N414TE

Raytheon 390 Premier 1

Raytheon Aircraft Company

3 Hours

Duration of Flight

1350 NM

Range

451 MPH

Max Speed

N414TE

Gallery

Gallery item 1
Gallery item 2
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Aircraft Class
Aircraft Class
12,500 to 20,000lbs
Max passengers
Max passengers
8
Range
Range
1350 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
LocationGlastonbury, CT, US
Registration NumberN414TE
OwnershipDITEK CONSULTING LLC
Serial NumberRB-4

Airframe

Data valid as of 2023-06-09
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
2025-10-21N/AN/AN/A✓ Landed
2025-10-21N/AN/AN/A✓ Landed
2025-10-15N/AN/AN/A✓ Landed
2025-10-15N/AN/AN/A✓ Landed
2025-10-14N/AN/AN/A✓ Landed
2025-10-14N/AN/AN/A✓ Landed

AI Summary

Fact-checked by AI

Raytheon 390 Premier 1

Overview

Assigned. Registered to DITEK CONSULTING LLC (Glastonbury, CT). Certificate issued 2023-06-07; airworthiness date 2001-06-21; registration expiration 2030-06-30.

Specifications

  • Engines: 2× Williams FJ44-2A (2300 lbf each)
  • Range: 1350 nm
  • Cruise: 451 kts
  • Seats: 8
  • Ceiling: 41000 ft

Operations & Cabin

Typical 6-place executive club layout (forward club + two aft seats), small galley/refreshment center and aft lavatory 6–8 executive seats depending on configuration; forward refreshment center; baggage compartments in nose and external aft hold Avionics: Rockwell Collins Pro Line 21

Model & Market Context

The airframe bearing tail number N414TE is a 2001 Raytheon 390 Premier 1, serial RB-4, registered in the United States. The listed owner is DITEK CONSULTING LLC, an LLC based in Glastonbury, CT, US; ownership is recorded under that corporate entity in the U.S. registry. The airframe carries a US registration and is noted for its year-2001 build within the Raytheon Aircraft Company production run; no separate valuation or condition timeline is published in the supplied data.

This individual Premier 1 is outfitted in a typical six-place executive club cabin layout with a forward club and two aft seats, together accommodating a total seating complement of 8 when including cockpit positions. The cabin includes a small galley/refreshment center and an aft lavatory, supporting short- to medium-haul executive missions within its 1,350 nm range and high-speed cruise capability of 451 kts. Avionics are a Rockwell Collins Pro Line 21 suite, providing integrated flight management and systems common to modern light-cabin business jets; maintenance considerations for this airframe would focus on its twin Williams FJ44-2A turbofan engines and legacy Pro Line 21 avionics support. The owner/operator is based in Glastonbury, CT, US, suggesting primary operations and maintenance oversight from that locale.

The Raytheon 390 Premier 1, as represented by serial RB-4 and tail N414TE, occupies the light business jet niche with performance characterized by a high cruise speed and a 41,000 ft service ceiling, enabling rapid regional point-to-point transport. With twin Williams FJ44-2A engines delivering 2,300 lbf each, the model emphasizes a balance of speed, range and efficient twin-engine operation suited to owner-operators or charter operators. In the resale and maintenance market, aircraft of this configuration are evaluated on engine hours, Pro Line 21 avionics condition, and cabin refurbishment status—factors directly relevant to this specific airframe.

Aircraft Comparison

ParameterN414TEN100HLN100WE
Serial Number (MSN)RB-4258345RB-45
Year Manufactured200119972002
Duration of Flight3 Hours6 Hours3 Hours
Range1350 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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