs12,500-19,999lbs
Service Ceiling41000 ft41000 ft41000 ft
Max Passengers888
Cabin ComfortNo items found.No items found.No items found.

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