CIRRUS AIRPLANE MAINTENANCE MANUAL MODEL SR22

NAVIGATION AND PITOT-STATIC SYSTEMS

1. GENERAL This chapter describes the navigation systems, units, and components which provide airplane navigational information. Included are pitot-static, gyros, compass, landing aids, global positioning system (GPS), and indicators. The subjects to be covered in this chapter are as follows: The Flight Environmental Data/Pitot Static Section describes systems which sense environmental condi- tions and use the data to influence navigation of the airplane. This includes components that depend on the pitot-static system such as vertical speed indicator, airspeed indicator, and altimeter. (Refer to 34-10) The Attitude and Direction Section describes systems which use magnetic, gyroscopic and inertia forces. This includes gyros, magnetic compass, and turn coordinator. (Refer to 34-20) The Landing and Taxiing Aids Section describes systems which provide guidance during approach, land- ing, and taxiing. This includes components such as the glideslope and marker beacon systems. (Refer to 34-30) The Independent Position Determining Section describes systems which provide information to determine position from sources which are mainly independent of ground installations. This includes the optional Stormscope, SkyWatch, Terrain Awareness and Warning System (TAWS), and XM Weather systems. (Refer to 34-40) The Dependent Position Determining Section describes systems which provide information to determine position from sources which are mainly dependent on ground installations. This includes the global posi- tioning system (GPS), horizontal situation indicator, transponder, and radio navigational aids. (Refer to 34- 50) Navigational system instrument layout: (See Figure 34-001) Pitot-Static system schematic: (See Figure 34-002)

Note: This chapter does not address specific instrument repair. Federal Aviation Regulations require malfunctioning instruments be sent to an approved instrument overhaul and repair station or returned to the manufacturer for servicing.

EFFECTIVITY: All 34-00 Page 1 15 Apr 2007 CIRRUS AIRPLANE MAINTENANCE MANUAL MODEL SR22

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4 5 2 1 6 7

FASTEN SEATBELTS FIRE EXTINGUISHER UNDER PILOT SEAT FRONT INC NO SMOKING ENT DTA ALTITUDE GPH ALT DH VS BAR PULL 16000 17 TENTHS

ALT ALR DH VS MAN 12000 18 8000 21 4000 24 SL 27 MAX POWER FUEL FLOWS

0 9 1 20 20 8 10 10 2 160 AMMETER 10 10 SELECT 20 20 7 ALTIMETER 3 ALT 1 ALT 2 6 4 BATT 5

SANDEL SN3308 157KT A 311° 57.9 nm MAP OFF I 314° 311° N 3 V L 30 33 A 6 U S V W N 0 E 10 1 15 M 5 A 24 3 VERTICAL P 0 20 B 21 6 R G SPEED L R E E GPS1 5 15 12 15 NA V 10 284°

SHFT SYNC A-B 302°

13 14 12 8 9 10 11

Serials 0002 thru 0434, 0435 thru 0820 w/o PFD.

LEGEND 1. Airspeed Indicator (34-10) 8. VOR/LOC (34-50) 2. Attitude Indicator (34-20) 9. Turn Coordinator (34-20) 3. Magnetic Compass (34-20) 10. HSI (34-50) 4. Altitude Selector\Alerter (22-11) 11. Vertical Speed Indicator (34-10) 5. Altimeter (34-10) 12. Transponder (34-50) 6. Multifunction Display (34-60) 13. System 55X Autopilot (22-11) 7. Audio Panel w/ Marker Beacon (34-30) 14. GPS/COM/NAV Receiver (34-40)

SR22_MM34_1395D

Figure 34-001 Navigation and Pitot-Static System - Serials 0002 thru 0434, 0435 thru 0820 w/o PFD (Sheet 1 of 3) EFFECTIVITY: 34-00 Serials 0002 thru 0434, 0435 thru 0820 w/o PFD Page 2 15 Apr 2007 CIRRUS AIRPLANE MAINTENANCE MANUAL MODEL SR22

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15 6 7

FASTEN SEATBELTS FIRE EXTINGUISHER UNDER PILOT SEAT FRONT NO SMOKING ALTITUDE GPH 16000 17 12000 18 8000 21 4000 24 SL 27 MAX POWER FUEL FLOWS

AMMETER SELECT

ALT 1 ALT 2 BATT

L BO R TH S F T F A O R T

ACS

L R

14 9 1 2 5 13 12

Serials 0435 thru 0820 w/ PFD, 0821 thru 1601, 1603 thru 1643, 1645 thru 1662.

LEGEND 1. Airspeed Indicator (34-10) 9. Turn Coordinator (mounted behind RH bolster) 2. Attitude Indicator (34-20) 12. Transponder (34-50) 3. Magnetic Compass (34-20) 13. System 55X Autopilot (22-11) 5. Altimeter (34-10) 14. GPS/COM/NAV Receiver (34-40) 6. Multifunction Display (34-60) 15. Primary Flight Display (34-60) 7. Audio Panel w/ Marker Beacon (34-30)

SR22_MM34_1620B

Figure 34-001 Navigation And Pitot-Static System - Serials 0435 - 0820 w/ PFD, 0821 thru 1662 (Sheet 2 of 3) EFFECTIVITY: Serials 0435 - 0820 w/ PFD, 0821 thru 1662 34-00 Page 3 15 Apr 2007 CIRRUS AIRPLANE MAINTENANCE MANUAL MODEL SR22

3

15 6 7

L BO R TH

F F O

ACS

L R

14 9 1 2 5 13 12

Serials 1602, 1644, 1663 & subs.

LEGEND 1. Airspeed Indicator (34-10) 9. Turn Coordinator (mounted behind RH bolster) 2. Attitude Indicator (34-20) 12. Transponder (34-50) 3. Magnetic Compass (34-20) 13. System 55X Autopilot (22-11) 5. Altimeter (34-10) 14. GPS/COM/NAV Receiver (34-40) 6. Multifunction Display (34-60) 15. Primary Flight Display (34-60) 7. Audio Panel w/ Marker Beacon (34-30)

SR22_MM34_2198A

Figure 34-001 Navigation And Pitot-Static System - Serials 1663 & subs (Sheet 3 of 3) EFFECTIVITY: 34-00 Serials 1663 & subs Page 4 15 Apr 2007 CIRRUS AIRPLANE MAINTENANCE MANUAL MODEL SR22

Serials 0435 thru 0820 w/ PFD, Serials 0002 thru 0434, 0821 & subs. 0435 thru 0820 w/o PFD.

PRIMARY FLIGHT DISPLAY

AIRSPEED VERTICAL SPEED INDICATOR INDICATOR ALTIMETER

ALTITUDE ENCODER

ALTITUDE TRANSDUCER ALTERNATE (OPTIONAL) STATIC AIR SOURCE

PITOT-STATIC WATER TRAPS

PITOT MAST STATIC BUTTONS

SR22_MM34_1838B

Figure 34-002 Pitot-Static System Schematic EFFECTIVITY: All 34-00 Page 5 15 Apr 2007 CIRRUS AIRPLANE MAINTENANCE MANUAL MODEL SR22

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EFFECTIVITY: 34-00 All Page 6 15 Apr 2007