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Honeywell BENDIXKing APEX EDGE Series Pilot's Manual

Primary flight display
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  • Page 3 Telephone: (800) 601-3099 (U.S.A./Canada) Telephone: (602) 365-3099 (International) APEX EDGE SERIES KFD 840 Primary Flight Display Pilot’s Guide KFD 840 PG PN 7450-0840-01 Rev D July 12, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 4 Honeywell hereby grants you a limited, non-exclusive license to use these Materials to KFD 840 PG PN 7450-0840-01 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 5 Honeywell aerospace products only in accordance with that agreement. If you are a direct recipient of these Materials from Honeywell's Aerospace Technical Publication Distribution and are not a party to an agreement related to the operation, maintenance or repair...
  • Page 6 This license sets forth the entire agreement between you and Honeywell and may only be modified by a writing duly executed by the duly authorized representatives of the parties. Copyright - Notice Copyright 2010, Honeywell International Inc.
  • Page 7 Added a clarification for when the heading SYNC button is pressed when the aircraft is on a 360 degree heading. See page 7-3. KFD 840 PG PN 7450-0840-01 Record of Revisions Rev D July 12, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 8 NUMBER DATE Sept 13, 2009 Sept 23, 2009 May 28, 2010 July 12, 2010 Record of Revisions KFD 840 PG PN 7450-0840-01 RR-2 Rev D July 12, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 9 May 28, 2010 May 28, 2010 ■ indicates a changed or added page. KFD 840 PG PN 7450-0840-01 List of Effective Pages Rev D July 12, 2010. LEP-1 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 10 May 28, 2010 ■ 11-4 July 12, 2010 ■ indicates a changed or added page. List of Effective Pages KFD 840 PG PN 7450-0840-01 LEP-2 Rev D July 12, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 11: Table Of Contents

    AIRSPEED COLOR BANDS ..........4-4 OVER SPEED AWARENESS BAR ........4-5 LOW SPEED AWARENESS BAR .......... 4-5 KFD 840 PG PN 7450-0840-01 Table of Contents Rev C May 28, 2010 TC-1 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 12 GPS Identifier and Distance ..........7-7 CDI Source ................ 7-8 To/From Pointer ..............7-9 Table of Contents KFD 840 PG PN 7450-0840-01 TOC- 2 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 13 MINOR FAILURE INDICATIONS ......... 10-6 11. APPENDIX ................11-1 ACRONYMS AND ABBREVIATIONS ........11-1 AIRCRAFT CONFIGURATION ..........11-3 KFD 840 PG PN 7450-0840-01 Table of Contents Rev C May 28, 2010 TOC-3 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 14 Figure 10-2 Attitude Failure ............10-2 Figure 10-3 Heading Fail ............... 10-3 Figure 10-4 In-Flight Reinitialation ..........10-4 Table of Contents KFD 840 PG PN 7450-0840-01 TOC- 4 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 15: Introduction

    For additional support, contact Honeywell Customer & Product Support: at: US & Canada: 1-877-712-2386 All other countries: 1-913-712-2613 Fax: 1-913-712-5697 KFD 840 PG PN 7450-0840-01 Introduction Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 16: Honeywell Aerospace Technical Publications

    Honeywell Bendix/King KFD 840 Primary Flight Display Honeywell Aerospace Technical Publications If you have access to the Internet, go to the Honeywell Online Technical Publications Web site at https://portal.honeywell.com/wps/portal/aero • Download or see publications online • Make an order for a publication •...

  • Page 17: Getting Started

    This section provides an overview of the operating controls and displays of the KFD 840. The PFD is shown below. Figure 2-1 Controls and Displays KFD 840 PG PN 7450-0840-01 Getting Started Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 18: Main Display Areas

    The PFD display is divided into different display areas as shown on the figures below: Figure 2-2 Display Main Areas - Part 1 Getting Started KFD 840 PG PN 7450-0840-01 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 19 Rate of turn • Airspeed Area Airspeed tape, rolling digits, and trend vector Selected airspeed readout and bug KFD 840 PG PN 7450-0840-01 Getting Started Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 20 Vertical Speed Area Vertical speed readout, scale, and pointer • Checklist Area User defined Checklist pages Getting Started KFD 840 PG PN 7450-0840-01 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 21 CDI needle has been turned ON and Bearing sources are being displayed. The CDI is shown centered in a TO condition. Figure 2-4 Display Symbology KFD 840 PG PN 7450-0840-01 Getting Started Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 22 25. Heading Bug (HDG) 14. Vertical Speed Digital 26. Function Keys Menu Readout 27. Course Pointer Getting Started KFD 840 PG PN 7450-0840-01 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 23: Basic Operation

    (CONF), display information screen (INFO). Detailed operation of each selection is provided later in this manual. KFD 840 PG PN 7450-0840-01 Getting Started Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 24 For short press/release actions (less than two seconds), the selection will occur when the button is released. Getting Started KFD 840 PG PN 7450-0840-01 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 25: Function Keys

    Figure 2-7 Default KFD 840 Menu Structure KFD 840 PG PN 7450-0840-01 Getting Started Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 26: Display Brightness (Brt)

    Minimum Altitude Alert (MIN) DISABLED/ENABLED Outside Air Temperature (OAT) Units Degrees F or Degrees C Getting Started KFD 840 PG PN 7450-0840-01 2-10 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 27 The KFD Flight Settings page will be displayed. Figure 2-8 KFD Flight Settings Page Part 1 KFD 840 PG PN 7450-0840-01 Getting Started Rev C May 28, 2010 2-11 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 28 RETURN function key. To exit the KFD Flight Settings page without saving press the RETURN function key. Getting Started KFD 840 PG PN 7450-0840-01 2-12 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 29: Attitude Area

    PFD, is shown below. The descriptions of the elements of the ADI are given in the following paragraphs. Figure 3-1 Attitude Director Window KFD 840 PG PN 7450-0840-01 Attitude Area Rev D July 12, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 30: Artificial Horizon

    NOTE: The 30° up and 30° down markings on the attitude tape will not be displayed until the aircraft is pitched in the appropriate direction approximately 18°. Attitude Area KFD 840 PG PN 7450-0840-01 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 31 The pitch tape, roll pointer, and slip-skid indicator are removed; the ATTITUDE FAILURE annunciator is displayed. Figure 3-4 Attitude Failure Indication KFD 840 PG PN 7450-0840-01 Attitude Area Rev D July 12, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 32: Aircraft Reference Symbol

    -2.5 , -5 , -7.5 , -10 , -15 , -30 , -45 , and -60 Attitude Area KFD 840 PG PN 7450-0840-01 Rev D July 12, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 33 63º right wing down and 63º left wing down, and pitch angle is between 28º nose up and 18º nose down. KFD 840 PG PN 7450-0840-01 Attitude Area Rev D July 12, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 34: Attitude Roll Pointer And Scale

    The attitude roll pointer moves to the left as the roll angle increases and to the right as the roll angle decreases. Attitude Area KFD 840 PG PN 7450-0840-01 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 35 The attitude pitch tape is displayed behind the following symbols on the ADI: • Attitude reference aircraft symbol • Rate-of-turn indicator • Flight director KFD 840 PG PN 7450-0840-01 Attitude Area Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 36: Slip-Skid/Standard Rate Turn Marker Display

    Air Data, OAT, or TAS has failed or is inoperative. Figure 3-7 Slip-Skip Standard Rate Turn Marker Display Attitude Area KFD 840 PG PN 7450-0840-01 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 37: Flight Director Command Bars

    The single-cue command bar consists of two solid magenta wedges that move as shown in the figures below: Pitch up command Pitch down command KFD 840 PG PN 7450-0840-01 Attitude Area Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 38 Honeywell Bendix/King KFD 840 Primary Flight Display Roll right command. Roll left command The command bar moves behind the aircraft symbol. Attitude Area KFD 840 PG PN 7450-0840-01 3-10 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 39: Airspeed Area

    4. Selected Airspeed reference digital readout 5. Airspeed Trend Bar 6. Selected Airspeed Bug Figure 4-1 Airspeed Tape KFD 840 PG PN 7450-0840-01 Airspeed Area Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 40: Selected Speed Reference Digital Readout And Bug

    (airspeed reference line) of the tape. The scale slides down for accelerating airspeeds decelerating airspeeds. Airspeed Area KFD 840 PG PN 7450-0840-01 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 41: Airspeed Trend Vector

    The airspeed trend vector expands upward for positive acceleration values and downward for negative acceleration values. KFD 840 PG PN 7450-0840-01 Airspeed Area Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 42: Airspeed Color Bands

    Red Vertical Bar = Low speed awareness bar NOTE: V and V are only used in multi-engine aircraft. Airspeed Area KFD 840 PG PN 7450-0840-01 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 43: Over Speed Awareness Bar

    KFD 840 PG PN 7450-0840-01 Airspeed Area Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 44 Honeywell Bendix/King KFD 840 Primary Flight Display This Page Intentionally Left Blank Airspeed Area KFD 840 PG PN 7450-0840-01 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 45: Altitude Area

    9. Altitude Tape Indicator (MIN) 5. MIN Digits 10. Selected Altitude Digits Figure 5-1 Altitude Display KFD 840 PG PN 7450-0840-01 Altitude Area Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 46: Altitude Tape

    For negative altitudes, a leading minus sign is displayed. Altitude Area KFD 840 PG PN 7450-0840-01 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 47: Metric Altitude

    The altitude trend vector is removed when the aircraft is in level flight (not climbing or descending or zero trend). KFD 840 PG PN 7450-0840-01 Altitude Area Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 48: Altitude Data Invalid

    2 seconds when ALT is highlighted will cause the altitude bug to SYNC, synchronize to the current altitude. Altitude Area KFD 840 PG PN 7450-0840-01 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 49: Altitude Select Display

    If the selected altitude data is invalid, the selected altitude bug is removed and the selected altitude digital readout is replaced with amber dashes. KFD 840 PG PN 7450-0840-01 Altitude Area Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 50: Barometric (Baro) Setting

    Press the right knob four times to activate the MIN display. Turn the knob clockwise increase setting counterclockwise to decrease the value. Pressing and holding the Altitude Area KFD 840 PG PN 7450-0840-01 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 51: Minimum Altitude Alert Condition Armed

    If MIN data is invalid, the digital readout is replaced with three amber dashes (---).The MIN label continues to be displayed. KFD 840 PG PN 7450-0840-01 Altitude Area Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 52: Vertical Deviation Scale And Pointer

    429 format, the vertical deviation scale is removed when invalid. Refer to installer for your aircraft’s specific configuration. Altitude Area KFD 840 PG PN 7450-0840-01 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 53: Vsi Area

    The VS display includes the following: • Vertical speed scale and pointer • Vertical speed digital readout Figure 6-1 VSI Display KFD 840 PG PN 7450-0840-01 VSI Area Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 54: Vertical Speed Scale And Pointer

    +1000 fpm or greater. If vertical speed data is invalid, the vertical speed digital readout is removed. VSI Area KFD 840 PG PN 7450-0840-01 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 55: Vertical Speed Data Invalid

    If pressure altitude or vertical speed data is invalid, the vertical speed scale markings and pointer are replaced with a red X. KFD 840 PG PN 7450-0840-01 VSI Area Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 56 Honeywell Bendix/King KFD 840 Primary Flight Display This Page Intentionally Left Blank VSI Area KFD 840 PG PN 7450-0840-01 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 57: Hsi Area

    The full compass is shown below. Figure 7-1 HSI Display The partial compass (ARC HSI) is shown below. KFD 840 PG PN 7450-0840-01 HSI Area Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 58 The ARC HSI compass shows ±60 degrees from the current aircraft heading. HSI Area KFD 840 PG PN 7450-0840-01 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 59: Heading Readout

    Turning the HDG knob will restore the display. KFD 840 PG PN 7450-0840-01 HSI Area Rev D July 12, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 60: Heading Select Bug Off-Scale

    HDG FAIL flag is displayed in the middle upper portion of the compass display. HSI Area KFD 840 PG PN 7450-0840-01 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 61: Course Selected Digital Readout

    Lateral deviation information comes from the VOR, ILS, or the GPS. KFD 840 PG PN 7450-0840-01 HSI Area Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 62: Bearing Pointers

    NAV facility. When GPS is the source, the pointer points to the active waypoint in the flight plan. HSI Area KFD 840 PG PN 7450-0840-01 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 63: Bearing Pointer Source

    100 nm or more and a resolution of 0.1 nm for distances less the 100 Time to the waypoint is displayed below the distance. KFD 840 PG PN 7450-0840-01 HSI Area Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 64: Cdi Source

    The full menu of navigation selections is displayed even if that navigation unit is not installed. HSI Area KFD 840 PG PN 7450-0840-01 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 65: To/From Pointer

    GPS waypoint. Figure 7-8 TO Pointer Figure 7-9 FROM Pointer KFD 840 PG PN 7450-0840-01 HSI Area Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 66 Honeywell Bendix/King KFD 840 Primary Flight Display This Page Intentionally Left Blank HSI Area KFD 840 PG PN 7450-0840-01 7-10 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 67: Checklist Area

    ON/CHK OFF will be displayed above the CHK LST button as shown in the figure below. Figure 8-1 Checklist Menu - CHK OFF KFD 840 PG PN 7450-0840-01 Checklist Area Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 68 Press the right knob four times until CHK LST is highlighted. Turn the knob to move through the checklist pages as shown in the figure below. Checklist Area KFD 840 PG PN 7450-0840-01 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 69 KFD 840 while continuing to depress the #1 and #5 buttons until the Maintenance screen appears. KFD 840 PG PN 7450-0840-01 Checklist Area Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 70 Make sure they have not been corrupted by the transfer and read correctly. Checklist Area KFD 840 PG PN 7450-0840-01 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 71 9. If the checklist is ok, depress the SAVE button. This will save the selected Checklist to the KFD 840. Figure 8-6 Checklist Saved to KFD 840 KFD 840 PG PN 7450-0840-01 Checklist Area Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 72 Changes can be made to the checklist pages using the PC Utility tool noted above. Checklist Area KFD 840 PG PN 7450-0840-01 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 73: Miscellaneous Data Area

    True airspeed. The wind values can then be calculated based upon the most accurate true airspeed. KFD 840 PG PN 7450-0840-01 Miscellaneous Data Area Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 74: Ground Speed

    ADI display. Miscellaneous Data Area KFD 840 PG PN 7450-0840-01 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 75: 10. Emergency Operations

    The pilot must fly using the standby instruments when the air data has failed. KFD 840 PG PN 7450-0840-01 Emergency Operations Rev C May 28, 2010 10-1 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 76: Attitude Failure, Ahrs Failure

    The pilot must fly using the standby instruments when the AHRS has failed. Figure 10-2 Attitude Failure Emergency Operations KFD 840 PG PN 7450-0840-01 10-2 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 77: Hdg (Heading) Fail, Crm Failure (Compass Remote Magnetometer)

    The pilot must fly using the standby instruments when the magnetometer has failed. Figure 10-3 Heading Fail KFD 840 PG PN 7450-0840-01 Emergency Operations Rev C May 28, 2010 10-3 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 78: In-Flight Restart

    AHRS has been initialized and the failure condition is eliminated. Emergency Operations KFD 840 PG PN 7450-0840-01 10-4 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 79: Configuration Module Errors

    Flight and continued flight is permitted. It is recommended obtaining maintenance at the next available opportunity. KFD 840 PG PN 7450-0840-01 Emergency Operations Rev C May 28, 2010 10-5 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 80: Minor Failure Indications

    Loss of data, no computed data or failures to non critical or secondary display parameters will amber dash the data value field. Emergency Operations KFD 840 PG PN 7450-0840-01 10-6 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 81: 11. Appendix

    Hectopascals headwind InHg inches of mercury knots per hour KFD 840 PG PN 7450-0840-01 Appendix Rev C May 28, 2010 11-1 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 82 Airspeed VHF omnidirectional range VLOC VOR/localizer crosswind Appendix KFD 840 PG PN 7450-0840-01 11-2 Rev C May 28, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...

  • Page 83: Aircraft Configuration

    (MPH) 0-240 Kts / (276) (MPH) 0-240 Kts / (276) (MPH) 0-240 Kts / (276) (MPH) KFD 840 PG PN 7450-0840-01 Appendix Rev C May 28, 2010 11-3 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 84 AP Type NONE, ARINC, ANALOG ON, OFF BUG ON (0-14999) ACCEPT MIN DIM ACCEPT ON, OFF ENABLE Appendix KFD 840 PG PN 7450-0840-01 11-4 Rev D July 12, 2010 © Honeywell International Inc. Do not copy without express permission of Honeywell...
  • Page 85 Pressing the “SAVE” button will store the data permanently into the internal memory of the KFD 840 and the configuration module. KFD 840 PG PN 7450-0840-01 Appendix Rev C May 28, 2010 11-5 © Honeywell International Inc. Do not copy without express permission of Honeywell...

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