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Price
Make OfferRegistration
N8608Serial Number
680-0584Airframe
894 hours since new
562 landings since new
Engines
Two (2) Pratt & Whitney PW545C
Engine #1: 894 hours since new / 562 cycles
Engine #2: 894 hours since new / 562 cycles
Engine Program: Enrolled on PowerAdvantage
APU: Honeywell RE100(XL) / 740.6 hours since new
APU Program: Enrolled on AuxAdvantage
Maintenance
DOC 1 (12 months) last cw. 4/2/2024 next due 3/31/2025
DOC 3 (24 months) last cw. 5/5/2023 next due 3/31/2025
DOC 5 (36 months) last cw. 3/19/2022 next due 3/31/2025
DOC 6 (48 months) last cw. 5/5/2023 next due 3/31/2027
Additional Options
GoGo Avance L5
Dual HF Radios
FANS 1/A CPDLC
FDR
XM Weather
Extended Refreshment Center
CABIN CONFIGURATION
INTERIOR
The Eight (8) passenger interior is configured as follows:
Forward cabin: A right-hand extended refreshment center with ice chest, numerous flexible storage areas, trash container, and provisions to store catering. A left-hand closet, forward of the cabin entry door, provides storage for the navigation charts, flight manual, and general storage.
Main Cabin: Eight (8) pedestal-mounted passenger seats with adjustable headrests that can track forward/aft, laterally, and swivel 360 degrees. Four (4) fold out tables with ample work area is included. There are five (5) individual 110 VAC outlets throughout the aircraft. The refreshment center also has its own high-powered outlet.
Includes an AFT Lavatory
AVIONICS
- Avionics: Garmin G5000 Avionics Suite
- Flight Displays: Four Garmin G5000 14 diagonal inch, widescreen-format Liquid Crystal Displays
- Synthetic Vision Technology: Garmin Synthetic Vision Technology (SVT) presents terrain & obstacle information on the PFDs in a dynamic, three-dimensional format.
- Touchscreen Control Panels: Four full-color, touchscreen LCD control panels provide the primary user interface with the G5000 system
- Automatic Flight Control System: Garmin G5000 full-featured Automatic Flight Control System (AFCS) that is integrated with the autothrottle system and includes an Emergency Descent Mode
- Attitude/Heading Reference System: Dual Litef LCR-100 gyrocompassing Attitude Heading Reference System
- Integrated Avionics Units: Dual Integrated Avionics Units include Global Positioning System (GPS) receivers, Wide Area Augmentation System (WAAS) receivers, Very High Frequency (VHF) communication radios, VHF navigation radios, and glide slope receivers.
- Flight Management Systems: Dual Flight Management Systems (FMS) provides extensive navigation and flight planning capabilities as well as enroute, terminal and precision and non-precision approach capabilities (including LNAV/VNAV and Localizer Performance with Vertical Guidance (LPV) approaches)
- Weather Radar: A Garmin GWX 70 weather radar system with a 12-inch antenna
- Traffic Alert and Collision Avoidance System: Garmin TCAS II system and Change 7.1 compliant
- Terrain Awareness Warning System: Garmin G5000 system includes Class A TAWS
- Transponders: Dual Mode S Diversity transponders w/ Enhanced Surveillance and ADS-B Out
- Standby Instrumentation: An Electronic Standby Flight Display (ESFD) provides standby airspeed, attitude, heading, altitude, and VOR/ILS navigation information
- Radio Altimeter: Single Radio Altimeter is included with display on the PFD and in support of TCAS II and TAWS A
- Cockpit Voice Recorder: Yes
- Emergency Locator Transmitter: Artex 406-N ELT w/ navigation interface
- Maintenance Diagnostic System: Yes. Includes the capability to record specific maintenance diagnostic information
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