Bendix King Kap 150 Manual
Find great deals on eBay for bendix king. Shop with confidence. Skip to main content. Bendix King RDS 81 Radar install manual See more like this. Original Bendix/King KFC-150, KAP-150 & KAP-100 Trifold Brochure, 8.5 x 11' Pre-Owned.
. KAP 140 Pilot’s Guide Bendix/King ® Autopilot System Rev. 2 May 02 006. All rights reserved. Reproduction of this publication or any portion thereof by any means without the express written permission of Honeywell International Inc. Is prohibited.
For further information contact the Manager, Technical Publications; Honeywell; One Technology Center; 23500 West 105th Street; Olathe. Revision History and Instructions Manual KAP 140 Pilot’s Guide Revision 2, May 2002 Part Number 006- This revision makes some of the changes for software version 03/01 more consistent throughout the Pilot’s Guide. The affected pages are 9, 12, 13, 55, 58, 83, 86 and 109. Revision History and Instructions Manual KAP 140 Pilot’s Guide Revision 1, April 2002 Part Number 006- This revision incorporates changes for software version 03/01. Revision History and Instructions Manual KAP 140 Pilot’s Guide Revision 0, June 1998 Part Number 006- This is the original version of this publication.
This page intentionally left blank. KAP 140 Single Axis Operation.9. Operations With The KAP 140.90. The first of a malfunction. In addition to relia- of its type developed by Honeywell, bility, the KAP 140 is designed to be this system brings digital technology easily maintained in the field. And reliability into the light aircraft Qualified Honeywell Service Centers cockpit.
KAP 140 Single Axis KAP 140 Two Axis/Altitude Autopilot System Preselect Autopilot System The KAP 140 Single Axis system is The KAP 140 Two Axis system pro- an entry level digital panel-mount vides both lateral and vertical modes autopilot, offering lateral modes only with altitude preselect. HSI) HSI) HSI) Auto 45-degree Intercept Standard Standard Standard (with DG only) (with DG only) (with DG only) TEST Manual and Auto Trim Monitor Both Both Both Acceleration Monitor KAP 140 System Capabilities Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. The individual system diagrams on pages 5, 6, and 7 show the compo- nents and their relationship in typical KAP 140 Single Axis, KAP 140 Two Axis, and KAP 140 Two Axis/Altitude Preselect systems. The actual com- ponents on individual systems may.
KI 525A Pictorial Flux Detector Trim Interrupt Navigation Indicator (Optional) AUTO KCS 55A Slaved Compass System (Optional) KA 51B Slaving Accessory Control Manual WheelSteering Electrical Trim (Optional) (Optional) KAP 140 Single Axis System Diagram Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. KI 525A Pictorial Flux Detector Disconnect/ Navigation Indicator Trim Interrupt KCS 55A Slaved AUTO Compass System (Optional) KA 51B Slaving Accessory Control Manual WheelSteering Electrical Trim (optional) KAP 140 Two Axis System Diagram Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. KI 525A Pictorial Flux Detector Disconnect/ Navigation Indicator Trim Interrupt AUTO KCS 55A Slaved Compass System (Optional) KA 51B Slaving Accessory Control Manual WheelSteering Electrical Trim (optional) KAP 140 Two Axis/Altitude Preselect System Diagram Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02.
Introduction Power Application and Preflight Tests KAP 140 KAP 140 Preflight Test KAP 140 KAP 140 Preflight Test Complete For two-axis units only: A preflight test is performed upon power application to the com- NOTE: Following the preflight test, puter. This test is a sequence of. Single Axis Operation KAP 140 Single Axis Operation The KAP 140 is a high-performance digital, panel-mounted autopilot sys- tem for light aircraft.
KAP 140 Single-axis Flight Control Computer KAP 140 Full Single-axis KAP 140 Display 1. AUTOPILOT ENGAGE/DISEN- and maintain the heading selected.
(for 2 sec- onds). AUTOPILOT ENGAGED (AP) ANNUNCIATION - Illuminates whenever the autopilot is engaged. Flashes during pilot initiated or auto- matic disengagement. Only applica- ble for software versions 03/01 or later.
1 KAP 140 AUTOPILOT SYSTEM Apr/02. Single Axis Operation This page intentionally left blank Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. For software version 03/01 and later, the AP button must be pressed and held for 0.25 seconds to engage the autopilot. NO PITCH NOTE: The KAP 140 engages into INFORMATION ROL mode as a default. 2 KAP 140 AUTOPILOT SYSTEM May/02.
AP button must be pressed and held for 0.25 seconds to engage the autopilot. Depress the HDG button on the KAP 140 to engage the heading select mode. The autopilot will turn the aircraft in the shortest direction to intercept and fly the heading. In the navigation (NAV) mode, the autopilot intercepts and tracks TURN COORDINATOR VOR/RNAV and GPS courses. To arm NAV mode (with the KAP 140 currently in the HDG 2 MIN. Mode): NO PITCH INFORMATION 1.
Select the desired frequency for VOR or RNAV. If the D-Bar is less than 2 to 3 dots: the HDG mode will disengage upon select- ing NAV mode; the NAV annunci- ator will illuminate and the capture/ track sequence will automatically begin. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. In the navigation (NAV) mode, the autopilot intercepts and tracks TURN COORDINATOR VOR/RNAV and GPS courses. To arm NAV mode (with the KAP 140 currently in the ROL 2 MIN. Mode): NO PITCH INFORMATION 1. Maneuver the aircraft to the desired intercept angle prior to selecting ROL mode.
Note: Intercept angles greater than 45° can result in course overshoot when close station. Therefore, intercept angles greater than 45° are not recommended. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. In the navigation (NAV) mode, the autopilot intercepts and tracks TURN COORDINATOR VOR/RNAV and GPS courses.
To arm NAV mode (with the KAP 140 currently in the HDG mode): 2 MIN. NO PITCH INFORMATION 1. Select the desired frequency for VOR or RNAV. Note: Intercept angles greater than 45° can result in course overshoot when close to the station. Therefore, intercept angles greater than 45° are not recommended. 1 KAP 140 AUTOPILOT SYSTEM Apr/02.
TURN COORDINATOR track LOC, VOR/RNAV and GPS courses. To arm APR mode (with the 2 MIN. KAP 140 currently in the HDG NO PITCH mode): INFORMATION 1. Select the desired frequency for LOC, VOR or RNAV. For GPS, verify the desired approach. If the D-Bar is less than 2 to 3 dots: the HDG mode will disengage upon select- ing APR mode; the APR annunci- ator will illuminate and the capture/ track sequence will automatically begin. 1 KAP 140 AUTOPILOT SYSTEM Apr/02.
TURN COORDINATOR track LOC, VOR/RNAV and GPS courses. To arm APR mode (with the 2 MIN. KAP 140 currently in the ROL NO PITCH mode): INFORMATION 1. Maneuver the aircraft to the desired intercept angle prior to selecting ROL mode.
Note: Intercept angles greater than 45° can result in course overshoot when close station. Therefore, intercept angles greater than 45° are not recommended. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. The Approach (APR) mode allows the autopilot to intercept and TURN COORDINATOR track LOC, VOR/RNAV and GPS courses. To arm APR mode (with the KAP 140 currently in the HDG 2 MIN. Mode): NO PITCH INFORMATION 1.
Select the desired frequency for LOC, VOR or RNAV. APR annunciator will illumi- nate and the capture/track sequence will automatically begin. Note: Intercept angles greater than 45° can result in course overshoot when close station. Therefore, intercept angles greater than 45° are not recommended.
1 KAP 140 AUTOPILOT SYSTEM Apr/02. The Back Course (REV) mode allows the autopilot to intercept and TURN COORDINATOR track a localizer back course. To arm REV mode (with the KAP 140 currently in the HDG 2 MIN. Mode): NO PITCH INFORMATION 1. Select the desired frequency for LOC.
If the D-Bar is less than 2 to 3 dots: the HDG mode will disengage upon select- ing REV mode; the REV annunci- ator will illuminate and the capture/ track sequence will automatically begin. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. The Back Course (REV) mode allows the autopilot to intercept and TURN COORDINATOR track a localizer back course.
To arm REV mode (with the KAP 140 currently in the ROL 2 MIN. Mode): NO PITCH INFORMATION 1.
Maneuver the aircraft to the desired intercept angle prior to selecting ROL mode. Note: Intercept angles greater than 45° can result in course overshoot when close station. Therefore, intercept angles greater than 45° are not recommended. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. The Back Course (REV) mode allows the autopilot to intercept and TURN COORDINATOR track a localizer back course. To arm REV mode (with the KAP 140 currently in the HDG mode): 2 MIN.
Select the desired frequency for INFORMATION LOC. REV annunciator will illumi- nate and the capture/track sequence will automatically begin. Note: Intercept angles greater than 45° can result in course overshoot when close station. Therefore, intercept angles greater than 45° are not recommended. 1 KAP 140 AUTOPILOT SYSTEM Apr/02.
The heading bug on the DG or HSI is turned to the desired heading of 080° (runway heading). By depressing the HDG button on the KAP 140, the autopilot engages into the heading mode and maintains the selected heading of 080°. The autopilot has completed the turn and is mode with a left bank.
Now established on a 010° heading. Note: The autopilot controls only the roll axis.
The PILOT must maintain control of the pitch and yaw axis. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. HDG and flash for five seconds. ROL will then be redisplayed. While the HDG annunciation is flashing, move the heading bug to the desired course of 040°.
Bendix King Kap 150 Manual Projector
The aircraft will remain wings level until the capture point. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. The turn is complete and the autopilot is track- 3. When the computed capture point is reached, ing the GPS course. The ROL annunciation changes to NAV and a right turn is initiated by the autopilot. 1 KAP 140 AUTOPILOT SYSTEM Apr/02.
Continuing on heading 010°, a GPS waypoint is 2. GPS data is selected for the HSI. The course established. A 30° intercept is desired. Pointer is set to 040°.
The NAV button is depressed and NAV ARM is annunciated. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. The turn is complete and the autopilot is track- 3. When the computed capture point is reached, ing the GPS course. The HDG annunciation changes to NAV and a right turn is initiated by the autopilot. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. In this case, the aircraft will turn to to center a deviation of the index to the left).
Needle reversing takes place because you are fly- ing outbound on a front course. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. You must now select the approach mode outbound, the CDI course index goes off scale by depressing the APR button on the KAP 140. To the right. The aircraft is flying away from the While the HDG annunciation is flashing move localizer centerline at a 45°.
The capture point is now being computed based on closure Note: The left-right deviations of the HSI course rate. Needle operate just as though you were flying a front course approach. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. You must now select the approach mode outbound, the deviation bar shows that the air- by depressing the APR button on the KAP 140. Craft is flying away from the localizer centerline Automatic capture of the localizer will occur. (HDG annunciation changes to autopilot will make the bank changes as neces- APR).
The autopilot will capture the localizer sary to maintain localizer. And the CDI course index will center.
1 KAP 140 AUTOPILOT SYSTEM Apr/02. This cancels all operating modes. By depressing the HDG button on the The flashing AP annunciations are displayed and KAP 140, the autopilot engages into the head- a disconnect tone will sound.
Ing mode, commencing a right turn to a head- ing of 090°. The autopilot is following the localizer. The pling occurs (HDG annunciation changes to autopilot will make bank changes as necessary APR).
The autopilot will capture the localizer to maintain localizer. And the CDI course index will center. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. This cancels all operating modes. By depressing the HDG button on the KAP 140, the autopilot engages into the head- ing mode, commencing a right turn to a head- ing of 090°. 238°, the GPS’s Leg/OBS mode annunciator.
switching is set to OBS mode and the OBS is set to 238°. The autopilot initiates a left turn to track the 238° GPS course.
1 KAP 140 AUTOPILOT SYSTEM Apr/02. Check the heading displayed on the DG against Since the 45° intercept is 103°, the aircraft will the magnetic compass and reset if necessary. Not turn until the course is captured. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. Approach arm is indicated on the GPS pointer is set to 238°, the GPS’s Leg/OBS mode annunciator.
switching is set to OBS mode. The autopilot ini- tiates a left turn to track the 238° GPS course. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. Leg mode and the course pointer is set to aircraft is flying away from the GPS course at a 058°. Select approach mode by depressing the 45° angle on a selected heading of 283°.
1 KAP 140 AUTOPILOT SYSTEM Apr/02. The autopilot initiates a autopilot will make the bank changes as neces- left turn to track the 058° GPS course. Sary to maintain the GPS course. Approach active is indicated on the GPS annunciator.
Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02.
This cancels all operating modes. By depressing the HDG button on the The flashing AP annunciations are displayed and KAP 140, the autopilot engages into the head- a disconnect tone will sound. Ing mode, commencing a right turn to a head- ing of 090°. The autopilot initiates a autopilot will make the bank changes as neces- left turn to track the 058° GPS course.
sary to maintain the GPS course. Approach active is indicated on the GPS annunciator. Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. This cancels all operating modes. By depressing the HDG button on the The flashing AP annunciations are displayed and KAP 140, the autopilot engages into the head- a disconnect tone will sound. Ing mode, commencing a right turn to a head- ing of 090°.
Single Axis Operation This page intentionally left blank Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. Two Axis Operation KAP 140 Two Axis Operation The KAP 140 is a digital, panel-mounted autopilot system for light air- craft. KAP 140 Two-axis Flight Control Computer KAP 140 Full Two-Axis KAP 140 Display 1. PITCH AXIS, (P) ANNUNCIATOR and later, the AP button must be - When illuminated, indicates failure pressed and held for 0.25 seconds. ALT button is pressed.
If the be indicated by a solid PT. When the ALT button is pressed with an estab- fault is corrected, the annunciation lished VS rate present, there will be will extinguish. Altitude overshoot (approximately Rev.
1 KAP 140 AUTOPILOT SYSTEM Apr/02. Displays the active and armed pitch The lateral modes (HDG, NAV, APR modes (VS, ALT ARM, ALT, and and REV) operate identically as described in the KAP 140 Single Axis Operating Modes section. ROLL MODE DISPLAY Please refer to that section for text. VS and current vertical cal speed modes. Speed is displayed. Note: The KAP 140 engages into VS 2. UP or DN button - Select mode as a default.
Desired climb or descent rate. 20 feet per press, or if held continuously will com- mand a 500 ft/min altitude change, acquiring a new reference altitude upon button release.
Note: Incremented altitude changes should be limited to 500 ft. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. The heading bug on the DG or HSI is turned to the desired heading of 080° (runway heading). By depressing the HDG button on the KAP 140, the autopilot engages into the heading and ver- tical speed modes and maintains the selected heading of 080°. 010° heading. Desired decreased, using the DN button, in preparation altitude has been reached, altitude hold (ALT) for level off.
Has been engaged and the aircraft maintains the reference altitude. 1 KAP 140 AUTOPILOT SYSTEM Apr/02.
HDG and flash for five seconds. ROL will then be redisplayed. While the HDG annunciation is flashing, move the heading bug to the desired course of 040°. The aircraft will remain wings level until the capture point.
1 KAP 140 AUTOPILOT SYSTEM Apr/02. The turn is complete and the autopilot is track- 3. When the computed capture point is reached, ing the GPS course. The ROL annunciation changes to NAV and a right turn is initiated by the autopilot. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. Continuing on heading 010°, a GPS waypoint is 2.
GPS data is selected for the HSI. The course established. A 30° intercept is desired. Pointer is set to 040°. The NAV button is depressed and NAV ARM is annunciated.
1 KAP 140 AUTOPILOT SYSTEM Apr/02. The turn is complete and the autopilot is track- 3. When the computed capture point is reached, ing the GPS course.
The HDG annunciation changes to NAV and a right turn is initiated by the autopilot. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. This will initiate a 45° intercept to the localizer. In needle reversing takes place because you are fly- this case, the aircraft will turn to 283°. Ing outbound on a front course.
1 KAP 140 AUTOPILOT SYSTEM Apr/02. You must now select the approach mode outbound, the CDI course index goes off scale by depressing the APR button on the KAP 140. To the right. The aircraft is flying away from the.
The HDG annunciation will flash for five sec- localizer centerline at a 45°. The capture point is now being computed Note: The left-right deviations of the HSI course based on closure rate. Needle operate just as though you were flying a front course approach. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. You must now select the approach mode outbound, the deviation bar shows that the air- by depressing the APR button on the KAP 140. Craft is flying away from the localizer centerline Automatic capture of the localizer will occur. The ALT and the CDI course index will center.
Annunciator extinguishes and GS is displayed. The autopilot will make pitch and bank changes as necessary to maintain localizer and glides- lope. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. This cancels all operating modes. The flashing 090°. By depressing the HDG button on the AP annunciationa are displayed and a discon- KAP 140, the autopilot engages into the head- nect tone will sound.
Ing and vertical speed modes, commencing a right turn to a heading of 090°. The ALT and the CDI course index will center. Annunciator extinguishes and GS is displayed.
The autopilot will make pitch and bank changes as necessary to maintain localizer and glides- lope. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. This cancels all operating modes.
The flashing 090°. By depressing the HDG button on the AP annunciations are displayed and a discon- KAP 140, the autopilot engages into the head- nect tone will sound. Ing and vertical speed modes, commencing a right turn to a heading of 090°. 238°, the GPS’s Leg/OBS mode annunciator. switching is set to OBS mode and the OBS is set to 238°. The autopilot initiates a left turn to track the 238° GPS course.
1 KAP 140 AUTOPILOT SYSTEM Apr/02. The HDG annunciation will flash for five sec- onds then extinguish. Move the heading bug within five seconds to 058°. Since the 45° intercept is 103°, the aircraft will not turn until the course is captured. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. Approach arm is indicated on the GPS pointer is set to 238°, the GPS’s Leg/OBS mode annunciator. switching is set to OBS mode.
The autopilot ini- tiates a left turn to track the 238° GPS course. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. Leg mode and the course pointer is set to aircraft is flying away from the GPS course at a 058°. Select approach mode by depressing the 45° angle on a selected heading of 283°. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. The desired descent rate is left turn to track the 058° GPS course. Obtained using the DN button.
Approach active is indicated on the GPS Remember, speed needs to be controlled with annunciator. The throttle. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. By depressing the HDG button on the the autopilot with the button on the control KAP 140, the autopilot engages into the head- wheel. A flashing AP annunciation is displayed ing mode, commencing a right turn to a head- and a distinctive tone will sound.
The desired descent rate is left turn to track the 058° GPS course. Obtained using the DN button.
Approach active is indicated on the GPS Remember, speed needs to be controlled with annunciator. The throttle. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. At the MAP the pilot disengages 090°. By depressing the HDG button on the the autopilot with the button on the control KAP 140, the autopilot engages into the head- wheel. A flashing AP annunciation is displayed ing and vertical speed modes, commencing a and a distinctive tone will sound. Two Axis Operation This page intentionally left blank Rev.
1 KAP 140 AUTOPILOT SYSTEM Apr/02. Two Axis/Altitude Preselect Operations KAP 140 Two Axis with Altitude Preselect Operation The KAP 140 is a digital, panel-mounted autopilot system for light air- craft. BARO KAP 140 Two-axis w/Altitude PreSelect Flight Control Computer BARO KAP 140 Full KAP 140 Two-Axis with Altitude Preselect Display 1. If pushed and held for This button will engage the autopilot 2 seconds, will change the baro set- in units with software prior to soft- ting display from IN HG to HPA or ware version 03/01. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. Flashes during pilot initiated or auto- guishes 200 ft. Prior to the selected matic disengagement.
Only applica- altitude and illuminates momentarily ble for software versions 03/01 or when the selected altitude is later. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. Two Axis/Altitude Preselect Operations System Operating Modes The lateral modes (HDG, NAV, APR and REV) operate identically as depicted in the KAP 140 Single Axis Operating Modes section. Please refer to that sec- tion for text descriptions of lateral mode operation. 20 feet per press, or if held continuously will com- mand a 500 ft/min altitude change, acquiring a new reference altitude upon button release. Note: Incremented altitude changes should be limited to 500 ft.
1 KAP 140 AUTOPILOT SYSTEM Apr/02. The Altitude Preselect 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 KAP 140. The Altitude Alerting function will visually and aurally announce approaching, acquiring and deviation from a selected altitude. Glideslope coupling will preclude an 3. “AUTOPILOT” - Autopilot has altitude capture on an ILS.
Disengaged, either through pilot action or automatically. BARO KFC 140 Rev.
1 KAP 140 AUTOPILOT SYSTEM Apr/02. 7,000 feet is entered using the the desired heading of 080° (runway heading).
Rotary knobs. Altitude ARM annunciation occurs By depressing the HDG button on the KAP 140, automatically upon selection. The autopilot engages into the heading and ver- tical speed modes and maintains the selected heading of 080°. The vertical speed value will be 010° heading. Displayed upon selection of the DN button and will remain for three seconds. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. HDG and flash for five seconds.
ROL will then be redisplayed. While the HDG annunciation is flashing, move the heading bug to the desired course of 040°. The aircraft will remain wings level until the capture point. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. The turn is complete and the autopilot is track- 3. When the computed capture point is reached, ing the GPS course. The ROL annunciation changes to NAV and a right turn is initiated by the autopilot.
1 KAP 140 AUTOPILOT SYSTEM Apr/02. Continuing on heading 010°, a GPS waypoint is 2. GPS data is selected for the HSI.
The course established. A 30° intercept is desired. Pointer is set to 040°. The NAV button is depressed and NAV ARM is annunciated. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. The turn is complete and the autopilot is track- 3. When the computed capture point is reached, ing the GPS course.
The HDG annunciation changes to NAV and a right turn is initiated by the autopilot. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. 45° intercept to the localizer sig- needle reversing takes place because you are fly- nal. In this case, the aircraft will turn to 283°.
Ing outbound on a front course. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. You must now select the approach mode outbound, the CDI course index goes off scale by depressing the APR button on the KAP 140. To the right. The aircraft is flying away from the. The HDG annunciation will flash for five sec- localizer centerline at a 45°.
The capture point is now being computed Note: The left-right deviations of the HSI course based on closure rate. Needle operate just as though you were flying a front course approach. 1 KAP 140 AUTOPILOT SYSTEM Apr/02.
You must now select the approach mode aircraft is flying away from the localizer center- by depressing the APR button on the KAP 140. Line at a 45° angle on a selected heading of Automatic capture of the localizer will occur.
The ALT and the CDI course index will center. Annunciator extinguishes and GS is displayed. The autopilot will make pitch and bank changes as necessary to maintain localizer and glides- lope.
1 KAP 140 AUTOPILOT SYSTEM Apr/02. This cancels all operating modes. The flashing 090°.
By depressing the HDG button on the AP annunciations are displayed and a discon- KAP 140, the autopilot engages into the head- nect tone will sound. Ing and vertical speed modes, commencing a right turn to a heading of 090°.
The ALT and the CDI course index will center. Annunciation extinguishes and GS is displayed. The autopilot will make pitch and bank changes as necessary to maintain localizer and glides- lope. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. This cancels all operating modes. The flashing 090°.
By depressing the HDG button on the AP annunciations are displayed and a discon- KAP 140, the autopilot engages into the head- nect tone will sound. Ing and vertical speed modes, commencing a right turn to a heading of 090°. 238°, the GPS’s Leg/OBS mode annunciator. switching is set to OBS mode and the OBS is set to 238°. The autopilot initiates a left turn to track the 238° GPS course. 1 KAP 140 AUTOPILOT SYSTEM Apr/02.
Since the 45° intercept is 103°, the aircraft will not turn until the course is captured. Check the heading displayed on the DG against the magnetic compass and reset if necessary.
1 KAP 140 AUTOPILOT SYSTEM Apr/02. Approach arm is indicated on the GPS pointer is set to 238°, the GPS’s Leg/OBS mode annunciator. switching is set to OBS mode.
The autopilot ini- tiates a left turn to track the 238° GPS course. 1 KAP 140 AUTOPILOT SYSTEM Apr/02.
Leg mode and the course pointer is set to aircraft is flying away from the GPS course at a 058°. Select approach mode by depressing the 45° angle on a selected heading of 283°. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. The desired descent rate is left turn to track the 058° GPS course. Obtained using the DN button.
Approach active is indicated on the GPS Remember, speed needs to be controlled with annunciator. The throttle. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. At the MAP the pilot disengages 090°.
By depressing the HDG button on the the autopilot with the button on the control KAP 140, the autopilot engages into the head- wheel. A flashing AP annunciation is displayed ing and vertical speed modes, commencing a and a distinctive tone will sound. The desired descent rate is left turn to track the 058° GPS course. Obtained using the DN button. Approach active is indicated on the GPS Remember, speed needs to be controlled with annunciator. The throttle.
1 KAP 140 AUTOPILOT SYSTEM Apr/02. At the MAP the pilot disengages 090°. By depressing the HDG button on the the autopilot with the button on the control KAP 140, the autopilot engages into the head- wheel.
The flashing AP annunciations are dis- ing and vertical speed modes, commencing a played and a distinctive tone will sound. Two Axis/Altitude Preselect Operations This page intentionally left blank Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. Directional Gyro as well as the KI ception and tracking, while eliminat- 525A Pictorial Navigation Indicator is ing the need for scan coordination an optional part of the KAP 140 between two separate indicators. Autopilot System. AUTO KA 51B ı. This play so that the aircraft heading is miniature aircraft always points always at the top, under the lubber toward the top of the display and the line.
0 KAP 140 AUTOPILOT SYSTEM Jun/98. This pointer is set by rotating the to fly. This desired heading is cou- course select knob. Pled to the KAP 140 Autopilot to pro- vide the “Heading Select” function. Course Select Knob - Used to rotate the course pointer to the. The KA 51B can be mounted either vertically or horizon- tally. 0 KAP 140 AUTOPILOT SYSTEM Jun/98.
KCS 55A System, and gyro up degrees per minute to keep the to operating speed, the red “HDG” system aligned with the earth’s flag should disappear from view. Magnetic field. 0 KAP 140 AUTOPILOT SYSTEM Jun/98.
Rotate the course select knob to they do not come into view, a position the course pointer to the usable glideslope signal is not desired VOR course. Being received. 0 KAP 140 AUTOPILOT SYSTEM Jun/98. Note: For system limitations in your is malfunctioning. Glideslope is usu- particular aircraft type, refer to your ally not available during a back Flight Manual Supplement. Course approach. (The VOR and LOC course display will continue to Rev.
0 KAP 140 AUTOPILOT SYSTEM Jun/98. KI525A HSI should the deviation bar will swing give you a better idea towards the center and the angle of intercept will of how simple and decrease. Comprehensive the dis- play is. 0 KAP 140 AUTOPILOT SYSTEM Jun/98. ANX 088 radial.
Once again, you can make a pre- cise, coordinated course inter- ception by adjusting your head- ing to keep the top of the deviation bar touching the lub- ber line. 0 KAP 140 AUTOPILOT SYSTEM Jun/98.
Columbia to Foristell 12 inbound course to FTZ. (FTZ) is 098°, you now set The TO/FROM indicator the selected course pointer on changes to “TO”. 098° and fly to keep the devi- ation bar centered. 0 KAP 140 AUTOPILOT SYSTEM Jun/98. Select the Note: For system limitations St. Louis VORTAC on the NAV refer to your Flight Manual receiver and set the course Supplement.
Pointer on the STL 062° course. 0 KAP 140 AUTOPILOT SYSTEM Jun/98. By keeping the top of the deviation bar on the lubber line, you can complete your turn and roll out precisely on course. Note: For system limitations refer to your Flight Manual Supplement. 0 KAP 140 AUTOPILOT SYSTEM Jun/98. 5° to the display indicates your aircraft is still the right to maintain the localizer course.
Below the glidepath at this point. Note: For system limitations refer to your Flight Manual Supplement. 0 KAP 140 AUTOPILOT SYSTEM Jun/98. You may reset the tion. Heading bug to 058° for easy reference. Note: For system limitations refer to your Flight Manual Supplement. 0 KAP 140 AUTOPILOT SYSTEM Jun/98.
Bendix King Kap 150 Autopilot Manual
Manipulate the controls as required to safely main- tain operation of the airplane within all of its operating limitations. CAUTION: Refer to the Airplane Flight Manual or the Airplane Flight Manual Supplement for your particular aircraft for pertinent emergency procedures. 0 KAP 140 AUTOPILOT SYSTEM Jun/98. Abnormal Procedures This page intentionally left blank Rev.
0 KAP 140 AUTOPILOT SYSTEM Jun/98. Honeywell International Inc. One Technology Center 23500 West 105th Street Olathe, Kansas 66061 FAX 913-791-1302 Telephone: (913) 782-0400 Copyright © 1998, 2002 Honeywell International Inc.
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KFC-150 Autopilot BENDIX/KING KFC 150 Precio: Consultar precio de instalacion KING RADIO KFC-150 Autopilot System (Includes Flight Director and KCS-55A HSI Compass System) If you are interested in the ultimate in panel-mounted flight control systems for a single or twin-engine aircraft, consider the KFC-150 Flight Control System. The system incorporates a sophisticated two-axis autopilot with a flight director system. This combination simplifies your job in the cockpit dramatically, particularly in a challenging IFR environment. The KFC-150 Flight Control System panel units consist of the KC-192 Flight Computer/Mode Controller/Mode Annunciator, the KI-256 Flight Command Indicator, and the KI-525A Horizontal Situation Indicator (HSI). The flight director system is a computer which calculates and displays the appropriate pitch and roll attitudes required to intercept and maintain a course, an approach path, an altitude or a heading. Once computed, the commands are displayed to the pilot on a single cue steering command, which is part of the KI-256 Flight Command Indicator. In some installations, the KI-256 is replaced by a KI-254, which contains an electrically driven, rather than air driven, gyro.
The KI-254 is similar to the KI-256, but has flags for the Flight Director and gyro. The instrument is labeled 'DC' and has a knob to 'cage' the gyro. The KI-525A HSI is part of the Bendix/King KCS-55A Compass System. The KI-525A displays both magnetic heading and horizontal navigation information on the same instrument-hence the name Horizontal Situation Indicator (HSI). The KCS-55A Compass System also helps relieve pilot workload by removing the necessity of periodically resetting magnetic heading.
Since it is a slaved system, it makes automatic adjustments for gyro precession. The autopilot and flight director functions of the KFC-150 combine to provide sophisticated digital flight control capability for singles and twins.