N679SJ

Raytheon (Beechcraft) 400A Beechjet (400A)

Raytheon Aircraft Company

4 Hours

Duration of Flight

1693 NM

Range

468 MPH

Max Speed

N679SJ

Gallery

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Aircraft Class
Aircraft Class
12,500 to 20,000lbs
Max passengers
Max passengers
10
Range
Range
1693 NM
Service Ceiling
Service Ceiling
45000 ft
Duration of Flight
Duration of Flight
4 Hours
Max Speed
Max Speed
468 MPH

Basic Information

Year Manufactured1997
LocationRantoul, KS, US
Registration NumberN679SJ
OwnershipDodson International Parts Inc
Serial NumberRK-168

Airframe

Data valid as of 2023-09-09
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
No flights

No flight history available

Flight records for this aircraft have not been tracked yet.

AI Summary

Fact-checked by AI

Raytheon (Beechcraft) 400A Beechjet (400A)

Overview

US-registered Beechjet 400A, MSN RK-168; certificate issue 2016-10-07; airworthiness date 1997-11-19; last FAA action recorded 2023-09-09, expiry 2029-10-31.

Specifications

  • Engines: 2× Pratt & Whitney Canada JT15D-5 (2900 lbf each)
  • Range: 1693 nm
  • Cruise: 443 kts
  • Seats: 10
  • Ceiling: 45000 ft

Operations & Cabin

Executive 7–10 place club/forward‑facing layout with enclosed aft lavatory (typical 400A fit) Enclosed lavatory, executive seating (7–10 pax), in‑flight entertainment and refreshed interiors vary by operator Avionics: Rockwell Collins Pro Line 4 (typical for 400/400A retrofits)

Model & Market Context

This entry covers airframe N679SJ, a 1997 Raytheon (Beechcraft) 400A Beechjet built by Raytheon Aircraft Company with serial number RK-168. The aircraft is registered in the US and is recorded as owned by the corporation Dodson International Parts Inc, based in Rantoul, KS, US. Ownership is held by a parts-focused corporate operator, and the airframe is appraised at $1,600,000, reflecting its age and typical equipment fit for the 400A variant.

The cabin configuration for this specific 400A-example follows the typical executive layout: an enclosed aft lavatory and a 7–10 place club/forward‑facing seating arrangement, which on this airframe is listed as an executive 7–10 place club/forward‑facing layout with enclosed aft lavatory (typical 400A fit). Avionics are recorded as the common retrofit fit, Rockwell Collins Pro Line 4 (typical for 400/400A retrofits), supporting modern navigation and flight management capabilities for the type. Operated from a corporate base in Rantoul, KS, US, the aircraft’s systems and cabin are consistent with light executive transport and parts-support roles noted by the owner’s corporate profile. Maintenance and mission planning for this airframe would align with its twin JT15D-5 engines and high‑altitude capability.

This airframe is a member of the Raytheon (Beechcraft) 400A Beechjet lineage, characterized here by a combination of twin JT15D engines, a 45,000 ft service ceiling and a longish range of 1,693 nm, positioning the model for high-speed, mid-range executive missions. The documented cruise speed of 443 kts and seating for 10 reflect the aircraft’s performance niche as a fast, small executive transport. Typical market considerations for this specific 1997 airframe include avionics retrofit status (Rockwell Collins Pro Line 4), the condition implied by its assessed value ($1,600,000), and ongoing maintenance demands associated with its engines and airframe age.

Aircraft Comparison

ParameterN679SJN100HLN100WE
Serial Number (MSN)RK-168258345RB-45
Year Manufactured199719972002
Duration of Flight4 Hours6 Hours3 Hours
Range1693 NM2470 NM1460 NM
Max Speed468 MPH447 MPH454 MPH
Aircraft Class12,500 to 20,000lbsOver 20,000lbs12,500-19,999lbs
Service Ceiling45000 ft41000 ft41000 ft
Max Passengers1088
Cabin ComfortNo items found.No items found.No items found.

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