This low-time, Beechjet 400A was built in 1998, is US-registered and FAA Part 135 maintained.
It has freshly overhauled engines and up-to-date maintenance inspections. The interior includes an executive seating layout and a belted aft lavatory for a total of 8 seats. The interior has been completely refurbished in October 2017 with a custom design, new materials, metal accent plating, lighting, and more. The wood has also been replaced with new veneer and hardwood and features a durable, high-gloss finish.
The exterior was stripped and repainted in a custom design in October 2017.
This stunning aircraft is ready to impress any owner and will be in high demand by charter customers.
ALL SPECIFICATIONS AND REPRESENTATIONS OF AIRCRAFT SUBJECT TO VERIFICATION BY BUYER
| Summary | |
|---|---|
| Serial Number: | RK-197 |
| Build Date: | 1998 |
| Total Time: | 4,403.0 |
| Total Cycles: | 3998 |
| Seats: | 8 |
| Avionics: | Collins |
| Registration: | N940VA |
| Registration Country: | USA |
Engine Details
| #1 Position | Serial/Value |
|---|---|
| JT15D-5 Engine | PCE–JA-0162 |
| Total Time | 3,677.3 |
| Total Cycles | 3,510 |
| Time Since Overhaul | 39.1 |
| Cycles Since Overhaul | 25 |
| #2 Position | Serial/Value |
|---|---|
| JT15D-5 Engine | PCE-JA-0161 |
| Total Time | 3,677.3 |
| Total Cycles | 3,510 |
| Time Since Overhaul | 39.1 |
| Cycles Since Overhaul | 25 |
Landing Gear Details
| L/H Main | CSO | Cycles Remaining |
|---|---|---|
| Shock Strut | 3,876 | 1,124 |
| Side Strut | 3,876 | 1,124 |
| R/H Main | CSO | Cycles Remaining |
|---|---|---|
| Shock Strut | 3,876 | 1,124 |
| Side Strut | 3,876 | 1,124 |
| Nose | CSO | Cycles Remaining |
|---|---|---|
| Shock Strut | 3,876 | 1,124 |
| Drag Brace | 3,876 | 1,124 |
Inspections
| Hourly | Last Performed | Cycles Remaining |
|---|---|---|
| Complete A (200 HR) | June 28, 2017 | 160.9 |
| Complete B (400 HR) | February 23, 2017 | 187.5 |
| Complete C (1200 HR) | February 23, 2017 | 987.5 |
| Complete D (2400 HR) | June 28, 1998 | 597 |
| Item | Value |
|---|---|
| Number and Location of Galley | 1 FWD |
| Number and Location of Lavatory | 1 AFT |
| Number of Crew Seats | 2 Cockpit |
| Aircraft Painting Scheme | Matterhorn White, Platinum/Phantom Gray Stripes |
| FAR 121 Compliant | — |
| TCAS | Yes |
| TAWS | Yes |
| ETOPS | — |
| FAR Part 36, Stage III Noise Compliant | — |
| Item | Value |
|---|---|
| Maximum Take-Off Weight | 16,100 lbs |
| Maximum Landing Weight | 15,700 lbs |
| Maximum Zero Fuel Weight | 13,000 lbs |
| Operating Empty Weight | 10,585 lbs |
| Fuel Capacity | 4,912 lbs |
| Nomenclature | Manufacturer | Model | Qty |
|---|---|---|---|
| ACARS | Not Installed | Not Installed | 0 |
| Autopilot w/Yaw Damper | Collins | APS 850 | 1 |
| VHF Comm. | Collins | VHF-422A | 2 |
| VOR/ILS | Collins | VIR-432 | 2 |
| DME | Collins | DME-422 | 2 |
| TCAS Computer | Collins | TTR-920 | 1 |
| ADF | Collins | ADF-462 | 1 |
| FMS W/4000A GPS | Collins | FMS-5000 | 2 |
| 3-Tube EFIS | Collins | 3-Tube EFIS | 1 |
| Radar | Collins | RTA-854 | 1 |
| HF | Collins | — | 1 |
| Radio Altimeter | Collins | ALT 55B | 1 |
| ATC (Mode S) | Collins | TDR-94D | 2 |
| CVR | Fairchild | A 105S | 1 |
| RMI | Collins | SDU-640B | 1 |
| TAWS | Allied Signal | — | 1 |
ALL SPECIFICATIONS AND REPRESENTATIONS OF AIRCRAFT SUBJECT TO VERIFICATION BY BUYER
