2 The system information, procedures and guidelines found in this presentation are for Reference Only. The information & procedures in this presentation have been taken from the FAA Approved Airplane Flight Manual and Pilot’s Operating Handbook (POH). The Information & Procedures in this presentation DO NOT SUPERSEDE the Information & Procedures in the POH. In the event of conflict, the POH shall take precedence.
3 General Rate autopilot Two axis control system Roll axis controlled by aileron trim motor and spring cartridgePitch axis controlled by pitch trim motorPowered by Essential Bus
6 Manufacturers NotesSR-22 installation utilizes aircrafts roll trim actuator. The automatic trim feature is not utilized.
7 Limitations Operation prohibited at speeds in excess of 185 KIAS Autopilot must be disengaged for takeoff and landingAutopilot must be disengaged for the missed approach, go around, or balked landingFlaps must be set to 50% for autopilot operation in Altitude Hold at speeds below 95 KIASFlap deflection is limited to 50% during autopilot operationsThe S-Tec System 55X POH must be carried in the airplane and available to the pilot while in flight
8 LimitationsAutopilot must be disconnected in moderate or severe turbulenceMinimum engagement height is 400 feet AGLFor VOR/GPS, ILS glideslope and localizer intercept, capture, and tracking, the following limitations apply:Autopilot must be disengaged no later than 100 feet below the MDAAutopilot must be disconnected if course deviation exceeds 50% (approach may be continued if hand flown)Autopilot must be disengaged at the Decision Height12 knot maximum crosswind component between the outer marker and the missed approach pointIf the crosswind component is greater than 12 knots but less than 17, the intercept should occur at least 10 miles outside the outer marker
9 LimitationsThe intercept of the localizer shall occur at least 5 miles outside of the outer markerThe intercept angle shall be no greater than 45°The glideslope is approached in such a manner to allow automatic arming of the glideslope, or if the glideslope is manually armed no more than 15% above the glideslope
10 InitializationAt power up verify illumination of all autopilot mode annunciatorsCWS and TRIM annunciators will not illuminateRDY will illuminate when Turn Coordinator gyro has reached an operational speed
11 Preflight Test Heading Mode Center HDG Bug on PFD Select HDG Mode on autopilot mode controllerRotate HDG knob left and right of lubber lineVerify proper roll control inputsVertical SpeedSelect VS mode on autopilot mode controllerRotate VS control knob to feet and – 500 feetVerify proper pitch control inputs
12 Preflight Test Altitude Hold Select ALT mode on autopilot mode controllerVerify ALT annunciation, VS annunciation extinguishes, and stationary yokeOverpowerGrasp control yoke and move in all directions. Action should be smooth in all directions with no noise or jerky feel
13 Preflight Test Radio Check Tune to a valid NAV station Select VLOC on HSI displaySelect NAV mode on autopilot mode controllerTurn CDI left and right of course verifying roll inputs in direction of needle adjustment
14 Autopilot Disconnect Check Select HDG and ALT modePress A/P DISC switch, verify disconnectEngage pitch trim, verify disconnectHolding DISC switch will cancel beeping
15 In-Flight Procedures Heading Mode Select HDG Mode on autopilot mode controllerPosition HDG Bug as desiredSame as Pre Flight test proceduresBe aware that if the HDG Bug exceeds 180° from the current heading, the AP will want to turn in the opposite direction as desiredNOTE
16 In-Flight Procedures NOTE Navigation Mode Ensure a reliable VOR or Localizer signal existsSelect the desired course using the CDISelect NAV mode on the autopilot mode controllerIf the CDI is at full scale deflection the autopilot will command a default 45° intercept angleTo intercept the course at an angle other than 45°Position the HDG Bug to the desired intercept angleHold the HDG button while selecting NAV mode on autopilot mode controllerAutopilot will fly selected heading until course interceptNOTE
17 In-Flight Procedures GPS Steering Mode Ensure a reliable GPS signal and flight plan existVerify the HSI will auto-slew your coursePress the NAV button twice on the autopilot mode controllerVerify illumination of NAV and GPSS annunciators
18 In-Flight Procedures NOTE GPS Steering Mode If the CDI is at full scale deflection the autopilot will command a default 45° intercept angleTo intercept the course at an angle other than 45°Position the HDG Bug to the desired intercept angleHold the HDG button while pressing the NAV button twice on autopilot mode controllerAutopilot will fly selected heading until course interceptNOTE
19 In-Flight Procedures Difference between NAV mode and GPSS mode While the AP is in NAV mode it will determine what guidance corrections are needed by reference to what is happening on the HSI.While the AP is in GPSS mode it will determine what guidance corrections are needed by reference to what is happening on the GPS unit. (Selected GPS unit if using PFD)The AP flies a much more accurate course because the difference between your desired course (DTK) and your current track (TRK) can be determined by the GPS unit. GPSS also allows turn anticipation. A HSI does not know your groundspeed, distance to waypoint or degree of course change to determine an early turn, the GPS does.NOTE
20 In-Flight Procedures Altitude Hold Mode Manually fly the airplane to the desired altitude and level offA roll mode (HDG/NAV/GPSS/APR) must be selected prior to engaging a pitch modeSelect ALT mode on autopilot mode controllerAltitude may be fine tuned using the VS knob20 foot incrementsMaximum authority +/- 360 feetNOTE
21 In-Flight Procedures Vertical Speed Mode Select VS mode on autopilot mode controllerA roll mode (HDG/NAV/GPSS/APR) must be selected prior to engaging a pitch modeSelect the desired vertical speed using the VS knob on the PFD100 foot incrementsMaximum authority +/ feetNOTENOTE
22 In-Flight Procedures Altitude Capture The autopilot will capture an altitude that is selected in the PFDSelect the desired altitude on the PFDSelect the desired climb/descent rateIf none is selected a +/- 500 fpm is defaultedEngage a roll mode (HDG/NAV/GPSS/APR)Hold the VS button while pressing the ALT button and verify that both annunciators remain lit
23 In-Flight Procedures Vertical Speed Mode A flashing VS annunciator indicates excessive error between selected vertical speed and actual vertical speed.The pilot should adjust power or vertical speed rate selected to correct errorBe aware that the AP will stall the aircraft in the event that a vertical speed is to high for the current altitude or power settingCAUTION
24 Approach Procedures VOR / Localizer Approach Ensure a reliable VOR or Localizer signal existsSelect the desired course using the CDISelect APR mode on the autopilot mode controllerVerify illumination of NAV and APR annunciatorsCourse intercept is identical to the In-Flight ProceduresFor station passage, select HDG mode with the HDG bug set within 5° of the selected courseProcedure turns must be flown using HDG modeNOTE
25 Approach Procedures Localizer Back Course Approach Ensure a reliable Localizer signal existsSelect the desired course using the CDISelect APR and REV modes on the autopilot mode controllerVerify illumination of NAV, APR, and REV annunciatorsCourse intercept is identical to the In-Flight ProceduresThe front course should always be selected course when executing a LOC BC approachProcedure turns must be flown using HDG modeNOTE
26 Approach Procedures GPS Approach Ensure the GPS approach has been properly loaded and activatedVerify the HSI will auto-slew your inbound courseSelect GPSS mode on the autopilot mode controllerCourse intercept is identical to the In-Flight ProceduresNOTE
27 Approach Procedures GPS Approach Procedure turns must be flown using HDG mode.The autopilot will fly the outbound and the inbound segment of an approach. However you must fly the procedure turn using HDG modeAlthough displayed on the GPS, the autopilot is not capable of flying the depicted turn without pilot actionNOTE
28 Approach Procedures ILS Approach Ensure a reliable Localizer signal existsVerify that the HSI will auto-slew your inbound courseSelect APR mode on the autopilot mode controllerVerify illumination of NAV and APR annunciatorsCourse intercept is identical to the In-Flight ProceduresProcedure turns must be flown using HDG modeIf it is necessary to track outbound on the front course, REV mode must be selectedNOTE
29 Approach Procedures ILS Approach Glideslope Coupling APR and ALT modes must be selectedAircraft must be within ½ scale deflection of localizerAircraft must be 60% or more below the glideslopeCondition must exist for 10 seconds for GS mode to armArm indicated by illumination of ALT and GS annunciatorsALT annunciator extinguishes at glideslope interceptGS mode may be manually engaged by pressing ALT once when in ALT mode and a glideslope signal exists as long as the aircraft has the criteria aboveNOTE
30 Abnormal ProceduresWARNINGDo not attempt to correct autopilot malfunctions unless you are in a safe maneuvering phase of flight and at a safe altitude
31 Abnormal Procedures Autopilot Disconnect Annunciation Condition Action Flashing RDY for 5 seconds with audible toneAutopilot disconnect. All annunciations except RDY are cleared.None.
32 Abnormal Procedures Low Gyro Speed Annunciation Condition Action Flashing RDY with audible tone then goes outTurn coordinator gyro speed low. Autopilot disengages and cannot be re-engaged.Check power to turn coordinator. If starting aircraft in cold weather, allow additional time for gyro to come to speed.
33 Abnormal Procedures Off Course Annunciation Condition Action Flashing NAV, REV, or APROff navigation course by 50% needle deviation or more.Use HDG mode until problem is identified. Crosscheck raw NAV data, compass heading, and radio operation.
34 Abnormal Procedures Invalid radio navigation signal Annunciation ConditionActionFlashing NAV, REV, or APR with steady FAILInvalid radio navigation signalCheck Nav radio for proper reception. Use HDG mode until problem is corrected.
35 Abnormal Procedures Excessive Vertical Speed Error Annunciation ConditionActionFlashing VSExcessive vertical speed error over selected vertical speed. Usually occurs in climb.Reduce VS command and/or adjust power as appropriate.
36 Abnormal Procedures Glideslope deviation Annunciation Condition Action Flashing GSOff glideslope centerline by 50% needle deviation or more.Check altitude and power. Adjust power as appropriate.
37 Abnormal Procedures Invalid Glideslope signal Annunciation Condition ActionFlashing GS with steady FAILInvalid glideslope radio navigation signal.Disconnect autopilot and initiate go-around or missed approach procedure. Inform ATC.
38 Abnormal Procedures Manual Glideslope Disabled Annunciation Condition ActionFlashing GS plus ALTManual glideslope disabled.Re-enable by pressing NAV mode button.
39 Emergency Procedures Autopilot Malfunction The autopilot may be disconnected by:Pressing A/P DISC on the control yokeUsing manual pitch trim with a vertical mode selectedPulling the Autopilot Circuit BreakerDue to the positioning on the circuit breaker panel, the pilot should be able to identify the following circuit breakers without visual referenceAutopilotPitch Trim ServoRoll Trim ServoWARNING
40 Emergency Procedures Recovery – Loss of Altitude Use of these figures assumes an immediate response to an autopilot malfunctionFlight PhaseBank AngleAltitude LossClimb40°200 feetCruise45°300 feetDescent350 feetManeuvering10°60 feetApproach80 feetWARNING
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