HONEYWELL BENDIX KING® KG...
BENDIX KING KG 102A TSO'd Remote Mounted Directional Gyro can be used in in BK KCS 55A compass system in conjunction with KMT 112 Magnetic Azimuth Transmitter to provide a gyro-stabilized magnetic heading to KI 525A HSI.
The KANNAD 406 AS (P/N S1823502-03) is a aeronautical survival beacon. Thanks to its small size and light weight, the Kannad 406 AS fits easily inside a liferaft. It is supplied with a floating collar.
The KANNAD 406 AS is qualified by the French Civil Aviation in Europe with JTSO-2C91a & JTSO-2C126 and by FAA with TSO-C91a & TSO-C126 applied to “survival” beacons.
The ELT is programmed with either the aircraft tail number, a serial number or the aircraft operator designator. It can be installed inside an aircraft on a mounting bracket or in a carry-off bag (both on options).
The mounting bracket option includes a locking pin to avoid accidental activation before ELT removal. The locking pin can be ordered separately with the carry off version.
The ELT can be fitted with a "Water Switch Sensor" to be activated automatically when in contact with water. A buzzer and a led indicate activation.
An integrated “self test” checks the main functions of the beacon. The test result is given by the led flashing sequence.
Product Features:
Battery replacement is only every 6 years.
Precise pinpointing (<1NM) due to the unparalleled frequency accuracy of the 406 transmitter.
Three frequency transmitter (121.5 / 243 / 406 MHz)
Weight (including battery, auxiliary antenna and floating collar) 2.53 lbs (1150 g)
Options:
P/N S18 20 511-03 carry-off bag
P/N S1820511-02 Mounting bracket with locking pin
P/N S1820514-14 Water Switch Sensor
KANNAD 406 AS Technical Specifications:
TRANSMISSION
406.025 MHz
5W (37 ±2dBm)
Modulation 16K0G1D (bi-phase L encoding) with aircraft identification code
Distress message every 50 s
121.5 MHz and 243 MHz
100mW min (+20dBm)
Modulation 3K20A3X
Audio sweep from 1420 Hz to 490 Hz
Continuous transmission
POWER SUPPLY
Solid Cathode Lithium battery pack (LiMnO2)
Battery replacement every 6 years
PROGRAMMING
Aircraft nationality and registration marking
Aircraft operator designator and ELT serial number up to 4096
Aircraft ICAO 24 bit address
Serial number
ACTIVATION
Manually
Water Switch Activation on option
SELF TEST
406 MHz RF power
Battery voltage
Frequency
Programming
TEMPERATURE RANGE
Operating -20°C to +55°C
Storage -55°C to +85°C
MECHANICS
Molded plastic
Color yellow (color compounded)
WEIGHT AND DIMENSIONS
1150 gr (2.53lbs) including battery pack, auxiliary antenna and floating collar
Transmitter 172 x 82 x 82 mm (6.77 x 3.22 x 3.22”)
TESTS & CERTIFICATION
Type ELT(S)
JTSO-2C91a,JTSO-2C126
ED 62, ED14
TSO-C91a, TSO-C126
DO183, DO204, DO160
Resistance, crush, 500 G shocks, cabin depressurization, watertightness
CONTROLS
ARM / OFF / ON switch
Bright red LED
BNC or TNC antenna connector
DIN 12 programming connector input or remote control connector
ANTENNA
Three frequency (121.5 / 243 / 406 MHz)
Whip 400 mm (15.75”)
TNC connector
BENDIX KING KG 102A TSO'd Remote Mounted Directional Gyro can be used in in BK KCS 55A compass system in conjunction with KMT 112 Magnetic Azimuth Transmitter to provide a gyro-stabilized magnetic heading to KI 525A HSI.
VDO Fuel Level Gauges have always been known for the superb fit, finish, and appearance, as well as the wide range of styles VDO offers. VDO Fuel Level 10-180 ohm Gauges are offered in 2" and 2-1/4'" diameters with matching Fuel Level Senders (aka sensors or probes) for their operation. This 12/24 VDC Fuel Level Sender has a resistance rating of 10 ohms when the tank is empty and 180 ohms when full. The unit can be adjusted to read accurately in tanks from 6" to 23" deep. In the case of the 2" 33-240 ohm Fuel Gauge, the appropriate fuel sender is P/N 226-007.
VDO product range also include Standard Tubular Level sensors mounted direct into the tank with different tube diameters and lengths from 200 mm to 650 mm and different resistances. They feature:
- Resistance output
- Compatibility to the VDO gauges 301-010-00X and X10-110-981-009 (adjustable to 60 to 90 Ohm at empty).
- M4 bolt and hexagon nut or 6,3 x 0,8 mm spade terminal
- Optional ground connector
- Optional warning contact
- Mounting bolt circle 54 mm dip tube fuel senders with different tube diameters and lengths.
For additional information please consult the supplied documentation or contact us.
The new OROLIA-KANNAD INTEGRA 406 GPS ELT is a major step forward in the development of ELT technology and aircraft safety. Major benefits over standard ELTs include a fail-safe automatically activated system for transmission of both the unique identification and GPS position in case of ditching of the aircraft or a crash landing as well as the ability for the pilot/ crew to remove the ELT from a downed aircraft. In addition,it features internal 406MHz and GPS antennas saving significant cost on aircraft installation without the need for an external antenna (national authorities’ rules and regulations permitting) and additional external GPS interface.
The 406 INTEGRA fixed ELT(AF) transmits on both the international 406MHz satellite search and rescue system (min 24 hours from activation) and on 121.5MHz for local direction finding. Minimum operating temperature is -20°C. The internal battery life of the INTEGRA is 6 years. Complies with European and FAA standards.
406 INTEGRA ELT(AF) is designed for flat installation on fixed wing aircraft and can be connected to an outside antenna (sold separately).
This ELT comes with:
the COMPACT universal mounting bracket
RC200 remote control panel
DIN-12 connector
SUB-D 9 pts female connector
Note: Hazardous Material
LONE STAR AVIATION manufactures multiple fans and blowers for OEM applications.
The CYCLONE 100 FAA-PMA approved 1 port blower is the smallest (1 x 2 x2 ), most efficient (brushless dc motor), and the most versatile cooling fan for avionics and or other electronics needing thermal cooling. Its universal mounting bracket makes it easy to set-up and install on on many make and model aircraft and or rotor-craft. Also installed in Land-Mobile, Marine and Military Vehicles for many PED, radio, GPS applications. Offered in Input 12VDC/24VDC versions.
Lone Star Aviation's new FAA-PMA approved Cyclone 1 port blower is the smallest (1 x 2 x2 ), most efficient (brushless dc motor), and the most versatile cooling fan for avionics and or other electronics needing thermal cooling. Its universal mounting bracket makes it easy to set-up and install on on many make and model aircraft and or rotor-craft. Also installed in Land-Mobile, Marine and Military Vehicles for many PED, radio, GPS applications.
The CYCLONE 21 FAA-PMA approved 3 port blower is a compact (3 x 3 x 1") aircraft electronics cooling fan that delivers 21 cubic feet per minute of forced air cooling to a variety of avionics equipment. It is the top FAA approved avionics blower for 14/28 volt aircraft with the smallest footprint and the highest output but also the number one choice for OEM and aftermarket sales world-wide for many make and model aircraft and rotor-craft.
For more information on the above products please consult the Product Description section and the supplied documentation.
ROTAX® aircraft engines form part of the product portfolio of BRP-Powertrain GmbH & Co. KG which develops and manufactures engines for snowmobiles, watercrafts, boats, roadsters, all-terrain and side-by-side vehicles, motorcycles, carts, and aircrafts.
BRP-ROTAX® product range includes certified and non certified internal combustion engines, parts and accessories for light and ultralight aircraft.
Fuel pressure gauges are used in BRP-ROTAX® aircraft engines and offered as certified or non certified parts from their respective manufacturers. Non certified parts can be used in ultralights or other aircraft not requiring certification of parts for their installation.
Aircraft engine parts are subject to changes from time to time. Some parts may be no longer available or replaced by others with different part numbers. Listed BRP-ROTAX® engine parts do not imply their current availability or suitability for your engine application. Always consult the most recent Illustrated Part Catalogs (IPCs) or other documentation available from the manufacturer for the correct part number before ordering.
Fuel pressure gauges are no longer offered as ROTAX Part Numbers. These part numbers are provided for reference only. For these gauges please refer to our product presentation on AVIASPORT Fuel Pressure Gauges or contact us.
The HONEYWELL BENDIX KING® KCS 55A Compass System provides the pilot with a simple, comprehensive visual display of the aircraft's heading and position in relation to a desired course. The system simplifies course orientation, intercept and tracking. Although only the KI 525A Pictorial Navigation Indicator (PNI) and the KA 51B Slaving Control & Compensator Unit appear in the aircraft panel, other remote components of the KCS 55A system include the KMT 112 Magnetic Slaving Transmitter, the KG 102A Directional Gyro for stabilization of the system and optionally the KA 52 or KA 57 Autopilot Adapters making the KCS 55A a complete slaved compass system. Installation parts and manuals of the above components are sold separately. For further information on these components please refer to their individual product presentations. For additional information on KCS 55A and technical specifications please consult the Product Description section.
The HONEYWELL BENDIX KING® components of KCS 55A Compass System can be furnished in NEW condition or as USED in Serviceable or Overhauled conditions indicated respectively by the letters "SV" and "OH" in the product reference numbers (SKU and accompanied by the relevant certification (e.g. yellow tag, 8130-3 form). They are also offered as exchanges / trade-ins for returned customer owned units indicated by the letter "EX" in the SKU. In the case of an exchange/trade-in option of a customer unit, the full selling price of the ordered unit is charged and the core credit is refunded or credited towards future orders when our co-operating supplier verifies that the unit is in a reasonable, repairable condition. It is recommended that this option is selected by our customers mainly for upgrades and only in cases when their units are functioning properly at the time removal from the aircraft. In cases when customer units are found by our supplier to be non-repairable, the core deposit shall not be refunded and shipping charges shall apply if customers wish the return of these units to them.
The Distance Measuring Equipment (DME) systems used on aircraft provide information on aircraft slant distance, ground speed, and time to a ground station. They operate in the 960 – 1215 MHz frequency band.
HONEYWELL BENDIX KING®, a leading avionics manufacturer offers panel mounted, remote DME, DME displays outlined below as well as accesories such as racks & connectors for DME installation and connection. They are offered for outright sale or in exchange for returned customer owned units in NEW Condition or USED (Serviceable or Overhauled) Conditions. The letters "SV","OH" and "EX" in the product reference numbers (SKU) indicate the condition/sale terms.
For additional information please consult the Product Description section & the supplied documentation.
HONEYWELL BENDIX KING® Panel Mounted DME
BENDIX KING® Silver Crown Plus line of Panel Mounted 100 watt KN 62A and 50 watt KN 64 DME are self-contained, 200-channel systems, which can be channeled remotely through almost any NAV receiver or tuned directly with their own frequency selection knobs. They offer dual channeling capability with two DME frequencies available at all times (one remote & one stored internally). Also feature redesigned faceplates for improved readings' illumination, large sturdy knobs and a three-position function switch for easy operation. They operate on any 11 to 33 VDC voltage without adapters or power converters while due to their modest power requirements no external cooling is needed.
HONEYWELL BENDIX KING® Remote DME
BENDIX KING® TSO'd KN 63 DME is a complete 100 watt, 200-channel remote DME system utilizing Large Scale Integrated (LSI) circuit technology. Offering significant advantages in DME reliability and performance, the KN 63 is all solid-state (no transmitter tubes) and can be installed with either single or dual panel DME indicators (displays) such as the BENDIX KING® KDI-572 or KDI-574.
HONEYWELL BENDIX KING® DME Displays
BENDIX KING® TSO'd KDI-572 or KDI-574 DME Displays can be used as master display controls and information displays from KN 63 remote DME transceiver. The top-quality KDI 572 DME displays distance, groundspeed, and time-to-station all at the same time. Slant-range distance is computed digitally and displayed up to the maximum range of 399 nautical miles. Station lock-on is typically achieved within three seconds, with accurate groundspeed and time to station computations becoming available within one minute. The KDI 572's single control switch offers easy operation of the entire DME system as well as DME channeling. It has settings for ON/OFF, NAV 1, NAV 2, and DME HOLD. Comes with an indicator for area navigation (RNAV) to let you know if the displayed distance and time are to a waypoint or a radio navigation beacon. The TSO'd KDI 574 DME display is similar to KDI-572 but DOES NOT include ON/OFF, NAV 1/2, DME Hold selector. For use with Bendix/King Remote DMEs KDM-706 / KDM-706A, KN-63 DME and KTU-709 TACAN.
The EDM 930 by JPI collects and displays engine data in a useful way. This EDM monitors engine temperatures and voltages, adjusts the fuel/air mixture, and diagnoses engine malfunctions. The EDM 930 display screen is arranged into three sections. The top left is the RPM and MAP section. The bottom left is the Scanner® section. And the right side is the Bar Graphs section.
The RPM and MAP Display shows the RPM (Revolutions per Minute) and the MAP (Manifold Pressure).
The Bar Graphs Display shows:
- Oil temperature
- Oil pressure
- Fuel pressure
- Bus voltage
- Amps load or charge/discharge
- Outside air temperature (or owner selectable )
- Fuel flow, units per hour
- Left fuel quantity (or owner selectable)
- Right fuel quantity (or owner selectable)
The Scanner Display has the exhaust gas temperature (EGT) bar graph presentation as its central part with additional Cylinder Head Temperature (CHT) and TIT indications.
Sigma-Tek 5000B Series Attitude Indicators (Artificial Horizons) are air-driven gyros that have a pictorial horizon mask and fixed airplane. The mask moves to indicate climb, dive, and bank. Bank and pitch attitudes are displayed so that the pilot’s sensing of the gyro indication is the same as the interpretation of the relation between the wings of the aircraft and the natural horizon during visual flight. These instruments are FAA certified (TSO-C4c), and can be used to replace the aircraft’s turn coordinator when equipped with an inclinometer. Different versions available mainly based on the layout, dispay colors, warning flag and lighting capabilities. Lighted indicators do not include lamp trays which are sold separately based on the aircraft voltage (14V or 28V).
DUKANE SEACOM, wholly-owned subsidiary of HEICO Corporation, is the world’s leading supplier of FAA / EASA & BSH qualified (Certified) high-impact underwater acoustic beacons for the commercial air transport, business and regional jets, as well as fixed and rotary wing commercial and military markets. Other products in DUKANE SEACOM range include marine underwater beacons for Voyage Data Recorder (VDR) applications and Emergency Locator Transmitters (ELT) separately listed.
The DK120/90 was the first ULB certified to provide a minimum of 90-day underwater operating life. Certified to TSO-C121b & TSO-C142a and ESO ETSO-C121b & ETSO-C142a. Airframe mounted DK180 series low frequency beacon is designed and qualified to meet the newly developed standards FAA TSO-C200 / ETSO-C200 dated 6/26/2012 as per SAE–AS6254 & ARINC 667. For applications not requiring compliance to the 90-day operating requirement, the DUKANE SEACOM DK120/90 and DK140 (short) are still available. An overview of DUKANE SEACOM Aviation Underwater Location Beacons is provided in the Product Description Section.
HONEYWELL BENDIX KING® manufactures a range of TSO'd VOR/LOC/Glidescope indicators. These navigation instruments include VOR/LOC left-right needles, To-From indicator, VOR/LOC warning flag, glideslope deviation needle, glideslope warning flag and 30Hz OBS resolver. Depending on the model, the feature rectilinear instead of pendulum type meter movements for more precise indicator readings, 14/28 volt internal lighting, metal bezel with glass lens and course datum synchro for autopilot use.
These indicators are commonly used with BENDIX KING® remote mounted VOR/LOC converters such as KN-72 or KN-77, remote mounted Glideslope Receivers such as KN-73 or KN-75, KNS-80, KNS-81 nav systems and KX-155/KX-165 NAV/COMM transceivers.
The KI203 model features an internal VOR/ LOC converter and it is compatible with the BENDIX KING® KX155 transceiver. It has a rectilinear meter movement. Compatible with the BENDIX KING KX155 NAV/COMM transceiver.
The KI 204 VOR/LOC/Glideslope Indicator features a built-in VOR/LOC converter and scallop rejection filter, rectilinear needle movement and an optically coated glass lens. Requires input from external glideslope receiver. Compatible with the BENDIX KING® KX 155 or KX 155A NAV/COMMs. Requires input from external glideslope receiver.
The KI 206 VOR/LOC/Glideslope Indicator is rectilinear and internally lighted. It is used with the KNS 80/81 units, KX 165 transceiver and the KNR 634 VOR/LOC/GS/MB receiver. It is available with course datum synchro.
The KI208 model features a built-in VOR/ LOC converter and it is compatible with the BENDIX KING® KX 155 or KX 155A NAV/COMMs. It has a pivoted needle action and a plastic lens.
The KI209 model features an internal VOR/ LOC converter and it is compatible with the BENDIX KING® KX155 transceiver. It features a pivot needle action. The KI209 model includes GPS interface capability.
Range of special accessories by FRANZ AIRCRAFT ENGINES for use in BRP-ROTAX® aircraft engines and other applications.
UNITED INSTRUMENTS 8000/8100 Series Air Speed Indicators (ASI) are FAA TSO'd for installation on certified aircraft.
The 8000 Series ASI indicate the speed relative to the air at sea level altitude. The 8100 Series True ASI indicate the speed relative to the air at sea level or the desired altitude.The indicator has an inner dial to indicate true airspeed. The altitude and temperature are the conversion factors used to obtain this reading with the use of a setting knob.
When properly connected to an airspeed tube, the 8000/8100 Series airspeed indicators measure the differential pressure developed between the pitot and static opening.
The pressure is indicated in units of airspeed mph (M) and/or knots (K).
Product Specifications:
Certification: FAA TSO C2b
Case Configuration: MS33638, 3 inch
Typical Weight: 0.7 pounds
Static, Pitot Pressure Connector: 1/8-27 ANPT
Installation: Removable spring nuts and #6-32 screws
Lighting: Available upon request. All lighted instruments require a light tray sold separately. Please refer to offered SIGMA-TEK 5000B 14V or 28V Light Tray.
HONEYWELL BENDIX KING® KNI-582 Radio Magnetic Indicator (RMI) provides bearing information to either ADF or VOR stations by means of two pointers each of which is read against compass card. The KNI-582 RMI requires inputs from ADF, HSI and NAV receivers and combines three data points on one indicator. The current aircraft heading from an HSI is shown on the card. The magnetic headings to VOR and NDB stations are shown by the twin needles. By combining all this information visually, less interpretation is required thus enhancing overall situational awareness, something especially helpful when the workload is high.
Product Features:
Dual pointer RMI
Accepts AC SIN/COS, DC SIN/COS, Serial, and VOR Composite inputs
Compatible with NAV Receivers such as KN-53, KNS-80, KNS-81, KX-155/165, KX-170B/175B, KNR-615, KNR-630, KNR-634, KNR-665, KNR-665A
Compatible with ADF receivers such as KR-85 (w/ KI-227 -01/04), KR-87, KDF-800/805/8000
Compatible with Compass Systems and NAV indicators such as KCS-305, KCS-55/55A, and KPI-550
Models available with 5 or 28 volt lighting
Models available with black or gray bezel
TACAN compatible and night vision goggle versions available
TSO'd
Specifications:
Altitude: To 50,000 feet
Operating Temperature: -20 to +55°C
Weight: 3.0 lbs. (1.4 kg)
Power Requirements: 28V 4A / 26VAC 6VA
TSO Compliance: Env. Cat. RTCA DO-160A A1D1/A/SKP/XXXXXSABAAA; TSO C6c (compass); TSO C41c Class A (ADF); TSO C40a (VOR)
Compass Heading Input: Operates from any slaved magnetic compass with ARINC X,Y,Z outputs.
The LXNAV G–Meter (accelerometer) is a standalone unit, designed to measure, indicate and log g–forces. The unit is offered in 57 mm or 80 mm diameters for installation into the aircraft instrument panel. It comes in two versions, standard and with flight recorder (FR).
The LXNAV G–Meter has an integrated high precision digital pressure sensor and inertial system. The sensors are sampled more than 100 times per second. Real Time Data is displayed on a QVGA 320x240 pixel 2.5″ high brightness color display. To adjust values and settings the LXNAV g–meter has three push buttons with fixed functions. The top button is ESC (CANCEL), the middle is to switch between modes and the lower button is the ENTER (OK) button.
The unit's inertial platform integrates a ±8g accelerometer. Device is showing current g–load in navbox/needle and it’s min-max values in bar. Last flight min/max load navboxes are persistent till next flight. Min/Max limits with Warning zones can be defined.
Real Time Data is displayed on a QVGA 320×240 pixel 2.5-inch high brightness color display.
The Logbook menu displays the list of flights. If the RTC time is set properly the take-off and landing time shown will be correct. Each flight item consists of the maximum positive g–load, the maximum negative g–load from the flight and the maximum IAS. This function is available only with “FR” version.
Product Features:
• An extremely bright 2.5″ QVGA color display readable in all sunlight conditions with the ability to adjust the backlight.
• Three push buttons are used for input.
• RS232 input/output.
• Micro SD card
• 320x240 pixels color screen for additional information such as minimum and maximum g–force
• Built in RTC (Real time clock)
• Logbook
• 100Hz sampling rate for very fast response.
• Power supply cable included
WULTRAD INC. is a manufacturer of non-certified flight and engine instruments under FALCON GAUGE brand for experimental and homebuilt aircraft. Although their products are Non-TSO, they are made to TSO or MIL specifications for quality.
FALCON GAUGE Non Certified Airspeed Indicators have been one of the most chosen flight instruments by fixed wing airplanes, helicopters and ultralights. The great advantages of these gauges are excellent slow speed characteristics, very progressive increments, a variety of ranges, light weight, short length, and affordable price. FALCON GAUGE Airspeed Indicators ranging up to 80 MPH, 100 MPH, 120 MPH and 150 MPH make for excellent MPH increments for helicopters and ultralight aircraft. All FALCON GAUGE Airspeed Indicators are housed in an aluminum case and consist of all metal parts. They come in 2-1/4" and 3-1/8" sizes. Available ranges: MPH, Knots, KPH; single range or dual range readings. Optional: Custom color range markings can be special ordered. For additional information please refer to the supplied documentation or contact us.
The PAI-700 TSO'd Vertical Card Compass is manufactured exclusively by Precision Aviation, Inc. This non-liquid (dry) type compass is magnet driven thus it is subject to lead and lag, however, these tendencies are greatly reduced due to the absence of pendulosity. It is inherently stable due to the use of eddy current damping which is a natural phenomenon built into the basic design and as such has no overshoot. The PAI-700 has been designed to replace the float/liquid type compasses eliminating leaking fluid or backward azimuth readings. Available for Southern and Northern Hemisphere and different supply systems (5V, 14V and 28V). Precision Avionics Inc. also manufactures different compass brackets for overhead or glare shield mounting.
The Precision PAI-700 Vertical Card Compass consists of a 2" vertical rotating dial which is compared with a fixed miniature airplane (lubber line) to present the magnetic heading of the aircraft at all times. Heading information is more natural because the heading is read at the12 o'clock position and off the nose of the miniature aircraft. The compass card rotates and presents all quadrants in their true relation to line of flight. Requires no power (except for lighting) to operate. Installed in many current production aircraft & helicopters. Size: 2-7/8"H x 2-3/8"W x 2-1/8"D. Wt. 0.6 lb. After installing compass must be compensated using standard compensation procedures. Also used in sailplanes.
Note: Compass deviation card is included. A mount, sold separately, is required for installation with the unit.
KANARDIA HORIS Air Data-Attitude/Heading Reference System (AD-AHRS) includes several state of the art sensors and combines them into a small PFD display. It can serve as standalone PFD displays and it can be used as a primary instrument or as a perfect backup. It is offered as standalone (master) device with integrated sensors or as a slave unit when an I-ALT-IAS or EMSIS PFD or NESIS are present on the CAN bus. AD-AHRS standalone unit shows: attitude (roll, pitch), airspeed (IAS and TAS), vertical speed (Vario) indication, altitude, outside temperature, QNH setting, heading rate (1 minute and 30 seconds turn), tracking course (True or Magnetic). It is offered for two standard panel hole diameters of 57 mm (2.25") and 80 mm (3.15") and comes supplied with digital outside temperature sensor.
Product Features:
very low power consumption (< 2W at 12V),
low cost,
precise altitude pressure and IAS (indicated airspeed) sensor – connects to pitostatic,
precise angular rate sensors – gyros and accelerometers,
GPS receiver,
digital outside temperature sensor,
lightweight design (weighs only 235 g),
CAN bus compatible.
Available Options for HORIS AD-AHRS 57/80 (sold separately). They must be specified at the time of ordering.
MAGU Electronic magnetic compass.
AP-K Two servos for the two axis autopilot function. Must include also AMIGO.
AMIGO Autopilot panel for direct access to Autopilot functions. Must include also AP-K.
The HONEYWELL BENDIX KING® KMT 112 is a Magnetic Azimuth Transmitter (aka Flux Detector or Valve) which senses the direction of the earth’s magnetic field and continuously transmits this information through the slaving circuitry to a directional gyro (such as the HONEYWELL BENDIX KING® KG 102A or KSG 105 slaved directional gyros). This sensor is mounted remotely, usually in a wingtip, to eliminate the possibility of magnetic interference. The KMT 112 is typically used in HONEYWELL BENDIX KING® KCS 55A and KCS 305 compass systems. The KMT-112 flux valve is a sealed unit and cannot be serviced or have parts replaced. The unit must be replaced when/if it fails.
Like other KCS 55A compass system components, the KMT 112 transmitter can be furnished in NEW condition or as USED in Serviceable or Overhauled conditions indicated respectively by the letters "SV" and "OH" in the product reference numbers (SKU and accompanied by the relevant certification (e.g. yellow tag, 8130-3 form). They are also offered as exchanges / trade-ins for returned customer owned units indicated by the letter "EX" in the SKU. In the case of an exchange/trade-in option of a customer unit, the full selling price of the ordered unit is charged and the core credit is refunded or credited towards future orders when our co-operating supplier verifies that the unit is in a reasonable, repairable condition. It is recommended that this option is selected by our customers mainly for upgrades and only in cases when their units are functioning properly at the time removal from the aircraft. In cases when customer units are found by our supplier to be non-repairable, the core deposit shall not be refunded and shipping charges shall apply if customers wish the return of these units to them.
Installation parts and manuals are sold separately.
For additional information and technical specifications please refer to the Product Desscription section, the product presentation of the HONEYWELL BENDIX KING® KCS 55A compass system or contact us.
The KANNAD 406 AS (P/N S1823502-03) is a aeronautical survival beacon. Thanks to its small size and light weight, the Kannad 406 AS fits easily inside a liferaft. It is supplied with a floating collar.
The KANNAD 406 AS is qualified by the French Civil Aviation in Europe with JTSO-2C91a & JTSO-2C126 and by FAA with TSO-C91a & TSO-C126 applied to “survival” beacons.
The ELT is programmed with either the aircraft tail number, a serial number or the aircraft operator designator. It can be installed inside an aircraft on a mounting bracket or in a carry-off bag (both on options).
The mounting bracket option includes a locking pin to avoid accidental activation before ELT removal. The locking pin can be ordered separately with the carry off version.
The ELT can be fitted with a "Water Switch Sensor" to be activated automatically when in contact with water. A buzzer and a led indicate activation.
An integrated “self test” checks the main functions of the beacon. The test result is given by the led flashing sequence.
Product Features:
Battery replacement is only every 6 years.
Precise pinpointing (<1NM) due to the unparalleled frequency accuracy of the 406 transmitter.
Three frequency transmitter (121.5 / 243 / 406 MHz)
Weight (including battery, auxiliary antenna and floating collar) 2.53 lbs (1150 g)
Options:
P/N S18 20 511-03 carry-off bag
P/N S1820511-02 Mounting bracket with locking pin
P/N S1820514-14 Water Switch Sensor