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Part #: 066-01197-0205

Model: KGP-860

BendixKing - EGPWS
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Part Number :


KGP-860
 
FEATURES
  • Same as Honeywell P/N 965-1199-005
  • Enhanced Ground Proximity Warning System specifically designed for light turbine and piston aircraft
  • Combines early alert/warning capability with optional terrain display (when used with compatible display)
  • Incorporates GPS position and terrain/obstacle database to indicate terrain above and below aircraft
  • Terrain display can be presented on KMD-550 or KMD-850 MFDs, weather indicator (with compatible terrain input), or dedicated display (such as Honeywell TRA-45A Display)
  • Capable of displaying terrain on displays implementing KCPB picture bus protocol or ARINC 453/708 interface (see sample list of compatible displays below)
  • Available six-color terrain alerting and display output

Note: display option not required for Class B TAWS compliance

  • Click Here to view an example of the KGP-860 terrain display
  • Meets TSO C151a Class B TAWS requirements (-0101 version)
  • Meets TSO C151b Class B TAWS requirements (-0205 version)
  • Updateable worldwide terrain database
  • Up to 320 nm display capability
  • Built-in GPS sensor - preferred interface
  • Accepts GPS data from external sensor with RS-232/422 and ARINC 743/743A formats (see sample list of compatible sensors below)
  • GPS data is supplied via optional KA-91 or KA-92 GPS antenna (Optional antenna splitter also available $360 list)
  • Available six-color terrain alerting and display output
  • EFIS 40/50 interface
  • Advanced Runway Field Clearance Floor (RFCF) feature provides 360 degree coverage of terrain and obstacles within 5 nm of public runways of more than 2000 ft.
  • Exclusive "peaks" mode displays terrain below the aircraft
  • Easy to install weighing less than 1.5 pounds
  • Radar altitude input
  • Typical system consists of KGP-860 EGPWS computer, database card (Americas, Atlantic, or Pacific), configuration module, and installation kits
  • Configuration module provides mean to store aircraft specific information such as aircraft configuration, GPS source, audio levels, etc.
  • Capable to interface with most EFIS systems such as Collins FDS-255/2000 and Honeywell Radar Systems such as Primus 90/300/400/440/600/660/880/1000
  • Added warning modes over KGP-560 for descent, closure to terrain, altitude loss after takeoff, terrain clearance, and altitude callouts
  • Same as KGP-560 but includes advanced features such as rad alt input, EFIS interface, bank angle alert, and gear/flap warnings

(COMPATIBLE TERRAIN DISPLAYS) - Avidyne EX500 MFD - Collins WXR-220, WXR-270, WXR-300 (when used with Avtech DSU) - Honeywell EFIS-40/50 - Honeywell GNS-XLS FMS (P/N 17960-0203-XXXX only) - Honeywell IN-182A, IN-812A, IN-842A, IN-862A, RDR-4A, RDR-4B Radar Indicators - Honeywell KMD-550 and KMD-850 MFD (with KAC-502 module) - Honeywell Primus 90 / 200 / 300 / 400SL / 400 Std / 440 / 500 / 650 / 660 / 700 / 800 / 880 (when used with Avtech DSU) - Honeywell TRA-45A Terrain Display (COMPATIBLE GPS SENSORS) GNS-XLS, Universal UNS-1C/1D/1K/1M FMS KLN-94, KLN-900 GPS, NOT compatible with KLN-90B GPS GNS-430 and GNS-530 GPS/NAV/COMM (Compatible Barometric Altitude Sources) KEA-130A and KEA-346 Encoding Altimeters 8130B Aero-Mechanism Encoding Altimeter AR850 Narco and SSD120 Trans-Cal Encoders (PLEASE NOTE THAT THE ABOVE LISTS OF COMPATIBLE AVIONICS UNITS IS NOT COMPREHENSIVE AND FINAL. IT IS POSSIBLE THAT THERE ARE OTHER UNITS NOT INCLUDED ON THESE LISTS THAT MAY BE COMPATIBLE SHOULD THESE OTHER UNITS CONTAIN THE PROPER SPECS AND PARAMETTERS FOR CORRECT INTERFACING.)

 

SPECIFICATIONS
Temperature Range: -40 to 55C Altitude: 55000 ft.
Weight: 1.5 lbs. Dimensions: 2.2"W x 4.15"H x 6.25"D
Power Input: 10-32 VDC Outputs: Display annunciators, aural warnings
Part Number EGPWS Computer:
066-01197-0101 Original production unit
066-01197-0205 Current production version (2004) with TSO C151b certification

 

066-01197-0205
- 965-1199-005 EGPWS Computer
Price Condition Status
$6,995.00 NEW OUTRIGHT REQUEST

Click on a question below to see the answer. If you have a question about this model that is not answered below, please contact questions@seaerospace.com

Many avionics systems require a configuration or setup process. This process is required to interface certain avionics systems to other systems in the aircraft that will be inputting or outputting information to and from these systems. Some examples of systems that require a configuration or setup process include:

Autopilot
EFIS
GPS
EGPWS
EHSI
RADAR
TAWS
TCAS


In addition, most newer technology or solid state systems require configuration via computer interface of some type. A qualified avionics technician should always refer to the appropriate manufacturer's installation manual for complete information and instructions.
In April 2004, Honeywell announced on Installation Bulletin No. 507 that the Sandisk flash card used in the database card for the KGP-560 and KGP-860 was being replaced with a new flash card manufactured by Smart Modular Technologies.

These new database cards will only work with KGP-560 units with Mod or Service Bulletin 3 and KGP-860 units with Mod/B 1 incorporated. These Service Bulletins consist of replacing the Processor Card Board in the unit.

As Honeywell considers this a product improvement, the cost to incorporate these mods is approximately $2500 and must be performed at the factory.