1997 Beechcraft Beechjet 400A
Description
The Beechcraft Beechjet 400A is a light business jet produced by Beechcraft, a subsidiary of the Raytheon Company. It was introduced in 1992, and it is the first light business jet with a composite airframe. The aircraft is powered by two turbofan engines, and it has a range of 1,875 nautical miles, a maximum speed of 461 knots, and a service ceiling of 43,000 feet. It is equipped with a Collins Pro Line 21 avionics suite and has a seating capacity of up to nine passengers. The aircraft is commonly used for corporate, charter, and private transportation.
Features
- Year of Delivery: 1997
- Airframe Total Hours: 9,862
- Airframe Total Cycles: 9,173
- Engine(s)
- Manufacturer: Pratt & Whitney
- Type: JT15D-5
- Engine 1 Total Time: 9,118
- Engine 1 Total Cycles: 8,493
- Engine 2 Total Time: 9,145
- Engine 2 Total Cycles: 8,456
- Avionics
- Avionics Package: Collins FCS-850 3-tube/Pro Line 4
- ADF: Collins ADF-462
- Autopilot: Collins APS-4000
- Comm Radios: Dual Collins VHF-422A
- CVR: Fairchild A100S
- FDR: Flight Data Recorder
- DME: Dual Collins DME-442
- EFIS: Collins FCS-850 3-tube
- Flight Director: Collins FCS-850 3-tube EFIS
- FMS: Dual Collins FMS-5000 w/GPS-4000
- Nav Radios: Dual Collins VIR-432
- Radar Altimeter: Collins ALT-55B
- RMI: Dual Collins SDU-640B
- Transponder: Dual Collins TDR-94B
- Weather Radar: Collins RTA 4-color
- Features/Options
- Artex C-406-1 ELT
- Dual DB-438 audio panels
- ADS-B Out
- TCAS II 7.1
- Thrust Reversers
- Gross Weight increase mod
- Logo Lights
Location
