N330AC
Raytheon 390 Premier I (Premier IA) (1A)
Raytheon Aircraft Company
3 Hours
Duration of Flight
1360 NM
Range
454 MPH
Max Speed

Gallery




Basic Information
Airframe
Data valid as of 2025-02-14No flight history available
Flight records for this aircraft have not been tracked yet.
AI Summary
Raytheon 390 Premier I (Premier IA) (1A)
Overview
US registration assigned to LEXAIR LLC (Mangonia Park, FL). Certificate issued 2023-12-05; airworthiness date 2007-01-22; registration expiration 2030-12-31.
Specifications
- Engines: 2× Williams FJ44-2A (2300 lbf each)
- Range: 1360 nm
- Cruise: 426 kts
- Seats: 8
- Ceiling: 41000 ft
Operations & Cabin
Typical executive 6–8-place club layout (6 executive seats common; up to 8 possible with belted lav), enclosed lavatory, 77 cu ft baggage Spacious light-jet cabin for class (approx 13.5 ft × 5.5 ft × 5.4 ft); executive club seating and folding tables commonly fitted on 2007 Premier IA airframes Avionics: Collins / Rockwell Collins Pro Line 21 (typical installation for Premier I/IA)
Model & Market Context
The airframe bearing tail number N330AC is a 2007-built Raytheon 390 Premier I (Premier IA) with serial RB-173, manufactured by Raytheon Aircraft Company. Registered in the United States and recorded as owned by LEXAIR LLC, an LLC based in Mangonia Park, FL, US, this specific Premier I represents the later-production execution of the type in the mid-2000s. Registry entries and owner location indicate an operator/home base link to Mangonia Park, Florida, with the airframe valuation listed at $1,938,691, reflecting market assessment for a 2007 Premier I in typical executive configuration. Notable registry actions include the formal U.S. registration under the tail N330AC and continued operation under the owner/operator entity LEXAIR LLC.
The cabin of N330AC is fitted in a typical executive 6–8-place club layout, with six executive seats common and up to eight seats possible when using the belted lavatory option; an enclosed lavatory is fitted and the airframe offers 77 cu ft of baggage capacity. Avionics for the airframe reflect the common installation for Premier I/IA examples, the Collins / Rockwell Collins Pro Line 21 suite, supporting modern navigation, flight management, and communications for business missions. Typical missions for this airframe would include short-to-medium range executive transport and on-demand charter segments from its Mangonia Park-associated operator, balancing fast cruise performance with light-jet operating economics. Maintenance considerations align with Williams FJ44 engine support and Pro Line 21 avionics lifecycle management typical of the fleet.
The Raytheon 390 Premier I (Premier IA) occupies the light business jet niche, offering higher cruise speeds and a pressurized composite fuselage section compared with older entrants in its class; the twin Williams FJ44-2A engines deliver 2,300 lbf thrust each and enable a 41,000 ft ceiling and a 426 kt cruise. Competitors in the segment include other light-cabin jets offering similar range-performance tradeoffs; buyer and charter demand typically values low operating costs, speed, and an executive cabin layout like that aboard N330AC. Resale and maintenance considerations for this airframe hinge on engine program status, Pro Line 21 avionics condition, and the documented owner/operator history, elements reflected in the airframe’s assessed value of $1,938,691.
Aircraft Comparison
| Parameter | N330AC | N100HL | N100WE |
|---|---|---|---|
| Serial Number (MSN) | RB-173 | 258345 | RB-45 |
| Year Manufactured | 2007 | 1997 | 2002 |
| Duration of Flight | 3 Hours | 6 Hours | 3 Hours |
| Range | 1360 NM | 2470 NM | 1460 NM |
| Max Speed | 454 MPH | 447 MPH | 454 MPH |
| Aircraft Class | 12,500 - 19,999 lbs | 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. |