Airplane Flight Manual (AFM) Temporary Change Information in this Temporary Change adds to, supersedes, or deletes information in the basic Pilot s Operating Handbook. Affected Publications: Filing Instructions: Purpose: Basic Airplane Flight Manual: PN 13772-00 Original Issue (FAA Approved) PN 13772-00AR Original Issue (FAA Approved on behalf of ANAC-DA of Argentina) PN 13772-00E Original Issue (FAA Approved on behalf of the European Aviation Safety Agency (EASA)) PN 2100-00 Original Issue (FAA Approved on behalf of ANAC of Brazil) Insert the following revised pages and retain until further notice. Remove and discard the superseded pages. Insert this cover page adjacent to the last page of the List of Effective Pages and retain until further notice. This POH Temporary Change revises the illustrations for Instrument Panel and Console, and Equipment Locations. Affected Sections: Section 7 - Airplane and Systems Description - Pages 7-15 and 7-1 - Pages 7-93 and 7-9 17-08 1 of 2
Intentionally Left Blank 2 of 2 17-08
USB POWER 5 VDC, 2.1 AMPS MAX PER PORT AUDIO INPUT 1 21 2 20 19 18 17 1 15 1 13 3 5 7 8 9 10 11 12 Legend 1. Cirrus Airframe Parachute System 13. Engine & Fuel System Controls (CAPS) Activation T-Handle Cover 1. Left Side Console 2. Magnetic Compass Circuit Breaker Panel 3. Multifunction Display ELT Remote Switch. Fresh Air Eyeball Outlet Alternate Static Source 5. Temperature/Ventilation Controls 15. Avionics Panel. Control Yoke 1. Parking Brake 7. ADF (opt) 17. Flight Instrument Panel 8. Conditioned Air Outlet 18. Bolster Switch Panel 9. Rudder Pedals 19. Start/Ignition Key Switch 10. Flap Control & Position Indicators 20. Primary Flight Display 11. Armrest 21. Overhead Light & Switch 12. Passenger Audio & USB Jack(s) _FM07_53A Figure 7- Instrument Panel and Console - Serials w/o MD302 (1 of 2) 17-08 7-15
USB POWER 5 VDC, 2.1 AMPS MAX PER PORT AUDIO INPUT 1 21 2 20 19 18 17 1 15 1 13 3 5 7 8 9 10 11 12 Legend 1. Cirrus Airframe Parachute System 13. Engine & Fuel System Controls (CAPS) Activation T-Handle Cover 1. Left Side Console 2. Magnetic Compass Circuit Breaker Panel 3. Multifunction Display ELT Remote Switch. Fresh Air Eyeball Outlet Alternate Static Source 5. Temperature/Ventilation Controls 15. Avionics Panel. Control Yoke 1. Parking Brake 7. ADF (opt) 17. Flight Instrument Panel 8. Conditioned Air Outlet 18. Bolster Switch Panel 9. Rudder Pedals 19. Start/Ignition Key Switch 10. Flap Control & Position Indicators 20. Primary Flight Display 11. Armrest 21. Overhead Light & Switch 12. Passenger Audio & USB Jack(s) _FM07_535A Figure 7- Instrument Panel and Console - Serials w/ MD302 (2 of 2) 7-1 17-08
3 2 1 31 30 29 28 25 27 2 25 2 23 22 21 5 7 8 9 10 11 12 13 1 15 1 17 18 19 20 LEGEND 1. GSU 75 ADAHRS 1 2. Integrated Avionics Unit 1 3. GSU 75 ADAHRS 2. Avionics Cooling Fan 5. Integrated Avionics Unit 2. Engine Airframe Unit 7. ADF (opt) 8. GMC 707 Mode Controller 9. CAPS Activation Handle (Cabin Ceiling) 10. Hour Meters 11. Egress Hammer 12. Passenger Audio & USB Jacks 13. Cabin Speaker 1. Roll Servo 15. Convenience System Controller 1. Pitch Trim Adapter (opt) 17. Pitch Servo 18. XM Radio Transceiver 19. Transponder 20. XM Satellite Data Link Receiver (opt) 21. ELT 22. Yaw Servo (opt) 23. Battery 2 2. Iridium Global Satellite Datalink (opt) 25. Tiedown Loops 2. CAPS Parachute 27. Stormscope WX-500 (opt) 28. Microphone 29. TAS Receiver (opt) 30. DME (opt) 31. Fire Extinguisher _FM07_5390A Figure 7-20 Equipment Locations 17-08 7-93
Avionics Support Equipment Antennas Two rod-type COM antennas are mounted to the airplane s exterior; COM 1 is mounted directly above the passenger compartment, COM 2 is mounted directly below the baggage compartment. These antennas are connected to the two VHF communication transceivers contained in the Integrated Avionics Units. The optional blade-type DME antenna is mounted on the airplane underside just aft, right of the firewall. A sled-type marker beacon antenna is mounted below the baggage compartment floor and provides a signal to the marker beacon receiver located in the audio panel. If the optional air conditioning system is installed this antenna is located below the baggage floor inside of the airplane. The transponder antenna is located on the bottom side of the airplane, just aft of the baggage compartment bulkhead on the RH side of the airplane. GPS 1 antenna is mounted directly above the passenger compartment. If the optional XM system is installed, a combination GPS 1/ XM antenna is installed in this location. A combination GPS 2 / Iridium antenna is mounted just forward of the baggage compartment window. These antennas are connected to the two GPS receivers contained in the Integrated Avionics Units. The optional Traffic System antenna is mounted just above the pilot/ copilot compartment. If the GTS 800 Traffic Advisory System is installed, a second bladetype antenna is located on the bottom RH side of the airplane just forward of the baggage compartment. The optional Lightning Detection antenna is mounted directly above the passenger compartment. The Navigation antenna is mounted to the top of the vertical fin. This antenna provides VOR and glidescope signals to the VHF navigation receivers contained in the Integrated Avionics Units. Headset and Microphone Installation The airplane is equipped with provisions for five Active Noise Reduction (ANR) and three conventional (MIC/HEADPHONES) 7-9 17-08