A 2 axis version is standard and a 3 axis version is available with an optional yaw damper. KAP 140 Bendix/King® Autopilot System Pilot’s Guide WARNING The enclosed technical data is eligible for export under License Designation NLR and is to be used solely by the individual/organization to whom it is addressed. Autopilot functionsĪltitude pre-select/alerter, GPS/ILS/VOR tracking and approaches. The optional KAP 235 is designed to replace existing KA-185/KA-285 legacy annunciators on installations that will not allow the KMC 231 Mode Controller to be in the pilot’s normal field of view. HSI interfaces can be through a digital data bus or analog using a KI 525A compatible legacy interface. AirData input is provided through a digital data bus. NAV VOR/ILS/GPS sources can be interfaced via a digital data bus or analog. AttitudeĪttitude input comes from a digital attitude source provided by the KI 300 primary attitude indicator or another approved digital attitude source. With a unique mechanical design the KMC 231 seamlessly integrates with the AeroCruze computer, allowing it to fit in the same mechanical location of the panel mounted KFC 150 autopilot flight computer. The KMC 231 Mode Controller provides the pilot control and annunciation functions via a glove friendly, color LCD touch screen with dedicated controls for frequent tasks. The AeroCruze has also been designed to be remote mounted to accommodate KFC 200 and 250 installations. This unit is designed to fit within the existing form factor of the legacy KFC 150 flight computer. The AeroCruze Flight Computer is the heart of the AeroCruze system. 116 KMT 112 Magnetic Slaving Transmitter. 114 Description of Indicator and Display Functions. 96 Outbound On Front Course For Procedure Turn To ILS Approach Using HSI. 94 Outbound On Front Course For Procedure Turn To ILS Approach Using DG. 90 Takeoff And Climb To Assigned Altitude. 80 KAP 140 Two Axis with Altitude Preselect Operation. 66 Outbound On Front Course For Procedure Turn To ILS Approach Using HSI. 64 Outbound On Front Course For Procedure Turn To ILS Approach Using DG.
38 Outbound On Front Course For Procedure Turn To LOC Approach Using HSI. 36 Outbound On Front Course For Procedure Turn To LOC Approach Using DG. 32 Takeoff And Climb To Assigned Altitude. 26 Back Course (REV) Mode Using a DG from ROL Mode (All Angle Intercept). 24 Back Course (REV) Mode Using a DG from HDG Mode (45° Intercept). 20 Approach (APR) Mode Using a DG from ROL Mode (All Angle Intercept). 16 Approach (APR) Mode Using a DG from HDG Mode (45° Intercept). 14 Navigation (NAV) Mode Using a DG from ROL Mode (All Angle Intercept). 13 Navigation (NAV) Mode Using a DG from HDG Mode (45° Intercept). 2 KAP 140 Two Axis/Altitude Preselect Autopilot System. This is the original version of this publication.
Bendix king kap 140 autopilot manual software#
This revision incorporates changes for software version 03/01. This revision makes some of the changes for software version 03/01 more consistent throughout the Pilot’s Guide.
This revision changes CW to CCW on page 116. For further information contact Aerospace Technical Publications Honeywell One Technology Center 23500 West 105th Street Olathe, Kansas 66061. Reproduction of this publication or any portion thereof by any means without the express written permission of Honeywell International Inc.
law is prohibited.ĬOPYRIGHT NOTICE Copyright © 1998, 2002, 2005 Honeywell International Inc. WARNING The enclosed technical data is eligible for export under License Designation NLR and is to be used solely by the individual/organization to whom it is addressed.