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s Guide Long Island Aviators
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Information subject to the export control laws This document which includes. any attachments and exhibits hereto contains information subject to. International Traffic in Arms Regulation ITAR or Export Administration. Regulation EAR of 1979 which may not be exported released or disclosed. to foreign nationals inside or outside the U S without first obtaining an export. license Violators of ITAR or EAR may be subject to a penalty of 10 years. imprisonment and a fine of 1 000 000 under 22 U S C 2778 or Section. 2410 of the Export Administration Act of 1979 Include this notice with any. reproduced portion of this document, COPYRIGHT NOTICE. 1998 AlliedSignal Inc, Reproduction of this publication or any portion thereof by any means without. the express written permission of AlliedSignal Electronic and Avionics. Systems is prohibited For further information contact the Manager Technical. Publications AlliedSignal Electronic and Avionics Systems One Technology. Center 23500 West 105th Street Olathe Kansas 66061 Telephone 913. Table of Contents, Introduction 1, General Description 2. KAP 140 Single Axis Autopilot System 2, KAP 140 Two Axis Autopilot System 2. KAP 140 Two Axis Altitude Preselect Autopilot System 2. System Integration 4, Power Application and Preflight Tests 8.
KAP 140 Single Axis Operation 9, System Operating Modes 12. Wing Leveler ROL Mode 12, Heading Select HDG Mode 13. Navigation NAV Mode Using a DG from HDG Mode, 45 Intercept 14. Navigation NAV Mode Using a DG from ROL Mode, All Angle Intercept 16. Approach APR Mode Using a DG from HDG Mode, 45 Intercept 20.
Approach APR Mode Using a DG from ROL Mode, All Angle Intercept 22. Approach APR Mode Using an HSI 24, Back Course REV Mode Using a DG from HDG Mode. 45 Intercept 26, Back Course REV Mode Using a DG from ROL Mode. All Angle Intercept 28, Back Course REV Mode Using an HSI 30. Operations With The KAP 140 32, Takeoff And Climb To Assigned Altitude 32.
GPS Capture Using DG 34, GPS Capture Using HSI 36, Outbound On Front Course For Procedure Turn To LOC Approach. Using DG 38, Outbound On Front Course For Procedure Turn To LOC Approach. Using HSI 40, Front Course LOC Approach Using DG 42. Front Course LOC Approach Using HSI 44, Outbound on GPS Approach Using DG 46. Outbound on GPS Approach Using HSI 48, Inbound on GPS Approach Using DG 50.
Inbound on GPS Approach Using HSI 52, KAP 140 Two Axis Operation 55. System Operating Modes 57, Vertical Speed VS Mode 58. Altitude Hold ALT Mode 59, Operations With The KAP 140 60. Takeoff And Climb To Assigned Altitude 60, GPS Capture Using DG 62. Jun 98 KAP 140 AUTOPILOT SYSTEM i, Table of Contents.
GPS Capture Using HSI 64, Outbound On Front Course For Procedure Turn To ILS Approach. Using DG 66, Outbound On Front Course For Procedure Turn To ILS Approach. Using HSI 68, Front Course ILS Approach Using DG 70. Front Course ILS Approach Using HSI 72, Outbound on GPS Approach Using DG 74. Outbound on GPS Approach Using HSI 76, Inbound on GPS Approach Using DG 78.
Inbound on GPS Approach Using HSI 80, KAP 140 Two Axis with Altitude Preselect Operation 83. System Operating Modes 86, Vertical Speed VS Mode 86. Altitude Hold ALT Mode 87, Altitude Alerting and Preselect 88. Altitude Alerter 88, Altimeter Setting 88, Altitude Preselect 89. Voice Messaging 89, Operations With The KAP 140 90.
Takeoff And Climb To Assigned Altitude 90, GPS Capture Using DG 92. GPS Capture Using HSI 94, Outbound On Front Course For Procedure Turn To ILS Approach. Using DG 96, Outbound On Front Course For Procedure Turn To ILS Approach. Using HSI 98, Front Course ILS Approach Using DG 100. Front Course ILS Approach Using HSI 102, Outbound on GPS Approach Using DG 104.
Outbound on GPS Approach Using HSI 106, Inbound on GPS Approach Using DG 108. Inbound on GPS Approach Using HSI 110, KCS 55A Compass System 113. KI 525A Indicator 114, Description of Indicator and Display Functions 114. Slaving Meter KA 51B 116, KMT 112 Magnetic Slaving Transmitter 117. KG 102A Directional Gyro 117, Abnormal Circumstances 119.
Flight Procedures with the KCS 55A 120, Abnormal Procedures 127. Autopilot Malfunction 127, ii KAP 140 AUTOPILOT SYSTEM Jun 98. Introduction, Introduction, The KAP 140 Autopilot System is a Internal monitors keep constant track. rate based digital autopilot system of the KAP 140 s status and provide. offering smooth performance and for automatic shutdown of the. enhanced features found only in autopilot or trim system in the event. more expensive autopilots The first of a malfunction In addition to relia. of its type developed by AlliedSignal 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 AlliedSignal Service. cockpit Centers are located around the, world to provide assistance when. It is also significant that the KAP 140 ever necessary. series autopilots have been, designed from their inception to To fully realize the capability of your.
interface with the Silver Crown pack new panel mount digital autopilot. age of products Consider the system you must understand the. advantage of having your avionics performance capabilities and basic. working together as an integrated operational requirements of the sys. system rather than as a group of tem This pilot s guide provides. components built by several manu information to aid in this and is. factures divided up into six sections The first, section provides general familiariza. Your new KAP 140 roll axis features tion of each autopilot system includ. include wing leveler heading select ing the associated panel mounted. and VOR LOC intercept and track displays The second section. ing The KAP 140 can also be cou describes the KAP 140 Single Axis. pled to GPS and RNAV receivers as Autopilot System The third section. well Roll rate information is derived describes the KAP 140 Two Axis. from the turn coordinator Pitch axis Autopilot System The fourth section. features include vertical speed describes the KAP 140 Two. glideslope and altitude hold along Axis Altitude Preselect Autopilot. with the optional altitude preselect System The fifth section describes. Pitch information is derived from a the optional KCS 55A slaved com. pressure sensor and accelerometer pass system The Sixth section. The KAP 140 Autopilot System oper describes abnormal procedures. ates independent of the aircraft s, artificial horizon Therefore the. autopilot retains roll stabilization and, all vertical modes in the event of vac. uum system failure, Jun 98 KAP 140 AUTOPILOT SYSTEM 1. Introduction, General Description, 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. with an electric trim option, D C ELEC D C ELEC, TURN COORDINATOR TURN COORDINATOR. 2 MIN 2 MIN, NO PITCH NO PITCH, INFORMATION INFORMATION. GS GS GS GS, 30 24 30 24, KAP 140 KFC 140 ARM BARO. AP HDG NAV APR REV AP HDG NAV APR REV ALT DN, KAP 140 Two Axis.
Autopilot System, The KAP 140 Two Axis system pro, vides both lateral and vertical. TURN COORDINATOR, INFORMATION, AP HDG NAV APR REV ALT DN. 2 KAP 140 AUTOPILOT SYSTEM Jun 98, Introduction, KAP 140 KAP 140 KAP 140. Two Axis Alt Two Axis Single Axis, HSI Optional Optional Optional. DG Standard Standard Standard, Turn Coordinator Standard Standard Standard.
Automatic Electric Elevator Trim Optional Optional Optional. Manual Electric Trim Optional Optional Optional, FUNCTIONS MODES. ALT Hold ALT Yes Yes, ALT Preselect ALERT Yes, Heading Select HDG Yes Yes Yes. NAV VOR RNAV GPS Yes Yes Yes, Approach APR Yes Yes Yes. Glideslope GS Yes Yes, Back Course REV Yes Yes Yes. Control Wheel Steering CWS Optional Optional Optional. Vertical Speed Hld Yes Yes, Auto Capture Yes Yes Yes.
Auto Track Yes Yes Yes, All Angle Intercept Standard with Standard with Standard with. DG or optional DG or optional DG or optional, HSI HSI HSI. Auto 45 degree Intercept Standard Standard Standard. with DG only with DG only with DG only, Manual and Auto Trim Monitor Both Both Both. Acceleration Monitor Yes Yes, KAP 140 System Capabilities. Jun 98 KAP 140 AUTOPILOT SYSTEM 3, Introduction, System Integration.
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, vary slightly in order to optimize cer. tification and installation require, Each system has a number of.
inputs sensor outputs are shown in, red combination inputs are shown in. blue display outputs are shown in, orange and aircraft control shown in. green The systems diagrams, reflect that the KAP 140 systems. control both pitch and roll axes of the, 4 KAP 140 AUTOPILOT SYSTEM Jun 98. Introduction, Middle VOR LOC RNAV KC 140 Single Axis.
Marker GPS Deviation Computer Controller, Annunciator. D C ELEC contains computer, functions mode, TURN COORDINATOR. TRIM control buttons, L R AP HDG NAV APR REV, FAIL and annunciations. INFORMATION, in a single unit, Turn Coordinator, 3 KS 271C Roll Servo. 21 S 21 15, Directional Gyro KI 204 or other Course.
Deviation Indicator, Slaved DG KS 272C Pitch Trim, Servo Optional. KI 525A Pictorial KMT 112 Disconnect, Navigation Indicator Flux Detector Trim Interrupt. KCS 55A Slaved, Compass System CCW CW, Slaving Accessory. Control Manual, WheelSteering Electrical Trim, Optional Optional. KAP 140 Single Axis System Diagram, Jun 98 KAP 140 AUTOPILOT SYSTEM 5.
Introduction, VOR LOC RNAV Static KC 140 Two Axis, GPS Deviation Pressure Computer. Glideslope Middle Controller, Deviation Marker Annunciator. contains computer, D C ELEC functions mode, control buttons. TURN COORDINATOR KAP 140, TRIM and annunciations, L R AP HDG NAV APR REV ALT UP in a single unit. INFORMATION, Also contains, static pressure, Turn Coordinator sensor and.
accelerometer, KS 271C Roll Servo, 21 S 21 15, Directional Gyro KI 204 or other Course KS 270C Pitch Servo. Deviation Indicator, not included, KG102A KS 272C Pitch Trim Servo. KI 525A Pictorial KMT 112 Autopilot, Navigation Indicator Flux Detector Disconnect. Trim Interrupt, KCS 55A Slaved AUTO MAN, Compass System CCW CW. Slaving Accessory, Control Manual, WheelSteering Electrical Trim.
KAP 140 Two Axis System Diagram, 6 KAP 140 AUTOPILOT SYSTEM Jun 98. Introduction, Baro RNAV Encoding, Setting GPS Altimeter KC 140 Two Axis with. Deviation Altitude Preselect, Glideslope Middle Static Computer Controller. Deviation Marker Pressure Annunciator, contains computer. D C ELEC functions mode, control buttons, TURN COORDINATOR KFC 140 ARM BARO.
TRIM and annunciations, L R AP HDG NAV APR REV ALT DN in a single unit Also. INFORMATION, contains static pressure, sensor and accelerometer. Turn Coordinator, KS 271C Roll Servo, 21 S 21 15, Directional Gyro KI 204 or other Course KS 270C Pitch Servo. Deviation Indicator, not included, KG102A KS 272C Pitch Trim Servo. KI 525A Pictorial KMT 112 Autopilot, Navigation Indicator Flux Detector Disconnect.
Trim Interrupt, KCS 55A Slaved, Compass System, Slaving Accessory. Control Manual, WheelSteering Electrical Trim, KAP 140 Two Axis Altitude Preselect System Diagram. Jun 98 KAP 140 AUTOPILOT SYSTEM 7, Introduction, Power Application and Preflight Tests. AP HDG NAV APR REV, KAP 140 Preflight Test, AP HDG NAV APR REV. KAP 140 Preflight Test Complete, A preflight test is performed For two axis units only.
upon power application to the com, puter This test is a sequence of NOTE Following the preflight test. internal checks that validate proper the red P warning on the face of the. system operation prior to allowing autopilot may illuminate indicating. autopilot engagement The preflight that the pitch axis cannot be. test PFT sequence is indicated by engaged This condition should be. PFT with an increasing number for temporary lasting no more than 30. the sequence steps Successful seconds The P will extinguish and. completion of self test is identified by normal operation will be available. all display segments being illumi, nated Display Test and the discon If power to the autopilot is cycled in. nect tone sounding flight i e through the autopilot circuit. breaker for instance it is possible, that a 5 minute delay may be neces. sary prior to autopilot engagement to, allow the pitch axis accelerometer. circuit to stabilize Engagement prior, to stabilization may result in mildly.
erratic pitch axis behavior, 8 KAP 140 AUTOPILOT SYSTEM Jun 98. Single Axis Operation, KAP 140 Single Axis Operation. The KAP 140 is a high performance digital panel mounted autopilot sys. tem for light aircraft, AP HDG NAV APR REV, Single axis Flight Control Computer. KAP 140 Pilot s Guide Bendix King Autopilot System 006 18034 0000 Jun 98 a WARNING Information subject to the export control laws This document which includes any attachments and exhibits hereto contains information subject to International Traffic in Arms Regulation ITAR or Export Administration Regulation EAR of 1979 which may not be exported released or disclosed to foreign

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