Download Print this page
MilViz KAP 140 Pilot's Manual

MilViz KAP 140 Pilot's Manual

Pilatus pc6 porter

Advertisement

Quick Links

MILVIZ PILATUS PC6 PORTER
KAP 140 Autopilot system
(Sources: KAP 140 Pilot's guide – KAP 140 Installation Manual)
KAP 140 Two Axis with Altitude Preselect Operation - Introduction
The KAP 140 Autopilot System included in the Pilatus PC6 is a rate based digital autopilot
system offering smooth performance and enhanced features found only in more expensive
autopilots. This system brings digital technology and reliability into the light aircraft cockpit.
KAP 140 roll axis features include wing leveler, heading select and VOR/LOC intercept
and tracking. The KAP 140 can also be coupled to GPS and RNAV receivers as well. Roll
rate information is derived from the turn coordinator.
Pitch axis features include vertical speed, glideslope and altitude hold along with altitude
preselect option. Pitch information is derived from a pressure sensor and accelerometer.
Manual Electric Trim and Control Wheel Steering (CWS) optionals are also included and
full operative.
The KAP 140 Autopilot System operates independent of the aircraft's artificial horizon.
Therefore, the autopilot retains roll stabilization and all vertical modes in the event of
vacuum system failure.
KAP 140 features in Pilatus PC6 version
HSI unit
Turn Coordinator
Automatic Electric Elevator Trim
Manual Electric Trim
FUNCTION MODES
Control Wheel Steering (CWS)
Auto Capture
Auto Track
All Angle Intercept
Auto 45-degree Intercept
Remote Barometric Input
YES
YES
YES
YES
ALT Hold (ALT); ALT Preselect/ALERT; Heading Select (HDG);
NAV (VOR/RNAV/GPS); Approach (APR); Glideslope (GS);
Back Course (REV); Wing Leveler (ROL); Vertical Speed Hold (VS)
YES
YES
YES
YES
NO
NO
1

Advertisement

loading
Need help?

Need help?

Do you have a question about the KAP 140 and is the answer not in the manual?

Questions and answers

Summary of Contents for MilViz KAP 140

  • Page 1 This system brings digital technology and reliability into the light aircraft cockpit. KAP 140 roll axis features include wing leveler, heading select and VOR/LOC intercept and tracking. The KAP 140 can also be coupled to GPS and RNAV receivers as well. Roll rate information is derived from the turn coordinator.
  • Page 2 Diagram - KAP 140 Pilatus PC6 version systems 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...
  • Page 3 System Technical Characteristics (In smooth air) Maximum Bank Angles Limited to standard rate turn. Heading Stability ± 2° VOR Crosswind Compensation Up to 30° right or left NAV/APR/REV Capture Capability All angles NAV/APR/REV Capture Computation Scheduled by beam closure rate NAV Track Computation Scheduled by beam rate and deviation APR/REV Track Computation...
  • Page 4 Power Application and Preflight Tests KAP 140 Preflight Test KAP 140 Preflight Test Complete A preflight test is performed upon power application to the computer. This test is a sequence of internal checks that validate proper system operation prior to allowing autopilot engagement.
  • Page 5 KAP 140 Two Axis with Altitude Preselect Operation 1. PITCH AXIS, (P) ANNUNCIATOR - 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. 2. AUTOPILOT ENGAGE/DISENGAGE (AP) BUTTON - When pushed and held for 0.25 seconds, engages autopilot if all logic conditions are met.
  • Page 6 7. BACK COURSE APPROACH (REV) MODE SELECTOR BUTTON - When pushed, will arm the Back Course approach mode. This mode functions similarly to the approach mode except that the autopilot response to LOC signals is reversed, and GS is disabled. 8.
  • Page 7 14. ALTITUDE ALERT (ALERT) ANNUNCIATION - The ALERT annunciate is illuminated 1000 ft. prior to the selected altitude, extinguishes 200 ft. prior to the selected altitude and illuminates momentarily when the selected altitude is reached. Once the selected altitude is reached a flashing ALERT illumination signifies that the 200 ft.
  • Page 8 System Operating Modes Functions independent of autopilot status Altimeter setting Upon successful completion of preflight test, the baro display will flash. 1. BARO setting - Enter barometric setting using the rotary knobs OR if correct as displayed, press BARO. Note: triggering Barometric event (FS default key is B) will synchronize this unit’s baro setting with the Altimeter baro setting.
  • Page 9 Altitude Alerter 1. ALTITUDE SELECT knob - ROTATE until the desired altitude is displayed. Outer knob for 1,000 ft. changes; inner knob for 100 ft. changes. The ALERT annunciation is illuminated 1000 ft. prior to the selected altitude, extinguishes 200 ft. prior to the selected altitude and illuminates momentarily when the selected altitude is reached.
  • Page 10 System Operating Modes ROLL functions available with autopilot engaged Wing Leveler (ROL) Mode In the roll mode, the autopilot maintains wings level flight. 1. Engage autopilot – Press and hold AP for 0.25 seconds to engage the autopilot. Note ROL, VS and current vertical speed is displayed.
  • Page 11 Navigation (NAV) Mode from HDG Mode In the navigation (NAV) mode, the autopilot intercepts and tracks VOR/RNAV and GPS courses. To arm NAV mode (with the KAP 140 currently in the HDG mode): 1. Select the desired frequency for VOR or RNAV. For GPS, verify the desired waypoint or destination.
  • Page 12 Approach (APR) Mode from HDG Mode In the approach (APR) mode, the autopilot intercepts and tracks VOR/LOC/ILS and GPS courses. To arm APR mode (with the KAP 140 currently in the HDG mode): 1. Select the desired frequency for VOR or LOC/ILS.
  • Page 13 Back Course (REV) Mode from HDG Mode The back course (REV) mode allows the autopilot to intercept and track a localizer back course. To arm REV mode (with the KAP 140 currently in the HDG mode): 1. Select the desired frequency for LOC/ILS.
  • Page 14 5. If the Course Deviation Bar is greater than 2 to 3 dots the aircraft will continue in HDG mode (or ROL if HDG is not selected) with REV ARM annunciated; when the computed capture point is reached HDG (or ROL) will disengage, the ARM annunciator will go out and the selected course will be automatically captured and tracked.
  • Page 15 The Vertical Speed (VS) mode allows variable vertical speed climbs and descents. The ALT button toggles between Altitude Hold (ALT) and Vertical Speed (VS) modes. Note: The KAP 140 engages into VS mode as a default. To operate in the VS mode (with autopilot currently disengaged): 1.
  • Page 16 The Altitude Preselect function allows capturing of a desired altitude and transferring into Altitude Hold (ALT). 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...
  • Page 17 Altitude Preselect 1. ALTITUDE SELECT knob - ROTATE until desired altitude is displayed. ARM annunciation occurs automatically upon altitude selection when the autopilot is engaged. 2. Airplane - ESTABLISH desired vertical speed to intercept the selected altitude. 3. Upon altitude capture, ALT ARM will extinguish and ALT will be annunciated. Altitude Arm To arm the capture of the current preselected altitude: 1.
  • Page 18 2. Airplane - ESTABLISH desired vertical speed to intercept the selected altitude. 3. Upon altitude capture, ALT ARM will extinguish and ALT will be annunciated. Note: Altitude preselect captures are not recommended on non-precision approaches to capture the MDA. Glideslope coupling will preclude an altitude capture on an ILS. 4.
  • Page 19 Autopilot disconnect When pressed disengages the autopilot or interrupt pitch trim travel if MET is being operated. Note: Pressing the button with autopilot disengaged or/MET not active produces no effect. FSim Technical Reference Standard captured Events: - AP button = AP_MASTER (default Z key- Hold for engage) - HDG button = AP_HDG_HOLD (default Ctrl-H keys) - NAV button = AP_NAV1_HOLD (default Ctrl-N keys) - APR button = AP_APR_HOLD (default Ctrl-A keys)