2002 Beechcraft Premier I
Description
The Beechcraft Premier I is a light business jet manufactured by Beechcraft. It was introduced in 2001, and production ended in 2012. It features a cantilever low-wing, a swept wing, and a retractable tricycle landing gear. The aircraft is powered by two Pratt & Whitney Canada PW535 turbofan engines, which produce a maximum thrust of 2,400 lbf each. It has a maximum speed of 455 knots and a range of 1,800 nautical miles. The cabin is capable of seating up to seven passengers and features a full galley and lavatory.
Features
- Total Airframe Time: 3,282 Hours
- Total Airframe Cycles: 2,781
- Engine(s)
- Engine Model: Williams FJ44-2A
- Engine Program: TAP Elite
- Engine Serial Numbers: 1: 1055/ 2: 1085
- Total Time Since New (hrs): 1: 3,282/ 2: 3,220
- Avionics
- CASP
- FGC 3000 Autopilot/FD
- FMC 3000 FMS
- Dual VHF-422A Comm
- Dual VIR-432 Nav
- RTA-800 Radar
- ALT-4000 Radio Altimeter
- ADF-462 ADF
- DME-442 DME
- TCAS-4000/TCAS II
- Dual AHC-3000 AHRS
- Collins ADC-3000 ADC
- Dual Collins CDU-3000
- Dual Collins AFD-3010 PFD
- Collins AFD-3010E MFD
- MDC-3000 MDC
- Collins IFIS 5000
- Collins 3 Tube EFIS 8x10 Displays
- Collins TTR-4000 TCAS II
- Garmin GA36 GPS
- Dual Garmin GTX3000 Transponder (ADS-B In/Out)
- L3 FA2100 CVR
- Collins SM GWX-3001
- Maintenance Status
- Inspection: Interval: Remaining
- A: 600 Hours: 452 Hours
- B: 1200 Hours: 265 Hours
- Features/Options
- 2 110V AC Personal Computer Power Outlets
- Premier 1A Hydraulic Brake Upgrade
- Aft Baggage Heat
Location
