Citation M2

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)

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.

Overall Base White with a Standard Stripe Scheme