Aircraft for Sale:
1998 Beechjet 400A – RK-197
This low-time, Beechjet 400A was built in 1998, is US-registered and FAR 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.
| 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 |
Configuration
| 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 135 Compliant | — |
| TCAS | Yes |
| TAWS | Yes |
Operating Weight
| 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 |
Avionics
| Nomenclature | Manufacturer | Model | Qty |
|---|---|---|---|
| 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 |
Summary
Additional Photos
