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For G1000 Equipped Aircraft Delivered in 2009 & 2010
NOTE: OPTIONAL EQUIPMENT AND VENDORS ARE SUBJECT TO CHANGE WITHOUT NOTICE.
AIRCRAFT PROFILE
STANDARD EQUIPMENT
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.
AVIONICS:
Standard Avionics Kit (includes Two
Headsets)
Garmin G1000 System includes:
GDU 1040A Pilot & Co-Pilot Primary Flight
Display (PFD)
GDU 1040A Multi Function Display (MFD)
GIA 63W Dual Com/Nav/GPS (WAAS)
GDC 74A Dual Air Data Computer (ADC)
GEA 71 Engine/Airframe Unit
GRS 77 Dual Attitude and Heading
Reference System (AHRS)
GFC 700 with GMC 710 Mode Controller,
Three Axis Automatic Flight Control
System (AFCS) with Integrated Pitch Trim
GMA 1347 Single Audio System with
Integrated Marker Beacon Receiver
GTX 33 Mode S Transponder, Non-
Diversity
Garmin Relative Terrain/Obstacles, Garmin
Flight Charts (No Geographic Aircraft
Overlay), Garmin SafeTaxi (Domestic
Only)
KN-63 DME
Switch, Avionics Power (Two) (On-Off)
Artex ME-406 2-Frequency (Non-Nav
Interfaced) ELT with Remote Switch and
Monitor Light (Dorsal Fin Installation)
Avionics Cooling, (2) cowl deck fans and
(3) display fans
PA System with Aft Cabin Speakers
ENGINE INDICATION SYSTEM (EIS)
Displayed on MFD During Normal
Operations:
Engine and System Displays - Show
numeric readouts of critical engine, fuel
and electrical indications and calcula-
tions for the following:
Torque
Interstage Turbine Temperature
Gas Generator Speed
Propeller Speed
Oil Pressure
Oil Temperature
Fuel Quantity
Fuel Flow
Ammeter/Voltmeter
Standby Engine Instrument:
Engine Torque Gauge, Wet Type
Altair Digital ADAS Engine Trend
Monitoring System
FLIGHT INSTRUMENTS:
Indications Displayed on each PFD:
Airspeed
Attitude with Slip/Skid Indication
Altitude
Vertical Deviation, Glideslope and Glidepath
Vertical Speed
Horizontal Situation Indication
Outside Air Temperature
System Time
Generic Timer
Wind Data
Standby Flight Instruments:
Airspeed Indicator
Attitude Gyro
Altimeter
Magnetic Compass
Heated Pitot System, Pilot & Co-Pilot
Alternate Static Source
Static Source Drains
Instrument Static System
Second Independent Pitot-Static System
FLIGHT CONTROLS:
Brake, Parking
Brakes, Hydraulic, Toe-Operated
Control Cables — Corrosion Resistant Steel