| Overview | |
| Listing Status: | Inactive |
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US Based Polar Interior Scheme Synthetic Vision Technology Avance L3 Max Extended Baggage |
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| Price: | N/A |
| Offered By: | Guardian Jet LLC |
| Registration: | N527M |
| S/N: | 525-1107 |
| Location: |
Guilford, Connecticut United States
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| Airframe | |
| Total Time: | 84 Hours |
| Landing Cycles: | 65 |
| Avionics | |
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Garmin 3000 Electronic Flight Instrument System (EFIS) with three 14.1 Garmin GDU 1400W touchscreen displays. Primary Flight Display (PFD) Multi-Function Display (MFD) – Primary shows moving map and engine data. Secondary Controller – GCU 275, controls PFD for map panning, ranging and other flight planning functions. Engine Indicating (EIS) and Crew Alerting System (CAS) Air Data and Attitude information – from pitot-static system with two electrically heated pitot and static sources. Dual VHF Communications Transceivers: 16 watts of transmission power, tuned with GTC 570 Remote Audio Processor: Dual GMA 36 Remote Audio Processors Navigation: Dual Garmin navigation receivers Global Positioning System (GPS): Interface Adapter Unit includes a WAAS capable GPS receiver Capable of monitoring 12 channels Flight Management System (FMS): Two GTC 570 with 5.7 inch display. Meets the operational requirements of oceanic/remote, NAT MNPS, RNP10 and RNP5/BRNAV Automatic Flight Control System (AFCS) or Autopilot: Garmin GFC 700 with Garmin Mode Controller GMC 710 Transponders with ADS-B Out Capability: Dual Mode S transponders with Automatic Dependent Surveillance - Broadcast Out (ADS-B Out) transmission capability in accordance with FAA TSO-166B Weather Radar: Garmin GWX 70 solid state radar with 40 watts transmit power and Altitude Compensated Tilt (ACT). Chart View: Approach, SID, STAR charts and airport diagrams provided on displays. DME: Collins DME-4000 (non Garmin component) Radio Altimeter: Collins ALT-4000 (from 2,500 feet to touchdown). Traffic Collision Avoidance System (TCAS I): Garmin GTS 855 Terrain Avoidance Warning System (TAWS): Garmin Terrain Avoidance Warning System Class B TAWS Avionics Dispatch Switch: Allows for limited use of the avionics system without excessive battery drain. Electronic Standby Instrument: L-3 Communications ESI-1000 Trilogy solid-state 3.7 inch LCD display located above pilot's PFD. Emergency Locator Transmitter (ELT): Artex C406-N with 121.5 and 243.0 MHz and the satellite frequency of 406 MHz, interfaces with the GIA. Remote control switch panel on the right hand tilt panel. ELT has a six year lithium battery pack. Maintenance Diagnostics system: allows for easier troubleshooting of the aircraft. Data is stored for the last 25+ flight hours on the aircraft. Uses Cessna Aircraft Recording System (AreS). |
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| Engines | |
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ENGINES: (2) FJ44-1AP-21 ENGINE CYCLES: 65 / 65 |
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| Engine 1 Hours: | 84 SNEW |
| Engine 2 Hours: | 84 SNEW |
| Interior & Exterior | |
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The Citation M2 cabin is configured with a single side facing seat opposite the entry, followed by a 4-place club set aft belted lavatory as standard. |
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| Overall Base White with a Standard Stripe Scheme | |
| Other Info | |
| Brochure: | View Brochure |