KAP 140 Two Axis with Altitude Preselect Operation

Transcription

1 Two Axis/Altitude reselect Operations K 0 Two Axis with Altitude reselect Operation The K 0 is a digital, panel-mounted autopilot system for light aircraft. 7 8 K 0 D AV V AT D Two-axis w/altitude reelect Flight Control Computer K 0 D AV V AT D Full K 0 Two-Axis with Altitude reselect Display. ITC AXI, () ACIA - hen illuminated, indicates failure of the pitch axis and will disengage the autopilot when the failure occurs and not allow engagement of the pitch axis.. AIOT A/DI- A () BT - hen pushed, engages autopilot if all logic conditions are met. The autopilot will engage in the basic roll (O) mode which functions as a wing leveler and in the vertical speed (V) hold mode. The commanded vertical speed is be displayed in the upper right corner of autopilot display area for three seconds after engagement or if either the or D button is pressed. The captured V will be the vertical speed present at the moment of button press. hen pressed again, will disengage the autopilot. For software version 0/0 ev. May/0 and later, the button must be pressed and held for 0.5 seconds to engage the autopilot.. O AXI () ACIA - hen illuminated, indicates failure of the roll axis and will disengage the autopilot and not allow engagement.. ADI (D) MOD C- BT - hen pushed, will arm the eading mode, which commands the airplane to turn to and maintain the heading selected by the heading bug on either the D or I. A new heading may be selected at any time and will result in the airplane turning to the new heading. Button can also be used to toggle between D and O modes. This button will engage the autopilot in units with software prior to software version 0/0. K 0 AIOT YTM 0 8

2 Two Axis/Altitude reselect Operations 5. AVIATIO (AV) MOD C BT - hen pushed, will arm the navigation mode. The mode provides automatic beam capture and tracking of VO, OC or as selected for presentation on the I or CDI. AV mode is recommended for enroute navigation tracking. AV mode may also be used for front course OC tracking when tracking is not desired.. OAC () MOD C BT - hen pushed, will arm the Approach mode. This mode provides automatic beam capture and tracking of VO,, OC, and lideslope () on an I, as selected for presentation on the I or CDI. mode is recommended for instrument approaches. 7. BACK CO OAC (V) MOD C BT - hen pushed, will arm the Back Course approach mode. This mode functions similarly to the approach mode except that the autopilot response to OC signals is reversed, and is disabled. 8. ATITD OD (AT) MOD CT BT - hen pushed, will select the Altitude old mode. This mode provides tracking of the reference altitude. The reference altitude is the altitude at the moment the AT button is pressed. If the AT button is pressed with an established V rate present, there will be altitude overshoot (approximately 0% of the V rate), with the airplane returned positively to the reference altitude. This button will engage the autopilot in units with software prior to software version 0/0. 8 K 0 AIOT YTM 9. VTICA TIM (/D) BT- - The action of these buttons is dependent upon the vertical mode present when pressed. If V mode is active, the initial button stroke will bring up the commanded vertical speed in the display. ubsequent immediate button strokes will increment the vertical speed commanded either up or down at the rate of 00 ft/min per button press, or at the rate of approximately 00 ft/min per second if held continuously. If AT mode is active, incremental button strokes will move the altitude hold reference altitude either up or down at 0 feet per press, or if held continuously will command the airplane up or down at the rate of 500 ft/min, synchronizing the altitude hold reference to the actual airplane altitude upon button release. (ote that the altitude hold reference is not displayed. The display will continue to show the altitude alerter reference.) 0. OTAY KOB - sed to set the altitude alerter reference altitude; or may be used immediately after pressing the button, to adjust the autopilot baro setting to match that of the airplane s altimeter when manual adjustment is required. (In some installations the baro setting is automatically synced to that of the altimeter.). T () BT - hen pushed and released, will change the display from the altitude alerter selected altitude to the baro setting display (either I or A) for seconds. If pushed and held for seconds, will change the baro setting display from I to A or ev.

3 Two Axis/Altitude reselect Operations vice versa. Once the baro setting display is visible the rotary knobs may be used to manually adjust the baro setting if automatic baro correction is not available.. ATITD () BT- - hen pushed will toggle altitude arming on or off. hen AT is annunciated, the autopilot will capture the altitude alerter displayed altitude (provided the aircraft is climbing or descending in V to the displayed altitude). hen the autopilot is engaged, AT arming is automatic upon altitude alerter altitude selection via the rotary knobs. ote that the alerter functions are independent of the arming process thus providing full time alerting, even when the autopilot is disengaged.. ATITD AT/VTI- CA D/ TTI DI- AY - ormally displays the altitude alerter selected altitude. If the or D button is pushed while in V hold, the display changes to the command reference for the V mode in FM for seconds. If the button is pushed, the display changes to the autopilot baro setting in either I or A for seconds. OT: This display may be dashed for up to minutes on start up if a blind encoder is installed which requires a warm up period. reached. Once the selected altitude is reached a flashing AT illumination signifies that the 00 ft. safe band has been exceeded and will remain illuminated until 000 ft. from the selected altitude. Associated with the visual alerting is an aural alert (5 short tones) which occurs 000 feet from the selected altitude upon approaching the altitude and 00 feet from the selected altitude on leaving the altitude.. ITC TIM (T) ACIA- TIO - A flashing T with arrows indicates the direction of required pitch trim. A solid T without an arrow head is an indication of a pitch trim fault. During manual electric trim operation (autopilot disengaged), detection of a stuck MT switch will be indicated by a solid T. hen the fault is corrected, the annunciation will extinguish.. ITC MOD DIAY - Displays the active and armed pitch modes (V, AT,, AT and ). 7. O MOD DIAY - Displays the active and armed roll modes (O, D, AV, AV,,, V, V, ). Also displayed will be flashing annunciation (5 seconds) at each autopilot disconnect accompanied by an aural tone (for seconds).. ATITD AT (AT) ACIATIO - The AT annunciate is illuminated 000 ft. prior to the selected altitude, extinguishes 00 ft. prior to the selected altitude and illuminates momentarily when the selected altitude is ev. 8. AIOT AD () ACIATIO - Illuminates whenever the autopilot is engaged. Flashes during pilot initiated or automatic disengagement. Only applicable for software versions 0/0 or later. K 0 AIOT YTM 85

4 Two Axis/Altitude reselect Operations ystem Operating Modes The lateral modes (D, AV, and V) operate identically as depicted in the K 0 ingle Axis Operating Modes section. lease refer to that section for text descriptions of lateral mode operation. K 0 D AV V AT D Vertical peed (V) Mode The Vertical peed (V) mode allows variable speed climbs and descents. The AT button toggles between altitude hold and vertical speed modes. ote: The K 0 engages into V mode as a default. To operate in the V mode (with autopilot currently disengaged):. button - ress. ote O, V and current vertical speed is displayed. If no other modes are selected the autopilot will operate in the O and vertical speed hold modes. For software version 0/0 and later, the button must be pressed and held for 0.5 seconds to engage the autopilot.. or D button - elect desired climb or descent rate. ach button stroke will increment the vertical speed commanded up or down by 00 ft/min per button press, or at the rate of approximately 00 ft/min per second if held continuously. To initiate a climb or descent from Altitude old (AT) mode:. AT button - ress. ote AT 8 K 0 AIOT YTM changes to V and current vertical speed is displayed.. or D button - elect desired climb or descent rate. ach button stroke will increment the vertical speed commanded up or down by 00 ft/min per button press, or at the rate of approximately 00 ft/min per second if held continuously. ote: V command value will be displayed during Control heel teering (C) and for three seconds following V engagement or pressing the or D button. Both altitude and vertical speed utilize the same display area. Altitude is always displayed except during vertical speed selection. If the V command value is not displayed, pressing (and releasing) the or D button will not change the indicated altitude reference but will display the V command value. ote: hen operating at or near the best rate of climb airspeed, at climb power settings, and using vertical speed hold, it is easy to decelerate to an airspeed where continued decreases in airspeed will result in a reduced rate of climb. Continued operation in vertical speed mode can result in a stall. ev. May/0

5 Two Axis/Altitude reselect Operations K 0 D AV V AT D Altitude old (AT) Mode The Altitude old (AT) mode maintains the pressure altitude acquired upon selection of altitude hold. The AT button toggles between altitude hold and vertical speed modes. To operate in the AT mode (with autopilot currently in the Vertical peed mode):. AT button - ress. ote AT is annunciated and autopilot maneuvers to maintain pressure altitude acquired at button selection.. or D button - elect to change altitude. Incremented button strokes will move the reference altitude by 0 feet per press, or if held continuously will command a 500 ft/min altitude change, acquiring a new reference altitude upon button release. ote: Incremented altitude changes should be limited to 500 ft. of change. ev. K 0 AIOT YTM 87

6 Two Axis/Altitude reselect Operations Altitude Alerting and reselect The Altitude reselect function allows capturing of a desired altitude and transferring into altitude hold. Manual input of desired altitude is accomplished through the rotary knobs on the faceplate of the K 0. The Altitude Alerting function will visually and aurally announce approaching, acquiring and deviation from a selected altitude. Altimeter etting Baro unit conversion Installations with remote baro input. setting - CCK. depressing the button will display the baro setting for three seconds. KFC 0 The barometric pressure display can toggled between I and A as needed by the pilot.. button - ress and hold for two seconds. KFC 0 D AV V AT D D AV V AT Installations without remote baro input pon successful completion of preflight test, the baro display will flash.. setting - nter barometric setting using the rotary knobs O if correct as displayed, press. D Altitude Alerter The function of the Altitude Alerter is independent of the autopilot.. ATITD CT knob - OTAT until the desired altitude is displayed. KFC 0 KFC 0 D AV V AT D D AV V AT ote: It is recommended that the baro value be updated whenever the aircraft altimeter setting is changed. 88 K 0 AIOT YTM D ote: The AT annunciation is illuminated 000 ft. prior to the selected altitude, extinguishes 00 ft. prior to the selected altitude and illuminates momentarily when the selected altitude is reached. Once the selected altitude is reached, a flashing AT illumination signifies that the 00 ft. safe band has been exceeded and will remain illuminated until 000 ft. from the selected altitude. Associated with the visual ev.

7 Two Axis/Altitude reselect Operations alerting is an aural alert (five short tones) which occurs 000 ft. from the selected altitude upon approaching the altitude and 00 ft. from the selected altitude on leaving the altitude. KFC 0 Altitude reselect. ATITD CT knob - OTAT until desired altitude is displayed. annunciation occurs automatically upon altitude selection when the autopilot is engaged. KFC 0. Airplane - TABI desired vertical speed to intercept the selected altitude. KFC 0 D AV V AT. pon altitude capture, AT will extinguish and AT will be annunciated. ote: Altitude preselect captures are not recommended on non-precision approaches to capture the MDA. lideslope coupling will preclude an altitude capture on an I. KFC 0 D AV V AT D AV V AT D D D Voice Messaging The following standard voice messages will be annunciated as conditions warrant:. TIM I MOTIO, TIM I MOTIO - itch trim running for more than 5 seconds.. CCK ITC TIM - An out of trim condition has existed for seconds. a. Airplane Control heel - FIMY, press C and check for an out of pitch trim condition. Manually retrim as required. b. C button - A. c. AIOT OATIO - COTI if satisfied that the out of trim condition was temporary. DICOTI if evidence indicates a failure of the auto trim function. The following optional voice messages will be annunciated if the system is configured for voice messaging:. ATITD feet before approaching selected altitude.. AVI ATITD - 00 feet away, departing selected altitude.. AIOT - Autopilot has disengaged, either through pilot action or automatically. D AV V AT D ev. K 0 AIOT YTM 89

8 Two Axis/Altitude reselect Operations OATIO IT T K 0 Two Axis/Altitude reselect Operations Takeoff And Climb To Assigned Altitude D.C. C. D.C. C. D.C. C. D.C. C. T COODIA T COODIA T COODIA T COODIA MI. MI. MI. MI. O ITC IFOMATIO O ITC IFOMATIO O ITC IFOMATIO O ITC IFOMATIO 0 0 O 0 O 0 0 O 0 O 0 0 K 0 K 0 K 0 K 0 D AV V AT D D AV V AT D D AV V AT D D AV V AT D. The aircraft is well off the ground and established at a safe climb rate. The heading bug on the D or I is turned to the desired heading of 080 (runway heading). By depressing the D button on the K 0, the autopilot engages into the heading and vertical speed modes and maintains the selected heading of 080 and current rate of climb. ote: ress and hold the button for 0.5 seconds to engage the autopilot (applicable only to software version 0/0 and later).. The heading bug on the D or I is turned to the new desired heading of 00 and the aircraft begins to respond with an immediate left turn. A cruise altitude of 7,000 feet is entered using the rotary knobs. Altitude annunciation occurs automatically upon selection.. The autopilot is responding to the heading select mode with a left bank. The climb rate has been decreased, using the D button, in preparation for level out. The vertical speed value will be displayed upon selection of the D button and will remain for three seconds.. Desired altitude has been reached and automatic altitude capture occurs. The autopilot has completed the turn and is now established on a 00 heading. ev. ev. 90 K 0 AIOT YTM K 0 AIOT YTM 9

9 Two Axis/Altitude reselect Operations Two Axis/Altitude reselect Operations Capture sing D 00 * Description of operation based on Bendix/King receiver. Others may require different operation. D.C. C. D.C. C. D.C. C. D.C. C. T COODIA T COODIA T COODIA T COODIA MI. MI. MI. MI. O ITC IFOMATIO O ITC IFOMATIO O ITC IFOMATIO O ITC IFOMATIO F F F F OB OB 0 OB OB K 0 K 0 K 0 K 0 D AV V AT D D AV V AT D D AV V AT D D AV V AT D. Continuing on heading 00, a waypoint is established. A 0 intercept is desired.. The D button is depressed to select O mode which will allow an all angle intercept. data is selected for the CDI and the OB is set to 00. The AV button is depressed and AV is annunciated. O will change to D and flash for five seconds. O will then be redisplayed. hile the D annunciation is flashing, move the heading bug to the desired course of 00. The aircraft will remain wings level until the capture point.. hen the computed capture point is reached, the O annunciation changes to AV and a right turn is initiated by the autopilot.. The turn is complete and the autopilot is tracking the course. ev. ev. 9 K 0 AIOT YTM K 0 AIOT YTM 9

10 0 0 0 Two Axis/Altitude reselect Operations Two Axis/Altitude reselect Operations Capture sing I 00 * Description of operation based on Bendix/King receiver. Others may require different operation. D.C. C. D.C. C. D.C. C. D.C. C. T COODIA T COODIA T COODIA T COODIA MI. MI. MI. MI. O ITC IFOMATIO O ITC IFOMATIO O ITC IFOMATIO O ITC IFOMATIO 0 0 K 0 K 0 K 0 K 0 D AV V AT D D AV V AT D D AV V AT D D AV V AT D. Continuing on heading 00, a waypoint is established. A 0 intercept is desired.. data is selected for the I. The course pointer is set to 00. The AV button is depressed and AV is annunciated.. hen the computed capture point is reached, the D annunciation changes to AV and a right turn is initiated by the autopilot.. The turn is complete and the autopilot is tracking the course. ev. ev. 9 K 0 AIOT YTM K 0 AIOT YTM 95

11 Two Axis/Altitude reselect Operations Two Axis/Altitude reselect Operations Outbound On Front Course For rocedure Turn To I Approach sing D D.C. C. D.C. C. D.C. C. D.C. C. T COODIA T COODIA T COODIA T COODIA MI. MI. MI. MI. O ITC IFOMATIO O ITC IFOMATIO O ITC IFOMATIO O ITC IFOMATIO 0 AV 0 AV 0 AV AV 0 F 0 F 0 F 0 F 0 OB OB OB OB K 0 K 0 K 0 K 0 D AV V AT D D AV V AT D D AV V AT D D AV V AT D. The aircraft is heading 70 with heading and altitude hold engaged. To intercept and fly the I front course outbound, set the front course on the OB and depress the reverse course (V) button. The D annunciation will flash for five seconds then extinguish. hile the D annunciation is flashing, move the heading bug to the front course 058. ince D was active upon selection of V the autopilot will initiate a 5 intercept to the localizer signal. In this case, the aircraft will turn to 8.. hen the computed capture point is reached, auto intercept mode is cancelled and reverse localizer mode is automatically activated and a left turn outbound on the localizer is initiated by the autopilot. ote: The left-right deviations of the CDI course deviation needle are reversed (you must turn right to center a deviation of the index to the left). This needle reversing takes place because you are flying outbound on a front course.. At the desired point, D mode is used to initiate the procedure turn. elect D and set the heading bug to 8. During the procedure turn outbound, the CDI course index goes off scale to the right. The aircraft is flying away from the localizer centerline at a 5 angle on a selected heading of 8. * Check the heading displayed on the D against the magnetic compass and reset if necessary.. ow you have reset the heading bug to 0 and made a 80 turn to this heading. This 0 heading will intercept the front course of 058. You must now select the approach mode by depressing the button on the K 0. * The D annunciation will flash for five seconds then extinguish. hile the D annunciator is flashing, move the heading bug to the front course 058. ince the 5 intercept is 0, the aircraft will not turn until the front course is captured. ev. ev. 9 K 0 AIOT YTM K 0 AIOT YTM 97

12 Two Axis/Altitude reselect Operations Two Axis/Altitude reselect Operations Outbound On Front Course For rocedure Turn To I Approach sing I D.C. C. D.C. C. D.C. C. D.C. C. T COODIA T COODIA T COODIA T COODIA MI. MI. MI. MI. O ITC IFOMATIO O ITC IFOMATIO O ITC IFOMATIO O ITC IFOMATIO K 0 K 0 K 0 K 0 D AV V AT D D AV V AT D D AV V AT D D AV V AT D. The aircraft is heading 70 with heading and altitude hold engaged. To intercept and fly the I front course outbound, set the front course on the I and depress the back course (V) button. The back course (V) mode is selected to go outbound on the front course. The capture point is now being computed based on closure rate.. hen the computed capture point is reached, D mode is cancelled and reverse localizer mode is automatically activated and a left turn outbound on the localizer is initiated by the autopilot. ote: The left-right deviations of the I course needle operate just as though you were flying a front course approach.. At the desired point, D mode is used to initiate the procedure turn. During the procedure turn outbound, the deviation bar shows that the aircraft is flying away from the localizer centerline at a 5 angle on a selected heading of 8.. ow you have reset the heading bug to 0 and made a 80 turn to this heading. The 0 heading will intercept the front course of 058. You must now select the approach mode by depressing the button on the K 0. Automatic capture of the localizer will occur. ev. ev. 98 K 0 AIOT YTM K 0 AIOT YTM 99

13 Two Axis/Altitude reselect Operations Two Axis/Altitude reselect Operations Front Course I Approach sing D D.C. C. D.C. C. D.C. C. D.C. C. T COODIA T COODIA T COODIA T COODIA MI. MI. MI. MI. O ITC IFOMATIO O ITC IFOMATIO O ITC IFOMATIO O ITC IFOMATIO F 0 0 F 0 F 0 0 F OB OB OB OB K 0 K 0 K 0 K 0 D AV V AT D D AV V AT D D AV V AT D D AV V AT D. Continuing the maneuver on page 9, coupling occurs (D annunciation changes to ), and the glideslope mode is automatically armed. The autopilot will capture the localizer and the CDI course index will center.. The autopilot is following the localizer. At the outer marker, the glideslope deviation needle is at midscale. Altitude hold is automatically disengaged when the glideslope is captured. The AT annunciator extinguishes and is displayed. The autopilot will make pitch and bank changes as necessary to maintain localizer and glideslope.. At the middle marker, the pilot disengages the autopilot with the button on the control wheel. This cancels all operating modes. The flashing annunciations are displayed and a disconnect tone will sound.. The pilot initiates the missed approach and stabilizes the aircraft in the climb. The heading bug is set to the missed approach heading of 090. By depressing the D button on the K 0, the autopilot engages into the heading and vertical speed modes, commencing a right turn to a heading of 090 and maintaining the rate of climb existing at engagement. ote: ress and hold the button for 0.5 seconds to engage the autopilot (applicable only to software version 0/0 and later). ev. ev. 00 K 0 AIOT YTM K 0 AIOT YTM 0

14 Two Axis/Altitude reselect Operations Two Axis/Altitude reselect Operations Front Course I Approach sing I D.C. C. D.C. C. D.C. C. D.C. C. T COODIA T COODIA T COODIA T COODIA MI. MI. MI. MI. O ITC IFOMATIO O ITC IFOMATIO O ITC IFOMATIO O ITC IFOMATIO K 0 K 0 K 0 K 0 D AV V AT D D AV V AT D D AV V AT D D AV V AT D. Continuing the maneuver on page 98, coupling occurs (D annunciation changes to ), and the glideslope mode is automatically armed. The autopilot will capture the localizer and the CDI course index will center.. The autopilot is following the localizer. At the outer marker, the glideslope deviation needle is at midscale. Altitude hold is automatically disengaged when the glideslope is captured. The AT annunciation extinguishes and is displayed. The autopilot will make pitch and bank changes as necessary to maintain localizer and glideslope.. At the middle marker, the pilot disengages the autopilot with the button on the control wheel. This cancels all operating modes. The flashing annunciations are displayed and a disconnect tone will sound.. The pilot initiates the missed approach and stabilizes the aircraft in the climb. The heading bug is set to the missed approach heading of 090. By depressing the D button on the K 0, the autopilot engages into the heading and vertical speed modes, commencing a right turn to a heading of 090 and maintaining the rate of climb existing at engagement. ote: ress and hold the button for 0.5 seconds to engage the autopilot (applicable only to software version 0/0 and later). ev. ev. 0 K 0 AIOT YTM K 0 AIOT YTM 0

15 Two Axis/Altitude reselect Operations Two Axis/Altitude reselect Operations Outbound on Approach sing D * Description of operation based on Bendix/King receiver. Others may require different operation. 8 D.C. C. D.C. C. D.C. C. D.C. C. T COODIA T COODIA T COODIA T COODIA MI. MI. MI. MI. O ITC IFOMATIO O ITC IFOMATIO O ITC IFOMATIO O ITC IFOMATIO F F F 0 F 0 OB OB OB OB K 0 K 0 K 0 K 0 D AV V AT D D AV V AT D D AV V AT D D AV V AT D. The aircraft is in mode approaching the IAF. Approach arm is indicated on the annunciator.*. pon waypoint alerting at the IAF, the heading bug is set to 8, the s eg/ob mode switching is set to OB mode and the OB is set to 8. The autopilot initiates a left turn to track the 8 course.. At the desired point, heading mode is used to initiate the procedure turn. During the procedure turn outbound, the deviation bar shows that the aircraft is flying away from the course at a 5 angle on a selected heading of 8. * Check the heading displayed on the D against the magnetic compass and reset if necessary.. The heading bug has been set to 0 and the aircraft has made a left turn to this heading. The s eg/ob mode switching is set to eg mode and the OB is set to 058. elect approach mode by depressing the button. *The D annunciation will flash for five seconds then extinguish. hile the D annunciation is flashing, move the heading bug to 058. ince the 5 intercept is 0, the aircraft will not turn until the course is captured. ev. ev. 0 K 0 AIOT YTM K 0 AIOT YTM 05

16 Two Axis/Altitude reselect Operations Two Axis/Altitude reselect Operations Outbound on Approach sing I * Description of operation based on Bendix/King receiver. Others may require different operation. 8 D.C. C. D.C. C. D.C. C. D.C. C. T COODIA T COODIA T COODIA T COODIA MI. MI. MI. MI. O ITC IFOMATIO O ITC IFOMATIO O ITC IFOMATIO O ITC IFOMATIO K 0 K 0 K 0 K 0 D AV V AT D D AV V AT D D AV V AT D D AV V AT D. The aircraft is in mode approaching the IAF. Approach arm is indicated on the annunciator.*. pon waypoint alerting at the IAF, the course pointer is set to 8, the s eg/ob mode switching is set to OB mode. The autopilot initiates a left turn to track the 8 course.. At the desired point, heading mode is used to initiate the procedure turn. During the procedure turn outbound, the deviation bar shows that the aircraft is flying away from the course at a 5 angle on a selected heading of 8.. The heading bug has been set to 0 and the aircraft has made a left turn to this heading. The s eg/ob mode switching is set to eg mode and the course pointer is set to 058. elect approach mode by depressing the button. ev. ev. 0 K 0 AIOT YTM K 0 AIOT YTM 07

17 Two Axis/Altitude reselect Operations Two Axis/Altitude reselect Operations Inbound on Approach sing D FAF * Description of operation based on Bendix/King receiver. Others may require different operation. 8 D.C. C. D.C. C. D.C. C. D.C. C. T COODIA T COODIA T COODIA T COODIA MI. MI. MI. MI. O ITC IFOMATIO O ITC IFOMATIO O ITC IFOMATIO O ITC IFOMATIO 0 0 F 0 OB 0 F 0 OB 0 F 0 OB 0 F OB K 0 K 0 K 0 K 0 D AV V AT D D AV V AT D D AV V AT D D AV V AT D. Continuing the maneuver on page 0, mode capture occurs. The autopilot initiates a left turn to track the 058 course. * Approach active is indicated on the annunciator.. At the FAF, AT is depressed to activate vertical speed mode. The desired descent rate is obtained using the D button. emember, speed needs to be controlled with the throttle.. At the MDA, the AT button is depressed causing the autopilot to level off and maintain a constant altitude. At the M the pilot disengages the autopilot with the button on the control wheel. A flashing annunciation is displayed and a distinctive tone will sound.. The pilot initiates the missed approach and stabilizes the aircraft in the climb. The heading bug is set to the missed approach heading of 090. By depressing the D button on the K 0, the autopilot engages into the heading and vertical speed modes, commencing a right turn to a heading of 090 and maintaining the rate of climb existing at engagement. ote: ress and hold the button for 0.5 seconds to engage the autopilot (applicable only to software version 0/0 and later). ev. ev. 08 K 0 AIOT YTM May/0 K 0 AIOT YTM 09

18 Two Axis/Altitude reselect Operations Two Axis/Altitude reselect Operations Inbound on Approach sing I FAF * Description of operation based on Bendix/King receiver. Others may require different operation. 8 D.C. C. D.C. C. D.C. C. D.C. C. T COODIA T COODIA T COODIA T COODIA MI. MI. MI. MI. O ITC IFOMATIO O ITC IFOMATIO O ITC IFOMATIO O ITC IFOMATIO K 0 K 0 K 0 K 0 D AV V AT D D AV V AT D D AV V AT D D AV V AT D. Continuing the maneuver on page 0, mode capture occurs. The autopilot initiates a left turn to track the 058 course. * Approach active is indicated on the annunciator.. At the FAF, AT is depressed to activate vertical speed mode. The desired descent rate is obtained using the D button. emember, speed needs to be controlled with the throttle.. At the MDA, the AT button is depressed causing the autopilot to level off and maintain a constant altitude. At the M the pilot disengages the autopilot with the button on the control wheel. The flashing annunciations are displayed and a distinctive tone will sound.. The pilot initiates the missed approach and stabilizes the aircraft in the climb. The heading bug is set to the missed approach heading of 090. By depressing the D button on the K 0, the autopilot engages into the heading and vertical speed modes, commencing a right turn to a heading of 090 and maintaining the rate of climb existing at engagement. ote: ress and hold the button for 0.5 seconds to engage the autopilot (applicable only to software version 0/0 and later). ev. ev. 0 K 0 AIOT YTM K 0 AIOT YTM

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