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Honeywell KAP 140 Pilot'S Manual Download Page 63

KAP 140 AUTOPILOT SYSTEM

Two Axis Operation

55

Rev. 2
May/02

KAP 140 Two Axis Operation

The KAP 140 is a digital, panel-mounted autopilot system for light air-

craft.

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/DISEN-
GAGE (AP) BUTTON  -  When
pushed,  engages autopilot if all logic
conditions are met.  The autopilot
will engage in the basic roll (ROL)
mode which functions as a wing lev-
eler and in the vertical speed (VS)
hold mode.  The commanded verti-
cal speed will be displayed in the
upper right corner of autopilot dis-
play area.  The captured VS will be
the vertical speed present at the
moment of AP button press.  When
pressed again, will disengage the
autopilot. For software version 03/01

AP

G

KAP 140

HDG

NAV

APR

REV

ALT

DN

UP

AP

G

KAP 140

HDG

NAV

APR

REV

ALT

DN

UP

P    R

P    R

1

2

4

5

6

7

8

9

3

13

12

11

Full Two-Axis KAP 140 Display

Two-axis Flight Control Computer

10

14

and later, the AP button must be
pressed and held for 0.25 seconds
to engage the autopilot.

3. ROLL AXIS (R) ANNUNCIATOR
-  When illuminated, indicates failure
of the roll axis and will disengage the
autopilot and not allow engagement.

4. HEADING (HDG) MODE SELEC-
TOR BUTTON  -  When pushed, will
arm the Heading mode, which com-
mands the airplane to turn to and
maintain the heading selected by the
heading bug on either the DG or
HSI.  A new heading may be
selected at any time and will result in
the airplane turning to the new head-
ing.  Button can also be used to tog-
gle between HDG and ROL modes.
This button will engage the autopilot
in units with software prior to soft-
ware version 03/01.

Summary of Contents for KAP 140

Page 1: ...KAP 140 Pilot s Guide Bendix King Autopilot System Rev 2 May 02 N 006 18034 0000 ...

Page 2: ...onal Inc 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 Kansas 66061 Telephone 913 782 0400 ...

Page 3: ... Manual KAP 140 Pilot s Guide Revision 2 May 2002 Part Number 006 18034 0000 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 ...

Page 4: ...R 2 Revision History and Instructions Manual KAP 140 Pilot s Guide Revision 1 April 2002 Part Number 006 18034 0000 This revision incorporates changes for software version 03 01 ...

Page 5: ...R 3 Revision History and Instructions Manual KAP 140 Pilot s Guide Revision 0 June 1998 Part Number 006 18034 0000 This is the original version of this publication ...

Page 6: ...R 4 This page intentionally left blank ...

Page 7: ... 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 Fo...

Page 8: ...ing 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 Outbou...

Page 9: ...KAP 140 Autopilot System oper 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 Internal monitors keep constant track of the KAP 140 s status and provide for automatic shutdown of the autopilot or trim system in the event of a malfunction In addition to relia bility the KAP 140 is d...

Page 10: ...40 Two Axis Altitude Preselect Autopilot System The KAP 140 Two Axis system pro vides both lateral and vertical modes with altitude preselect L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 33 3 0 W 2 4 2 1 S 1 5 1 2 E 6 3 ı AP G KAP 140 HDG NAV APR REV ALT DN UP L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 3 3 3 0 W 2 4 2 1 S 1 5 12 E 6 3 ı AP G KFC 140 HDG NA...

Page 11: ...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 DG or optional HSI Standard with DG or optional HSI Standard with DG or optional HSI Auto 45 degree In...

Page 12: ... Altitude Preselect systems The actual com ponents on individual systems may vary slightly in order to optimize cer tification and installation require ments 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...

Page 13: ...ndicator VOR LOC RNAV GPS Deviation Middle Marker KC 140 Single Axis Computer Controller Annunciator contains computer functions mode control buttons and annunciations in a single unit KS 271C Roll Servo KS 272C Pitch Trim Servo Optional KI 525A Pictorial Navigation Indicator KCS 55A Slaved Compass System Optional KG102A Slaved DG KMT 112 Flux Detector OR KA 51B Slaving Accessory Manual Electrical...

Page 14: ... included KC 140 Two Axis Computer Controller Annunciator contains computer functions mode control buttons and annunciations in a single unit Also contains static pressure sensor and accelerometer KS 271C Roll Servo KS 270C Pitch Servo KS 272C Pitch Trim Servo KI 525A Pictorial Navigation Indicator KCS 55A Slaved Compass System Optional KG102A Slaved DG KMT 112 Flux Detector OR KA 51B Slaving Acce...

Page 15: ... contains computer functions mode control buttons and annunciations in a single unit Also contains static pressure sensor and accelerometer KS 271C Roll Servo KS 270C Pitch Servo KS 272C Pitch Trim Servo KI 525A Pictorial Navigation Indicator KCS 55A Slaved Compass System Optional KG102A Slaved DG KMT 112 Flux Detector OR KA 51B Slaving Accessory Manual Electrical Trim Autopilot Disconnect Trim In...

Page 16: ... units only NOTE Following the preflight test the red P warning on the face of the autopilot may illuminate indicating that the pitch axis cannot be engaged This condition should be temporary lasting no more than 30 seconds The P will extinguish and normal operation will be available NOTE The red P warning may illu minate when the autopilot is not engaged This can occur when autopilot G limits hav...

Page 17: ...ds to engage the autopilot 2 ROLL AXIS R ANNUNCIATION When illuminated indicates failure of the roll axis and will disengage the autopilot and not allow engagement 3 HEADING HDG MODE SELEC TOR BUTTON When pushed will select 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 A new heading may be selected at any time a...

Page 18: ...rm the Back Course approach mode This mode functions similarly to the approach mode except that the autopilot response to LOC signals is reversed 7 ROLL MODE DISPLAY Displays the active and armed roll modes ROL HDG NAV ARM NAV APR ARM APR REV ARM REV Also displayed will be flash ing AP annunciation 5 seconds at each autopilot disconnect accompa nied by an aural tone for 2 sec onds 8 AUTOPILOT ENGA...

Page 19: ...KAP 140 AUTOPILOT SYSTEM Single Axis Operation 11 Rev 1 Apr 02 This page intentionally left blank ...

Page 20: ... KAP 140 HDG NAV APR REV Wing Leveler ROL Mode In the roll mode the autopilot maintains wings level flight 1 Engage autopilot Press AP For software version 03 01 and later the AP button must be pressed and held for 0 25 seconds to engage the autopilot NOTE The KAP 140 engages into ROL mode as a default System Operating Modes ...

Page 21: ... desired heading on the DG or HSI using the Heading Select knob 2 Engage autopilot Press AP For software version 03 01 and later the AP button must be pressed and held for 0 25 seconds to engage the autopilot 3 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 4 If you move the hea...

Page 22: ...ode 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 destina tion 2 OBS Knob SELECT desired course 3 NAV Mode Selector Button PRESS Note NAV ARM annunci ated NOTE When NAV is selected the autopilot will flash HDG for 5 sec onds to remind the p...

Page 23: ... 5 If the Course Deviation Bar is greater than 2 to 3 dots the autopilot will annunciate NAV ARM when the computed capture point is reached the ARM annun ciator will go out and the selected course will be automatically cap tured and tracked 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 ...

Page 24: ...cks VOR RNAV and GPS courses To arm NAV mode with the KAP 140 currently in the ROL mode 1 Maneuver the aircraft to the desired intercept angle prior to selecting ROL mode 2 Select the desired frequency for VOR or RNAV For GPS verify the desired waypoint or destina tion 3 OBS Knob SELECT desired course 4 NAV Mode Selector Button PRESS Note NAV ARM annunci ated NOTE When NAV is selected the autopilo...

Page 25: ...nnunciate NAV ARM when the computed capture point is reached the ARM annun ciator will go out and the selected course will be automatically cap tured and tracked If the D Bar is less than 2 to 3 dots the ROL mode will disengage upon select ing NAV mode the NAV annunci ator will illuminate and the capture track sequence will automatically begin Note Intercept angles greater than 45 can result in co...

Page 26: ... HSI 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 destina tion 2 Course Bearing Pointer SET to desired course 3 Heading Selector Knob SET BUG to provide desired intercept angle 4 NAV Mode Selector Button PRESS No...

Page 27: ...ll be automatically captured and tracked If the D Bar is less than 2 to 3 dots the HDG mode or ROL if HDG is not selected will disen gage upon selecting NAV mode the NAV 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 to the station Therefore intercept angles greater than 45 are not...

Page 28: ...d track LOC VOR RNAV and GPS courses To arm APR mode with the KAP 140 currently in the HDG mode 1 Select the desired frequency for LOC VOR or RNAV For GPS verify the desired approach 2 OBS Knob SELECT desired approach course For a localizer set it to serve as a memory aid 3 APR Mode Selector Button PRESS Note APR ARM annun ciated NOTE When APR is selected the autopilot will flash HDG for 5 sec ond...

Page 29: ...course 5 If the Course Deviation Bar is greater than 2 to 3 dots the autopilot will annunciate APR ARM when the computed capture point is reached the ARM annun ciator will go out and the selected course will be automatically cap tured and tracked 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 seq...

Page 30: ... To arm APR mode with the KAP 140 currently in the ROL mode 1 Maneuver the aircraft to the desired intercept angle prior to selecting ROL mode 2 Select the desired frequency for LOC VOR or RNAV For GPS verify the desired approach 3 OBS Knob SELECT desired approach course For a localizer set it to serve as a memory aid 4 APR Mode Selector Button PRESS Note APR ARM annun ciated NOTE When APR is sele...

Page 31: ...will annunciate APR ARM when the computed capture point is reached the ARM annun ciator will go out and the selected course will be automatically cap tured and tracked If the D Bar is less than 2 to 3 dots the ROL mode will disengage upon select ing APR mode the APR annunci ator will illuminate and the capture track sequence will automatically begin Note Intercept angles greater than 45 can result...

Page 32: ...n HSI The Approach APR mode allows the autopilot to intercept and track LOC VOR RNAV and GPS courses To arm APR mode with the KAP 140 currently in the HDG mode 1 Select the desired frequency for LOC VOR or RNAV For GPS verify the desired approach 2 Course Bearing Pointer SET to desired course 3 Heading Selector Knob SET BUG to provide desired intercept angle 4 APR Mode Selector Button PRESS Note A...

Page 33: ...isen gage the ARM annunciator will go out and the selected course will be automatically captured and tracked If the D Bar is less than 2 to 3 dots the HDG mode or ROL if HDG is not selected will disen gage upon selecting APR mode the 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 clo...

Page 34: ...rse 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 2 OBS Knob SELECT front course inbound heading 3 REV Mode Selector Button PRESS Note REV ARM annun ciated NOTE When REV is selected the autopilot will flash HDG for 5 sec onds to remind the pilot to reset the HDG bug to t...

Page 35: ...k course 5 If the Course Deviation Bar is greater than 2 to 3 dots the autopilot will annunciate REV ARM when the computed capture point is reached the ARM annun ciator will go out and the selected course will be automatically cap tured and tracked 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 s...

Page 36: ...ntercept and track a localizer back course To arm REV mode with the KAP 140 currently in the ROL mode 1 Maneuver the aircraft to the desired intercept angle prior to selecting ROL mode 2 Select the desired frequency for LOC 3 OBS Knob SELECT front course inbound heading 4 REV Mode Selector Button PRESS Note REV ARM annunci ated NOTE When REV is selected the autopilot will flash HDG for 5 sec onds ...

Page 37: ...t will annunciate REV ARM when the computed capture point is reached the ARM annun ciator will go out and the selected course will be automatically cap tured and tracked 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 Note Intercept angles greater than 45 can resu...

Page 38: ...REV Mode Using an HSI 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 2 Course Bearing Pointer SET to the FRONT COURSE inbound heading 3 Heading Selector Knob SET BUG to provide desired intercept angle 4 REV Mode Selector Button PRESS Note REV ARM annunci a...

Page 39: ...isen gage the ARM annunciator will go out and the selected course will be automatically captured and tracked If the D Bar is less than 2 to 3 dots the HDG mode or ROL if HDG is not selected will disen gage upon selecting REV mode the 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 clo...

Page 40: ...OPERATIONS WITH THE KAP 140 Takeoff And Climb To Assigned Altitude 1 The aircraft is well off the ground and estab lished at a desired climb rate 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 Note Press and hold the AP button fo...

Page 41: ...N TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 33 3 0 W 2 4 2 1 S 1 5 1 2 E 6 3 ı AP G KAP 140 HDG NAV APR REV N 33 3 0 W 2 4 2 1 S 1 5 1 2 E 6 3 P U S H PUSH OR N 080 0 1 0 1 2 3 4 3 The autopilot is responding to the heading select mode with a left bank 4 The autopilot has completed the turn and is now established on a 010 heading Note The autopilot controls only the roll axis The PILO...

Page 42: ...e 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 GPS Capture Using DG L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV N 33 3 0 W 2 4 2 1 S 1 5 1 2 E 6 3 P U S H PUSH TO FR N S E W 3 3 3 0 2 4 2 1 1 5 12 6 3 OBS GS ı L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D...

Page 43: ...he autopilot is track ing the GPS course L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV N 3 3 30 W 2 4 21 S 1 5 12 E 6 3 P U S H PUSH TO FR N S E W 3 3 30 2 4 21 1 5 12 6 3 OBS GS ı L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV N 3 3 30 W 2 4 21 S 1 5 12 E 6 3 P U S H PUSH TO FR N S E W 3 3 30 2 4 21 1 5 12 6 3 OBS GS ı...

Page 44: ...tton is depressed and NAV ARM is annunciated GPS Capture Using HSI L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 33 3 0 W 2 4 2 1 S 1 5 1 2 E 6 3 ı AP G KAP 140 HDG NAV APR REV L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 33 3 0 W 2 4 2 1 S 1 5 1 2 E 6 3 ı AP G KAP 140 HDG NAV APR REV Description of GPS operation based on Bendix King GPS receiver Others may r...

Page 45: ...itiated by the autopilot 4 The turn is complete and the autopilot is track ing the GPS course L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 3 3 30 W 2 4 21 S 1 5 12 E 6 3 ı AP G KAP 140 HDG NAV APR REV L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 3 3 30 W 2 4 21 S 1 5 12 E 6 3 ı AP G KAP 140 HDG NAV APR REV N 1 2 3 4 4 0 0 1 0 ...

Page 46: ...e is automatically activated and a left turn outbound on the localizer is initiated by the autopilot Note The left right deviations of the CDI course deviation needle are reversed you must turn right to center a deviation of the index to the left This needle reversing takes place because you are fly ing outbound on a front course Outbound On Front Course For Procedure Turn To LOC Approach Using DG...

Page 47: ...eading This 103 heading will intercept the front course of 058 You must now select the approach mode by depressing the APR button on the KAP 140 While the HDG annunciation is flashing move the heading bug to the front course 058 Since the 45 intercept is 103 the aircraft will not turn until the front course is captured L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV A...

Page 48: ...nt is reached HDG mode is cancelled and reverse localizer mode is automatically activated and a left turn outbound on the localizer is initiated by the autopilot Note The left right deviations of the HSI course needle operate just as though you were flying a front course approach Outbound On Front Course For Procedure Turn To LOC Approach Using HSI L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D...

Page 49: ...Now you have reset the heading bug to 103 and made a 180 turn to this heading The 103 heading will intercept the front course of 058 You must now select the approach mode by depressing the APR button on the KAP 140 Automatic capture of the localizer will occur L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 3 3 30 W 24 2 1 S 1 5 1 2 E 6 3 ı AP G KAP 140 HDG NAV APR REV L R 2 MIN T...

Page 50: ... The autopilot will make the bank changes as neces sary to maintain localizer L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV N 3 3 3 0 W 2 4 2 1 S 1 5 12 E 6 3 P U S H PUSH TO FR N S E W 33 3 0 24 2 1 15 1 2 6 3 OBS GS ı L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV N 33 3 0 W 24 2 1 S 15 1 2 E 6 3 P U S H PUSH TO FR N ...

Page 51: ...sing 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 Note Press and hold the AP button for 0 25 seconds to engage the autopilot applicable only to software version 03 01 and later L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV N 33 3 0 W 24 2 1 S 15 1 2 E 6 3 P U S H PUSH TO FR N S E W 33...

Page 52: ... will center 2 The autopilot is following the localizer The autopilot will make bank changes as necessary to maintain localizer L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 3 3 3 0 W 2 4 2 1 S 1 5 12 E 6 3 ı AP G KAP 140 HDG NAV APR REV L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 33 3 0 W 24 2 1 S 15 1 2 E 6 3 ı AP G KAP 140 HDG NAV APR REV Front Course LOC...

Page 53: ...f 090 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 Note Press and hold the AP button for 0 25 seconds to engage the autopilot applicable only to software version 03 01 and later L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 33 3 0 W 24 2 1 S 15 1 2 E 6 3 ı AP G KAP 140 HDG NAV APR REV L R 2 ...

Page 54: ... turn to track the 238 GPS course Outbound on GPS Approach Using DG L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV ALT N 3 3 30 W 24 2 1 S 1 5 1 2 E 6 3 P U S H PUSH TO FR N S E W 3 3 30 24 2 1 1 5 1 2 6 3 OBS GS ı L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV ALT N 33 3 0 W 24 21 S 15 1 2 E 6 3 P U S H PUSH TO FR N S E...

Page 55: ...PS s Leg OBS mode switching is set to Leg mode and the OBS is set to 058 Select approach mode by depressing the APR button The HDG annunciation will flash for five sec onds then extinguish While the HDG annuncia tion is flashing move the heading bug to 058 Since the 45 intercept is 103 the aircraft will not turn until the course is captured L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC ...

Page 56: ...o OBS mode The autopilot ini tiates a left turn to track the 238 GPS course L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 3 3 30 W 24 2 1 S 1 5 1 2 E 6 3 ı AP G KAP 140 HDG NAV APR REV ALT L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 33 3 0 W 24 21 S 15 1 2 E 6 3 ı AP G KAP 140 HDG NAV APR REV ALT Outbound on GPS Approach Using HSI Description of GPS operatio...

Page 57: ...ug has been set to 103 and the aircraft has made a left turn to this heading The GPS s Leg OBS mode switching is set to Leg mode and the course pointer is set to 058 Select approach mode by depressing the APR button L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 3 3 30 W 24 2 1 S 1 5 1 2 E 6 3 ı AP G KAP 140 HDG NAV APR REV ALT L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ...

Page 58: ...sary to maintain the GPS course Inbound on GPS Approach Using DG L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV ALT N 3 3 3 0 W 2 4 2 1 S 1 5 12 E 6 3 P U S H PUSH TO FR N S E W 33 3 0 24 2 1 15 1 2 6 3 OBS GS ı L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV ALT N 33 3 0 W 24 2 1 S 15 1 2 E 6 3 P U S H PUSH TO FR N S E W...

Page 59: ...ng of 090 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 Note Press and hold the AP button for 0 25 seconds to engage the autopilot applicable only to software version 03 01 and later L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV ALT N 33 3 0 W 24 2 1 S 15 1 2 E 6 3 P U S ...

Page 60: ...e The autopilot will make the bank changes as neces sary to maintain the GPS course Inbound on GPS Approach Using HSI Description of GPS operation based on Bendix King GPS receiver Others may require different operation L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 3 3 3 0 W 2 4 2 1 S 1 5 12 E 6 3 ı AP G KAP 140 HDG NAV APR REV ALT L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION...

Page 61: ...b The heading bug is set to the missed approach heading of 090 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 Note Press and hold the AP button for 0 25 seconds to engage the autopilot applicable only to software version 03 01 and later L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 33 3 0 W 24...

Page 62: ...Single Axis Operation 54 KAP 140 AUTOPILOT SYSTEM Rev 1 Apr 02 This page intentionally left blank ...

Page 63: ... button press When pressed again will disengage the autopilot For software version 03 01 AP G KAP 140 HDG NAV APR REV ALT DN UP AP G KAP 140 HDG NAV APR REV ALT DN UP P R P R 1 2 4 5 6 7 8 9 3 13 12 11 Full Two Axis KAP 140 Display Two axis Flight Control Computer 10 14 and later the AP button must be pressed and held for 0 25 seconds to engage the autopilot 3 ROLL AXIS R ANNUNCIATOR When illumina...

Page 64: ...ssed with an estab lished VS rate present there will be altitude overshoot approximately 10 of the VS rate with the air plane returned positively to the refer ence altitude This button will engage the autopilot in units with software prior to software version 03 01 9 VERTICAL TRIM UP DN BUT TONS The action of these buttons is dependent upon the vertical mode present when pressed If VS mode is acti...

Page 65: ...ion 5 sec onds at each autopilot disconnect accompanied by an aural tone for 2 seconds 14 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 The lateral modes HDG NAV APR and REV operate identically as described in the KAP 140 Single Axis Operating Modes sec...

Page 66: ...elect desired climb or descent rate Each button stroke will increment the vertical speed commanded up or down by 100 ft min per button press or at the rate of approxi mately 300 ft min per second if held continuously To initiate a climb or descent from Altitude Hold ALT mode 1 ALT button Press Note ALT changes to VS and current vertical speed is displayed 2 UP or DN button Select desired climb or ...

Page 67: ...e ALT mode with autopilot currently in the Vertical Speed mode 1 ALT button Press Note ALT is annunciated and autopilot maneuvers to maintain pressure altitude acquired at button selec tion 2 UP or DN button Select to change altitude Incremented but ton strokes will move the refer ence altitude by 20 feet per press or if held continuously will com mand a 500 ft min altitude change acquiring a new ...

Page 68: ... the autopilot applicable only to software version 03 01 and later 2 The heading bug on the DG or HSI is turned to the new desired heading of 010 and the aircraft begins to respond with an immediate left turn 1 2 3 4 L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 3 3 3 0 W 2 4 2 1 S 1 5 12 E 6 3 ı AP G KAP 140 HDG NAV APR REV ALT DN UP N 3 3 3 0 W 2 4 2 1 S 1 5 12 E 6 3 P U S H P...

Page 69: ...altitude has been reached altitude hold ALT has been engaged and the aircraft maintains the reference altitude N 080 0 1 0 1 2 3 4 L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 3 3 30 W 2 4 21 S 1 5 12 E 6 3 ı AP G KAP 140 HDG NAV APR REV ALT DN UP N 3 3 30 W 2 4 21 S 1 5 12 E 6 3 P U S H PUSH OR L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 33 3 0 W 2 4 2 1 S...

Page 70: ...nnunciation is flashing move the heading bug to the desired course of 040 The aircraft will remain wings level until the capture point GPS Capture Using DG L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV ALT DN UP N 33 3 0 W 2 4 2 1 S 1 5 1 2 E 6 3 P U S H PUSH TO FR N S E W 3 3 3 0 2 4 2 1 1 5 12 6 3 OBS GS ı L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D ...

Page 71: ...t is track ing the GPS course L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV ALT DN UP N 3 3 30 W 2 4 21 S 1 5 12 E 6 3 P U S H PUSH TO FR N S E W 3 3 30 2 4 21 1 5 12 6 3 OBS GS ı L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV ALT DN UP N 3 3 30 W 2 4 21 S 1 5 12 E 6 3 P U S H PUSH TO FR N S E W 3 3 30 2 4 21 1 5 12 6 3...

Page 72: ...ressed and NAV ARM is annunciated GPS Capture Using HSI L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 33 3 0 W 2 4 2 1 S 1 5 1 2 E 6 3 ı AP G KAP 140 HDG NAV APR REV ALT DN UP L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 33 3 0 W 2 4 2 1 S 1 5 1 2 E 6 3 ı AP G KAP 140 HDG NAV APR REV ALT DN UP Description of GPS operation based on Bendix King GPS receiver Oth...

Page 73: ...urn is initiated by the autopilot 4 The turn is complete and the autopilot is track ing the GPS course L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 3 3 30 W 2 4 21 S 1 5 12 E 6 3 ı AP G KAP 140 HDG NAV APR REV ALT DN UP L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 3 3 30 W 2 4 21 S 1 5 12 E 6 3 ı AP G KAP 140 HDG NAV APR REV ALT DN UP ...

Page 74: ...elled and reverse localizer mode is automatically activated and a left turn outbound on the localizer is initiated by the autopilot Note The left right deviations of the CDI course deviation needle are reversed you must turn right to center a deviation of the index to the left This needle reversing takes place because you are fly ing outbound on a front course Outbound On Front Course For Procedur...

Page 75: ... 103 heading will intercept the front course of 058 You must now select the approach mode by depressing the APR button on the KAP 140 The HDG annunciation will flash for five sec onds then extinguish While the HDG annuncia tion is flashing move the heading bug to the front course 058 Since the 45 intercept is 103 the aircraft will not turn until the front course is captured L R 2 MIN TURN COORDINA...

Page 76: ...is reached HDG mode is cancelled and reverse localizer mode is automatically activated and a left turn outbound on the localizer is initiated by the autopilot Note The left right deviations of the HSI course needle operate just as though you were flying a front course approach Outbound On Front Course For Procedure Turn To ILS Approach Using HSI L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ...

Page 77: ...d heading of 283 4 Now you have reset the heading bug to 103 and made a 180 turn to this heading The 103 heading will intercept the front course of 058 You must now select the approach mode by depressing the APR button on the KAP 140 Automatic capture of the localizer will occur L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 3 3 30 W 24 2 1 S 1 5 1 2 E 6 3 ı AP G KAP 140 HDG NAV ...

Page 78: ...tor extinguishes and GS is displayed The autopilot will make pitch and bank changes as necessary to maintain localizer and glides lope L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV ALT DN UP N 33 3 0 W 24 2 1 S 15 1 2 E 6 3 P U S H PUSH TO FR N S E W 33 3 0 24 2 1 15 1 2 6 3 OBS GS ı L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG N...

Page 79: ...d modes commencing a right turn to a heading of 090 and maintaining the rate of climb existing at engagement Note Press and hold the AP button for 0 25 seconds to engage the autopilot applicable only to software version 03 01 and later L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV ALT DN UP N 33 3 0 W 24 2 1 S 15 1 2 E 6 3 P U S H PUSH TO FR N S E W 33 3 0 2...

Page 80: ...needle is at midscale Altitude hold is automatically disen gaged when the glideslope is captured The ALT annunciator extinguishes and GS is displayed The autopilot will make pitch and bank changes as necessary to maintain localizer and glides lope L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 33 3 0 W 24 2 1 S 15 1 2 E 6 3 ı AP G KAP 140 HDG NAV APR REV ALT DN UP L R 2 MIN TURN ...

Page 81: ...ding of 090 By depressing the HDG button on the KAP 140 the autopilot engages into the head ing and vertical speed modes commencing a right turn to a heading of 090 and maintaining the rate of climb existing at engagement Note Press and hold the AP button for 0 25 seconds to engage the autopilot applicable only to software version 03 01 and later L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C...

Page 82: ...o track the 238 GPS course Outbound on GPS Approach Using DG L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV ALT DN UP N 3 3 30 W 24 2 1 S 1 5 1 2 E 6 3 P U S H PUSH TO FR N S E W 3 3 30 24 2 1 1 5 1 2 6 3 OBS GS ı L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV ALT DN UP N 33 3 0 W 24 21 S 15 1 2 E 6 3 P U S H PUSH TO FR ...

Page 83: ...ode and the OBS is set to 058 Select approach mode by depressing the APR button 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 L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV ALT DN UP N 3 3 30 W 24 2 1 S 1 5 ...

Page 84: ...de The autopilot ini tiates a left turn to track the 238 GPS course L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 3 3 30 W 24 2 1 S 1 5 1 2 E 6 3 ı AP G KAP 140 HDG NAV APR REV ALT DN UP L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 33 3 0 W 24 21 S 15 1 2 E 6 3 ı AP G KAP 140 HDG NAV APR REV ALT DN UP Outbound on GPS Approach Using HSI Description of GPS oper...

Page 85: ...een set to 103 and the aircraft has made a left turn to this heading The GPS s Leg OBS mode switching is set to Leg mode and the course pointer is set to 058 Select approach mode by depressing the APR button L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 3 3 30 W 24 2 1 S 1 5 1 2 E 6 3 ı AP G KAP 140 HDG NAV APR REV ALT DN UP L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C EL...

Page 86: ...eed needs to be controlled with the throttle Inbound on GPS Approach Using DG L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV ALT DN UP N 3 3 3 0 W 2 4 2 1 S 1 5 12 E 6 3 P U S H PUSH TO FR N S E W 33 3 0 24 2 1 15 1 2 6 3 OBS GS ı L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV ALT DN UP N 33 3 0 W 24 2 1 S 15 1 2 E 6 3 P...

Page 87: ...ssed approach heading of 090 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 Note Press and hold the AP button for 0 25 seconds to engage the autopilot applicable only to software version 03 01 and later L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV ALT DN UP N 33 3 0 W 24 ...

Page 88: ...ent rate is obtained using the DN button Remember speed needs to be controlled with the throttle Inbound on GPS Approach Using HSI Description of GPS operation based on Bendix King GPS receiver Others may require different operation 1 2 3 4 L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 3 3 3 0 W 2 4 2 1 S 1 5 12 E 6 3 ı AP G KAP 140 HDG NAV APR REV ALT DN UP L R 2 MIN TURN COORD...

Page 89: ...s set to the missed approach heading of 090 By depressing the HDG button on the KAP 140 the autopilot engages into the head ing and vertical speed modes commencing a right turn to a heading of 090 and maintaining the rate of climb existing at engagement Note Press and hold the AP button for 0 25 seconds to engage the autopilot applicable only to software version 03 01 and later L R 2 MIN TURN COOR...

Page 90: ...Two Axis Operation 82 KAP 140 AUTOPILOT SYSTEM Rev 1 Apr 02 This page intentionally left blank ...

Page 91: ... the vertical speed VS hold mode The commanded vertical speed is be 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 captured VS will be the vertical speed present at the moment of AP button press When pressed again will disengage the autopilot For software version 03 01 and later the AP button must be ...

Page 92: ...will engage the autopilot in units with software prior to soft ware version 03 01 9 VERTICAL TRIM UP DN BUT TONS The action of these buttons is dependent upon the vertical mode present when pressed If VS mode is active the initial button stroke will bring up the commanded vertical speed in the display Subsequent immediate button strokes will incre ment the vertical speed commanded either up or dow...

Page 93: ...ON The ALERT annunciate is illuminated 1000 ft prior to the selected altitude extin guishes 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 illumi nation signifies that the 200 ft safe band has been exceeded and will remain illuminated until 1000 ft from the selected altitude Associated w...

Page 94: ...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 changes to VS and current vertical speed is displayed 2 UP or DN button Select desired climb or descent rate Each button stroke will increment the vertical speed commanded up or down by 100 ft min per butt...

Page 95: ... operate in the ALT mode with autopilot currently in the Vertical Speed mode 1 ALT button Press Note ALT is annunciated and autopilot maneuvers to maintain pressure altitude acquired at button selec tion 2 UP or DN button Select to change altitude Incremented but ton strokes will move the refer ence altitude by 20 feet per press or if held continuously will com mand a 500 ft min altitude change ac...

Page 96: ...tting Installations with remote baro input 1 BARO setting CHECK depressing the BARO button will display the baro setting for three seconds Installations without remote baro input Upon successful completion of pre flight test the baro display will flash 1 BARO setting Enter baromet ric setting using the rotary knobs OR if correct as displayed press BARO Note It is recommended that the baro value be...

Page 97: ...e mes sages will be annunciated as condi tions warrant 1 TRIM IN MOTION TRIM IN MOTION Pitch trim running for more than 5 seconds 2 CHECK PITCH TRIM An out of trim condition has existed for 15 seconds a Airplane Control Wheel GRASP FIRMLY press CWS and check for an out of pitch trim condition Manually retrim as required b CWS button RELEASE c AUTOPILOT OPERATION CONTINUE if satisfied that the out ...

Page 98: ...Altitude 1 The aircraft is well off the ground and estab lished at a safe climb rate 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 and current rate of climb Note Press and hold the AP button for 0 25 seconds...

Page 99: ...1 S 1 5 1 2 E 6 3 ı AP G KAP 140 HDG NAV APR REV ALT DN UP N 33 3 0 W 2 4 2 1 S 1 5 1 2 E 6 3 P U S H PUSH OR ARM BARO N 080 0 1 0 1 2 3 4 3 The autopilot is responding to the heading select mode with a left bank The climb rate has been decreased using the DN button in preparation for level out The vertical speed value will be displayed upon selection of the DN button and will remain for three sec...

Page 100: ...annunciation is flashing move the heading bug to the desired course of 040 The aircraft will remain wings level until the capture point GPS Capture Using DG L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV ALT DN UP N 33 3 0 W 2 4 2 1 S 1 5 1 2 E 6 3 P U S H PUSH TO FR N S E W 3 3 3 0 2 4 2 1 1 5 12 6 3 OBS GS ı ARM BARO L R 2 MIN TURN COORDINATOR NO PITCH INFO...

Page 101: ...ot is track ing the GPS course L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV ALT DN UP N 3 3 30 W 2 4 21 S 1 5 12 E 6 3 P U S H PUSH TO FR N S E W 3 3 30 2 4 21 1 5 12 6 3 OBS GS ı ARM BARO L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV ALT DN UP N 3 3 30 W 2 4 21 S 1 5 12 E 6 3 P U S H PUSH TO FR N S E W 3 3 30 2 4 21 ...

Page 102: ...pressed and NAV ARM is annunciated GPS Capture Using HSI L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 33 3 0 W 2 4 2 1 S 1 5 1 2 E 6 3 ı AP G KAP 140 HDG NAV APR REV ALT DN UP ARM BARO L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 33 3 0 W 2 4 2 1 S 1 5 1 2 E 6 3 ı AP G KAP 140 HDG NAV APR REV ALT DN UP ARM BARO Description of GPS operation based on Bendix Ki...

Page 103: ...turn is initiated by the autopilot 4 The turn is complete and the autopilot is track ing the GPS course L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 3 3 30 W 2 4 21 S 1 5 12 E 6 3 ı AP G KAP 140 HDG NAV APR REV ALT DN UP ARM BARO L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 3 3 30 W 2 4 21 S 1 5 12 E 6 3 ı AP G KAP 140 HDG NAV APR REV ALT DN UP ARM BARO ...

Page 104: ... cancelled and reverse localizer mode is automatically activated and a left turn outbound on the localizer is initiated by the autopilot Note The left right deviations of the CDI course deviation needle are reversed you must turn right to center a deviation of the index to the left This needle reversing takes place because you are fly ing outbound on a front course Outbound On Front Course For Pro...

Page 105: ...ront course of 058 You must now select the approach mode by depressing the APR button on the KAP 140 The HDG annunciation will flash for five sec onds then extinguish While the HDG annuncia tor is flashing move the heading bug to the front course 058 Since the 45 intercept is 103 the aircraft will not turn until the front course is captured L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC ...

Page 106: ... is reached HDG mode is cancelled and reverse localizer mode is automatically activated and a left turn outbound on the localizer is initiated by the autopilot Note The left right deviations of the HSI course needle operate just as though you were flying a front course approach Outbound On Front Course For Procedure Turn To ILS Approach Using HSI L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C...

Page 107: ...bug to 103 and made a 180 turn to this heading The 103 heading will intercept the front course of 058 You must now select the approach mode by depressing the APR button on the KAP 140 Automatic capture of the localizer will occur L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 3 3 30 W 24 2 1 S 1 5 1 2 E 6 3 ı AP G KAP 140 HDG NAV APR REV ALT DN UP ARM BARO L R 2 MIN TURN COORDINA...

Page 108: ...y disen gaged when the glideslope is captured The ALT annunciator extinguishes and GS is displayed The autopilot will make pitch and bank changes as necessary to maintain localizer and glides lope L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV ALT DN UP N 33 3 0 W 24 2 1 S 15 1 2 E 6 3 P U S H PUSH TO FR N S E W 33 3 0 24 2 1 15 1 2 6 3 OBS GS ı ARM BARO L R ...

Page 109: ...ages into the head ing and vertical speed modes commencing a right turn to a heading of 090 and maintaining the rate of climb existing at engagement Note Press and hold the AP button for 0 25 seconds to engage the autopilot applicable only to software version 03 01 and later L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV ALT DN UP N 33 3 0 W 24 2 1 S 15 1 2 E...

Page 110: ... needle is at midscale Altitude hold is automatically disen gaged when the glideslope is captured The ALT annunciation extinguishes and GS is displayed The autopilot will make pitch and bank changes as necessary to maintain localizer and glides lope L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 33 3 0 W 24 2 1 S 15 1 2 E 6 3 ı AP G KAP 140 HDG NAV APR REV ALT DN UP ARM BARO L R ...

Page 111: ...ssing the HDG button on the KAP 140 the autopilot engages into the head ing and vertical speed modes commencing a right turn to a heading of 090 and maintaining the rate of climb existing at engagement Note Press and hold the AP button for 0 25 seconds to engage the autopilot applicable only to software version 03 01 and later L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 33 3 0...

Page 112: ...to track the 238 GPS course Outbound on GPS Approach Using DG L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV ALT DN UP N 3 3 30 W 24 2 1 S 1 5 1 2 E 6 3 P U S H PUSH TO FR N S E W 3 3 30 24 2 1 1 5 1 2 6 3 OBS GS ı ARM BARO L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV ALT DN UP N 33 3 0 W 24 21 S 15 1 2 E 6 3 P U S H P...

Page 113: ...eg OBS mode switching is set to Leg mode and the OBS is set to 058 Select approach mode by depressing the APR button The HDG annunciation will flash for five sec onds then extinguish While the HDG annuncia tion is flashing move the heading bug to 058 Since the 45 intercept is 103 the aircraft will not turn until the course is captured L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G K...

Page 114: ...mode The autopilot ini tiates a left turn to track the 238 GPS course L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 3 3 30 W 24 2 1 S 1 5 1 2 E 6 3 ı AP G KAP 140 HDG NAV APR REV ALT DN UP ARM BARO L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 33 3 0 W 24 21 S 15 1 2 E 6 3 ı AP G KAP 140 HDG NAV APR REV ALT DN UP ARM BARO Outbound on GPS Approach Using HSI Des...

Page 115: ... been set to 103 and the aircraft has made a left turn to this heading The GPS s Leg OBS mode switching is set to Leg mode and the course pointer is set to 058 Select approach mode by depressing the APR button L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 3 3 30 W 24 2 1 S 1 5 1 2 E 6 3 ı AP G KAP 140 HDG NAV APR REV ALT DN UP ARM BARO L R 2 MIN TURN COORDINATOR NO PITCH INFORMA...

Page 116: ...speed needs to be controlled with the throttle Inbound on GPS Approach Using DG L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV ALT DN UP N 3 3 3 0 W 2 4 2 1 S 1 5 12 E 6 3 P U S H PUSH TO FR N S E W 33 3 0 24 2 1 15 1 2 6 3 OBS GS ı ARM BARO L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 HDG NAV APR REV ALT DN UP N 33 3 0 W 24 2 1 S 15 ...

Page 117: ...essing the HDG button on the KAP 140 the autopilot engages into the head ing and vertical speed modes commencing a right turn to a heading of 090 and maintaining the rate of climb existing at engagement Note Press and hold the AP button for 0 25 seconds to engage the autopilot applicable only to software version 03 01 and later L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC AP G KAP 140 ...

Page 118: ...scent rate is obtained using the DN button Remember speed needs to be controlled with the throttle Inbound on GPS Approach Using HSI Description of GPS operation based on Bendix King GPS receiver Others may require different operation 1 2 3 4 L R 2 MIN TURN COORDINATOR NO PITCH INFORMATION D C ELEC GS GS N 3 3 3 0 W 2 4 2 1 S 1 5 12 E 6 3 ı AP G KAP 140 HDG NAV APR REV ALT DN UP ARM BARO L R 2 MIN...

Page 119: ...ug is set to the missed approach heading of 090 By depressing the HDG button on the KAP 140 the autopilot engages into the head ing and vertical speed modes commencing a right turn to a heading of 090 and maintaining the rate of climb existing at engagement Note Press and hold the AP button for 0 25 seconds to engage the autopilot applicable only to software version 03 01 and later L R 2 MIN TURN ...

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Page 121: ...ystem The panel mounted KI 525A HSI combines the display functions of both the standard Directional Gyro and the Course Deviation Indicator s VOR LOC Glideslope information to provide the pilot with a single pre sentation of the complete horizontal navigation situation This greatly simplifies course orientation inter ception and tracking while eliminat ing the need for scan coordination between tw...

Page 122: ...ing Flag Lubber Line Compass Warning Flag Heading Select Bug Dual Glideslope Pointers Symbolic Aircraft VOR and LOC Deviation Bar Course Select Knob VOR LOC Deviation Scale Compass Card Heading Select Knob Glideslope Deviation Scale To From Indicator Course Select Pointer KI 525A Pictorial Navigation Indicator Description of Indicator and Display Functions Compass Card Responding to the input from...

Page 123: ...deviation left or right of course When tuned to a Localizer the deviation is 1 2 degree per dot When GPS data is selected for presentation refer to the Pilot s Guide for the GPS receiver Heading Select Bug A movable orange marker on the outer perime ter of the display used primarily to select the desired heading you wish to fly This desired heading is cou pled to the KAP 140 Autopilot to pro vide ...

Page 124: ...lection to one side or another NOTE During level flight it is normal for the meter needle to continuously move from side to side and to be fully deflected during a turn If the needle stays fully deflected left or right during level flight the free gyro mode can be used to center it as follows Slave and Free Gyro Switch When the switch is in the AUTO position the system is in the slaved gyro mode W...

Page 125: ...tem and the direc tional gyro is up to speed a red flag labeled HDG will be visible in the upper right quadrant of the KI 525A Indicator In operation this warning flag will be visible whenever the power being sup plied is inadequate or the gyro is not up to speed 2 With the application of power to the KCS 55A System and gyro up to operating speed the red HDG flag should disappear from view 3 If th...

Page 126: ...ived 7 Rotate the course select knob to position the course pointer to the desired VOR course 8 The VOR deviation bar represents the selected course and the rela tionship of this bar to the symbolic aircraft in the center of the instru ment visually presents the actual relationship of the selected course to your aircraft heading In other words if the symbolic aircraft on the display indicates appr...

Page 127: ...tation glideslope transmitter is malfunctioning Glideslope is usu ally not available during a back course approach The VOR and LOC course display will continue to function normally even if a usable glideslope signal is not being received A continuous large deflection of the slaving meter or large discrepan cies between the magnetic compass and the KI 525A compass card may indicate a failure in the...

Page 128: ...shoot ing or bracketing One method of doing this is to adjust your heading so that the top of the deviation bar always touches the lubber line As your aircraft heading approaches the new course the deviation bar will swing towards the center and the angle of intercept will decrease GS GS N 33 3 0 W 24 2 1 S 15 1 2 E 6 3 ı GS GS N 3 3 3 0 W 2 4 2 1 S 1 5 12 E 6 3 ı Flight Procedures with the KCS 55...

Page 129: ... ception by adjusting your head ing to keep the top of the deviation bar touching the lub ber line 4 When the deviation bar is centered and aligned with the course arrow you are on course Notice that correction for wind drift in this case a 080 heading on a 088 course is completely auto matic as long as you keep the deviation bar centered 5 About midway between Napoleon and Columbia CBI you switch...

Page 130: ...m Columbia to Foristell FTZ is 098 you now set the selected course pointer on 098 and fly to keep the devi ation bar centered 7 Near the Herman intersection you switch to Foristell VOR TAC and move the course arrow to 100 which is the V 12 inbound course to FTZ The TO FROM indicator changes to TO GS GS N 3 3 3 0 W 2 4 2 1 S 1 5 12 E 6 3 ı GS GS N 3 3 3 0 W 2 4 2 1 S 1 5 12 E 6 3 ı ...

Page 131: ... course pointer on the STL 062 course 9 As you cross the Foristell VORTAC the deviation bar will align with the course arrow Now set the heading bug to 062 and turn left to follow V 14 to the STL VOR TAC 10 You are now established on V 14 flying to the STL VOR TAC Once again if you fly to keep the deviation bar cen tered correction for wind drift will automatically be accom plished Note For system...

Page 132: ...ly back to the radial in order to be on course during the inbound leg of the holding pattern 3 Outbound you are using the heading bug as reference for 244 The 244 radial is off the right wing and parallel to your outbound course 4 Halfway through your turn to the inbound 064 course the KI 525A shows the sym bolic aircraft approaching the deviation bar at a right angle By keeping the top of the dev...

Page 133: ...ith the course arrow Each dot on the LOC deviation scale represents 1 2 degree of deviation when tuned to an ILS frequency 3 The KI 525A shows you that you have inter cepted the localizer course The glideslope pointers have started to center although the display indicates your aircraft is still below the glidepath at this point 4 You are now centered on the localizer and the glideslope Once again ...

Page 134: ...orially that the air craft as represented by the symbolic air craft in the center of the KI 525A is flying away from the localizer centerline at a 45 angle when the heading bug is under the lubber line Note that left right deviations of the course bar give fly to indicators just as on the front course 3 Now you ve reset the heading bug to 013 and made a 180 turn to this heading This 013 heading wi...

Page 135: ... in react ing to an autopilot or trim malfunction or to an automatic disconnect of the autopilot is in maintaining control of the airplane Immediately grasp the con trol wheel and press and hold down the A P DISC TRIM INTER switch throughout the recovery Manipulate the controls as required to safely main tain operation of the airplane within all of its operating limitations CAUTION Refer to the Ai...

Page 136: ...Abnormal Procedures 128 KAP 140 AUTOPILOT SYSTEM Rev 0 Jun 98 This page intentionally left blank ...

Page 137: ...rnational 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 All rights reserved 006 18034 0000 Rev 2 5 02 N ...

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