Garmin 675 manual A I R C R A F T P R O F I L E, S Ta N Da R D E Q U I P M E N T

For G1000 Equipped Aircraft Delivered in 2009 & 2010

A I R C R A F T P R O F I L E

AIRCRAFT CERTIFICATION AND OPERATIONAL APPROVAL

Aircraft Certification: If the Purchaser elects to meet the certification criteria other than those required for U.S. FAA FAR 23–Normal category (day, night, VFR, IFR), compliance may necessitate airframe modifications and additional sys- tems. Certification Kits are, or will be, available to meet the type design requirements set forth by the relevant civil authority, at an additional charge.

Aircraft Operating Approval: The Purchaser is responsible for obtaining Aircraft operating approval from the relevant civil aviation authority. Additional equipment or airframe modifications, dependent upon the location and planned operations, may be identified by that authority (various regions within one country may have differing requirements).

International Certification: The Purchaser must furnish to Cessna the country of Aircraft registration, a properly assigned or designated aircraft registration with the applicable Artex ELT and Mode S code identification, and any addi- tional equipment or systems (if different from those mandated by the FAA for a similar operational category) required for the category of registration intended (e.g., private, commercial).

The Purchaser is responsible for added Aircraft modifications and associated expense to comply with operational requirements. International Certification Kit information is available upon request.

AIRCRAFT EQUIPMENT REGISTRATION

The Purchaser must furnish to Cessna from the relevant civil aviation authority, the binary code and country protocol for operation of the Artex ELT and the binary Mode S Transponder.

S TA N DA R D E Q U I P M E N T

AVIONICS:	Monitor Light (Dorsal Fin Installation)	FLIGHT INSTRUMENTS:
Standard Avionics Kit (includes Two	Avionics Cooling, (2) cowl deck fans and	Indications Displayed on each PFD:
Headsets)	(3) display fans	Airspeed
Garmin G1000 System includes:	PA System with Aft Cabin Speakers	Attitude with Slip/Skid Indication
GDU 1040A Pilot & Co-Pilot Primary Flight		Altitude
Display (PFD)	ENGINE INDICATION SYSTEM (EIS)	Vertical Deviation, Glideslope and Glidepath
GDU 1040A Multi Function Display (MFD)	Displayed on MFD During Normal	Vertical Speed
GIA 63W Dual Com/Nav/GPS (WAAS)	Operations:	Horizontal Situation Indication
GDC 74A Dual Air Data Computer (ADC)	Engine and System Displays - Show	Outside Air Temperature
GEA 71 Engine/Airframe Unit	numeric readouts of critical engine, fuel	System Time
GRS 77 Dual Attitude and Heading	and electrical indications and calcula-	Generic Timer
Reference System (AHRS)	tions for the following:	Wind Data
GFC 700 with GMC 710 Mode Controller,	Torque	Standby Flight Instruments:
Three Axis Automatic Flight Control	Interstage Turbine Temperature	Airspeed Indicator
System (AFCS) with Integrated Pitch Trim	Gas Generator Speed	Attitude Gyro
GMA 1347 Single Audio System with	Propeller Speed	Altimeter
Integrated Marker Beacon Receiver	Oil Pressure	Magnetic Compass
GTX 33 Mode S Transponder, Non-	Oil Temperature	Heated Pitot System, Pilot & Co-Pilot
Diversity	Fuel Quantity	Alternate Static Source
Garmin Relative Terrain/Obstacles, Garmin	Fuel Flow	Static Source Drains
Flight Charts (No Geographic Aircraft	Ammeter/Voltmeter	Instrument Static System
Overlay), Garmin SafeTaxi (Domestic	Standby Engine Instrument:	Second Independent Pitot-Static System
Only)	Engine Torque Gauge, Wet Type
KN-63 DME	Altair Digital ADAS Engine Trend	FLIGHT CONTROLS:
Switch, Avionics Power (Two) (On-Off)	Monitoring System	Brake, Parking
Artex ME-406 2-Frequency (Non-Nav		Brakes, Hydraulic, Toe-Operated
Interfaced) ELT with Remote Switch and		Control Cables — Corrosion Resistant Steel

NOTE: OPTIONAL EQUIPMENT AND VENDORS ARE SUBJECT TO CHANGE WITHOUT NOTICE.

2