4/29/2023 0 Comments Kap 45 setup bo4![]() This mode functions similarly to the approach mode except that the autopilot response to LOC signals is reversed, and GS is disabled. When pushed, will arm the Back Course approach mode. BACK COURSE APPROACH ( REV) MODE SELECTOR BUTTON.APR mode is recommended for instrument approaches. ![]() This mode provides automatic beam capture and tracking of VOR, GPS, LOC, and Glideslope (GS) on an ILS, as selected for presentation on the HSI or CDI. NAV mode may also be used for front course LOC tracking when GS tracking is not desired. NAV mode is recommended for enroute navigation tracking. The mode provides automatic beam capture and tracking of VOR, LOC or GPS as selected for presentation on the HSI or CDI. When pushed, will arm the navigation mode. This button will engage the autopilot in units with software prior to software version 03/01. Button can also be used to toggle between HDG and ROL modes. A new heading may be selected at any time and will result in the airplane turning to the new heading. When pushed, will arm the Heading mode, which commands the airplane to turn to and maintain the heading selected by the heading bug on either the DG or HSI. When illuminated, indicates failure of the roll axis and will disengage the autopilot and not allow engagement. For software version 03/01 and later, the AP button must be pressed and held for 0.25 seconds to engage the autopilot. ![]() When pressed again, will disengage the autopilot. The captured VS will be the vertical speed present at the moment of AP button press. The commanded vertical speed is displayed in the upper right corner of autopilot display area for three seconds after engagement or if either the UP or DN button is pressed. The autopilot will engage in the basic roll ( ROL) mode which functions as a wing leveler and in the vertical speed ( VS) hold mode. When pushed, engages the autopilot if all logic conditions are met. AUTOPILOT ENGAGE/DISENGAGE ( AP) BUTTON.When illuminated, indicates failure of the pitch axis and will disengage the autopilot when the failure occurs and not allow engagement of the pitch axis. The KAP 140 is a digital, panel-mounted autopilot system for light aircraft. KAP 140 Two Axis with Altitude Preselect Operation The software and hardware may be used or copied only in accordance with the terms of the license agreement. The software and hardware described in this document are provided under a license agreement. The information in this manual is subject to change without notice and does not represent a commitment on the part of the licensor. Its only purpose is to introduce the hardware and software to enable a pilot to use the system. This manual is in no respect a tutorial in visual flight, instrument flight or navigation. The reader of this manual is expected to know how to fly an aircraft or to be participating in a structured and approved flight training program.
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