Pilot’s Operating Handbook and FAA Approved …

1 Cirrus DesignSection 9SR22 / SR22 TSupplementsP/N 13772-1351 of 32 Pilot s Operating Handbook andFAA Approved Airplane flight ManualSupplementfor theGFC 700 Automatic flight Control System(Aircraft Serials w/ Perspective Avionics Only)Including optionally installed Electronic Stability and Protection(ESP), Underspeed Protection (USP), and Hypoxia Detection andAutomatic Descent the GFC 700 Automatic flight Control System is installed on theaircraft, this POH supplement is applicable and must be inserted inthe Supplements Section of the basic Pilot s Operating document must be carried in the airplane at all times. Informationin this supplement adds to, supersedes, or deletes information in thebasic Pilot s Operating Handbook . Note This POH supplement Change, dated Revision 04: 09-08-14,supersedes and replaces the Revision 03 release of this POHS upplement dated 04: 09-08-142 of 32P/N 13772-135 Section 9 Cirrus DesignSupplementsSR22 / SR22 TSection 1 - GeneralThe aircraft is equipped with a Garmin GFC 700 Automatic FlightControl System (AFCS) which is fully integrated within the CirrusPerspective Integrated Avionics System architecture.

2 Refer to Section7 - System Description and the Cirrus Perspective Pilot s Guide foradditional description of the AFCS and Operating status of Autopilot Underspeed Protection (USP)and Hypoxia Detection and Automatic DescentIf Perspective System software load 0764-09 or later is installed, theaircraft has these functions installed. Software load is displayed in theupper RH corner of the first MFD screen presented after status of Electronic Stability and Protection (ESP)If the aircraft is equipped with ESP (software load 0764-09 or later), itis identified and displayed on the second MFD splash screenpresented after power-up. This page will state This aircraft isequipped with Electronic Stability & Protection if load 0764-20 or later also supports Discrete-Triggered LowSpeed 2 - Limitations1.

3 The appropriate revision of the Cirrus Perspective CockpitReference Guide (p/n 190-00821-XX, where X can be any digitfrom 0 to 9) must be immediately available to the pilot during system software version stated in the reference guide must beappropriate for the system software version displayed on Minimum Autopilot Speed ..80 KIAS3. Maximum Autopilot Speed ..185 KIAS4. Autopilot Minimum-Use-Height:a. Takeoff and Climb .. 400 feet AGLb. Enroute and Descent .. 1000 feet AGLc. Approach (GP or GS Mode) .. Higher of 200 feet AGL or Approach MDA, DA, Approach (IAS, VS, PIT or ALT Mode)..Higher of 400 feetAGL or Approach Yaw Damper must be turned off for takeoff and 04: 09-08-14 Cirrus DesignSection 9SR22 / SR22 TSupplementsP/N 13772-1353 of 326. The Autopilot may not be engaged beyond the EngagementLimits.

4 If the Autopilot is engaged beyond the command limits (upto engagement limits), it will be rolled or pitched to within thecommand limits and an altitude loss of 1000 feet or more can beexpected while attitude is established in the selected The Autopilot and flight Director will not command pitch or rollbeyond the Command Use of VNAV is not supported during an approach with a teardropcourse reversal. VNAV will be disabled at the beginning of For aircraft with optional USP or optional Discrete-Triggered LowSpeed ESP, if Stall Warning is inoperative, Autopilot UnderspeedProtection will not be provided in Altitude Critical Modes (ALT, GS,GP, TO and GA), and Low Speed ESP will not be Engagement LimitPitch 30 Roll 75 AxisAutopilot Command Limit FD Pitch Command Limits+20 , -15 FD Roll Command Limits 25 Revision 04: 09-08-144 of 32P/N 13772-135 Section 9 Cirrus DesignSupplementsSR22 / SR22 TSection 3 - Emergency ProceduresAutopilot MalfunctionRefer to Electric Trim/Autopilot Failure abnormal procedure in thebasic POH.

5 Do not reengage the Autopilot until the malfunction hasbeen identified and corrected. The Autopilot may be disconnected by:1. Pressing the A/P DISC on the control yoke., or2. Pulling the AP SERVOS circuit breaker on MAIN BUS lost during a roll or pitch axis Autopilot malfunction andrecovery: flight PhaseBank AngleAltitude LossClimb45 300 ftCruise45 300 ftManeuvering45 300 ftDescent45 300 ftApproach45 70 ftRevision 04: 09-08-14 Cirrus DesignSection 9SR22 / SR22 TSupplementsP/N 13772-1355 of 32 Section 3A - Abnormal ProceduresAltitude MiscompareALT MISCOMP CautionFor dual ADC installations, altitude difference is greater than 200 feetbetween ADC1 and Altitude .. CROSS-CHECK ADC1 against Standby Altimeter2. ADC2 .. SELECTa. Press SENSOR softkey on PFD, followed by ADC2 softkeyb. Expect USING ADC2 message on PFD3.

6 Altitude .. CROSS-CHECK ADC2 against Standby Altimeter4. ADC .. SELECT more reliablea. Press SENSOR softkey, then select the ADC that provided themost reliable altitude indicationAirspeed MiscompareIAS MISCOMP CautionFor dual ADC installations, airspeed difference is greater than 7 knotsbetween ADC1 and CROSS-CHECK ADC1 against Standby Airspeed Indicator2. ADC2 .. SELECTa. Press SENSOR softkey on PFD, followed by ADC2 softkeyb. Expect USING ADC2 message on PFD3. CROSS-CHECK ADC2 against Standby Airspeed Indicator4. ADC .. SELECT more reliablea. Press SENSOR softkey, then select the ADC that provided themost reliable airspeed indicationALT MISCOMPIAS MISCOMPR evision 04: 09-08-146 of 32P/N 13772-135 Section 9 Cirrus DesignSupplementsSR22 / SR22 THeading MiscompareHDG MISCOMP CautionFor dual AHRS installations, heading difference is greater than 6 between AHRS 1 and AHRS CROSS-CHECK AHRS1 against Magnetic Compass2.

7 AHRS2 .. SELECTa. Press SENSOR softkey on PFD, followed by AHRS2 softkeyb. Expect USING AHRS2 message on PFD3. Altitude .. CROSS-CHECK AHRS2 against Magnetic Compass4. AHRS .. SELECT more reliablea. Press SENSOR softkey, then select the AHRS that providedthe most reliable heading indicationPitch MiscomparePIT MISCOMP CautionFor dual AHRS installations, pitch difference is greater than 5 between AHRS 1 and AHRS 2. flight Director, Autopilot, and ESP (ifinstalled) will not be available when pitch miscompare Pitch ..CROSS-CHECK AHRS1 against Stdby Attitude Indicator2. AHRS2 .. SELECTa. Press SENSOR softkey on PFD, followed by AHRS2 softkeyb. Expect USING AHRS2 message on PFD3. Pitch ..CROSS-CHECK AHRS2 against Stdby Attitude Indicator4. AHRS .. SELECT more reliablea. Press SENSOR softkey, then select the AHRS that providedthe most reliable pitch indication5.

8 UNRELIABLE AHRS CIRCUIT BREAKER .. PULLP ulling circuit breaker for unreliable AHRS will clear miscomparecondition, but will result in 'NO PIT/ROLL/HDG COMPARE'HDG MISCOMPPIT MISCOMPR evision 04: 09-08-14 Cirrus DesignSection 9SR22 / SR22 TSupplementsP/N 13772-1357 of 32advisory since backup source is not available for Director, Autopilot and ESP will become available whenunreliable AHRS CB is MiscompareROLL MISCOMP CautionFor dual AHRS installations, roll (bank) difference is greater than 6 between AHRS 1 and AHRS CROSS-CHECK AHRS1 against Stdby Attitude Indicator2. AHRS2 .. SELECTa. Press SENSOR softkey on PFD, followed by AHRS2 softkeyb. Expect USING AHRS2 message on PFD3. CROSS-CHECK AHRS2 against Stdby Attitude Indicator4. AHRS .. SELECT more reliablea.

9 Press SENSOR softkey, then select the AHRS that providedthe most reliable roll indication5. UNRELIABLE AHRS CIRCUIT PULLP ulling circuit breaker for unreliable AHRS will clear miscomparecondition, but will result in 'NO PIT/ROLL/HDG COMPARE'advisory since backup source is not available for Director, Autopilot and ESP will become available whenunreliable AHRS CB is MiscompareAP MISCOMP CautionAutopilot miscompare, Autopilot is not Continue flight without Autopilot or isolate and remove theunreliable sensor to clear the MISCOMP as described for ROLL orPIT MISCOMP checklists to restore the MISCOMPAP MISCOMPR evision 04: 09-08-148 of 32P/N 13772-135 Section 9 Cirrus DesignSupplementsSR22 / SR22 TAutopilot and PFD Using Different AHRSsAP/PFD AHRS CautionThe Autopilot and PFD are using different Attitude and HeadingReference Continue flight without Autopilot.

10 Monitor Standby may manually select other AHRS if Autopilot ADC Modes AvailableNO ADC MODES CautionAutopilot air data modes are not Autopilot may only be engaged in pitch (PIT) Autopilot Vertical Modes AvailableNO VERT MODES CautionAutopilot vertical modes are not Autopilot may only be engaged in lateral Selection DeviationALTITUDE SEL AdvisoryThe pilot has programmed the Autopilot to climb or descend away fromthe selected altitude. Typically done Altitude Selection .. CORRECT, AS REQUIREDAP/PFD AHRSNO ADC MODESNO VERT MODESALTITUDE SELR evision 04: 09-08-14 Cirrus DesignSection 9SR22 / SR22 TSupplementsP/N 13772-1359 of 32 Course Selection Track ErrorCOURSE SEL AdvisoryThe pilot has selected an Autopilot mode (ROL) and engaged a NAVmode (VLOC or GPS) and the current aircraft track will not interceptthe selected course.