2002 Raytheon 390 Premier I
Description
The Raytheon 390 Premier I is a light jet aircraft that was manufactured by Raytheon Aircraft Company. It was introduced in 1997 and is powered by two Pratt & Whitney JT15D-4A turbofan engines. The aircraft has a maximum range of 1,800 nautical miles and can seat up to eight passengers. The aircraft features a stand-up cabin with a full galley, an enclosed forward lavatory, and an optional aft lavatory. It is equipped with an advanced avionics suite, including a four-screen Honeywell Primus 1000 system with color weather radar and enhanced ground proximity warning system. The aircraft also features a pressurized fuselage, allowing it to fly at altitudes of up to 41,000 feet.
Features
- Total Time Since New: 2,061.6
- Landings: 1,840
- ENGINES:
- Williams International FJ44-2A – TAP Blue – 5,000 TBO
- Engine #1
- TTSN 2,061.6
- Cycles 1,840
- SMPI N/A
- SCZI N/A
- Engine #2
- TTSN 2,061.6
- Cycles 1,840
- SMPI N/A
- SCZI N/A
- AVIONICS:
- Pro-Line 21
- Three Tube EFIS Display
- Dual FMS-3000 w/Data Base
- Dual GPS 4000A
- TCAS II
- Dual Collins VFH-422C
- Emergency Locator Transmitter
- FGC-3000
- Dual ADC-3000
- Dual AHRS
- WXR-800 Weather Radar Receiver/Transmitter
- ALT-4000
- Dual VIR-432 VHF Navigation Receivers
- DME-422
- ADF-462
- Dual TDR-94D Mode S Transponder
- Dual Avionics Master Switches
- Dual DCU-3000
- Satphone
- ADDITIONAL EQUIPMENT:
- Automatic Pressurization Controller
- 77 Cu. Ft. Oxygen System
- Refreshment/Hang Up Baggage Cabinet
- Cockpit Sliding Door
- Remote Control Entry Lighting
- Remote Low Engine Oil Sensor System
- 2 Personal Computer Power Outlets (110AC)
- Aft Baggage Heat
- Enclosed Window Shades
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