Autopilot computer
$6750
Autopilot computer
Partner Stock
065-00176-7703 is the exact BendixKing Part Number for this KC 140 flight control computer. The unit is a central cockpit component of a compatible KAP 140 automatic flight control installation. It combines the pilot control interface, mode annunciation and flight-control computing functions in a single panel-mounted assembly. The complete Part Number, including the -7703 suffix, should be matched to the aircraft equipment list and approved installation data before ordering.
The KC 140 is not a complete autopilot by itself. It receives pilot selections and system inputs, processes the applicable control logic and sends commands to compatible servos installed in the aircraft control system. Availability of individual modes depends on the aircraft configuration, installed sensors, trim equipment, wiring and approved software or modification status. Similar KC 140 units must not be treated as interchangeable solely because their front panels look alike.
The front panel provides the controls and annunciations used by the crew to engage and monitor the autopilot. The photographed unit includes dedicated AP, HDG, NAV, APR, REV, ALT and ARM controls together with UP and DN selections and a rotary control. These labels identify the functions presented by the exact unit, but actual operation remains governed by the aircraft flight manual supplement and the approved KAP 140 installation.
In a typical installation, the crew selects a lateral or vertical mode at the KC 140. The computer evaluates the selected command together with the available heading, navigation, altitude and attitude-related inputs. It then develops servo commands for the applicable control axis. The annunciation window reports selected or captured modes so that the pilot can supervise system operation. Manual trim requirements and disconnect logic remain part of the complete aircraft installation.
A practical system chain is pilot selection and aircraft sensor input → KC 140 flight control computer → compatible roll, pitch and trim servos → aircraft control linkage. The precise connected units vary by approved installation. A KS 270-series pitch servo or KS 272C trim servo may be present in compatible BendixKing systems, but their use with a particular aircraft must be verified by complete Part Number, wiring diagram and supplemental type-certificate data.
The computer also depends on correct aircraft power, grounding, circuit protection and connector wiring. Troubleshooting should therefore consider the whole system rather than the panel alone. A mode that will not engage can be caused by an external sensor, servo, trim circuit, disconnect switch, wiring fault or installation interlock. Bench testing and return-to-service decisions require the applicable BendixKing maintenance data and approved test equipment.
The original identification plate on the illustrated unit reads KC 140 Flight Control Computer and shows exact Part Number 065-00176-7703. It specifies maximum DC input of 28 V / 1.0 A or 14 V / 1.5 A. The plate also carries TSO C9c, RTCA DO-160C and DO-178B Level C references. These details are taken directly from the photographed equipment and are not transferred from another KC 140 suffix.
The photographed serial number is 4534. The face and plate images preserve the original Bendix/King markings, controls, display window, fasteners and case construction. Exact rear-connector pin assignments, mounting dimensions and clearance requirements should be taken from the installation drawing applicable to 065-00176-7703. No reliable suffix-specific dimensional values were added where the reviewed documentation did not provide them.
This 065-00176-7703 KC 140 is offered in Serviceable condition from partner stock with a six-month warranty. The price is based on the confirmed offer-list position and the comparable same-condition market check. The images show the exact photographed unit; release documentation, bench-test records and serial-number allocation are confirmed for the unit supplied with the quotation.
For an inquiry, state Part Number 065-00176-7703, model KC 140, quantity, aircraft type and required paperwork. Servos, mounting hardware, mating connector, sensors and associated harnesses are included only when expressly listed. Other identified flight-control components can be reviewed in the Garmin / BendixKing / Honeywell / Collins category. Related products may work in the same autopilot system, but they are not automatically interchangeable.
Product Type: Panel-mounted autopilot flight control computer
Manufacturer: BendixKing / Honeywell
Model: KC 140
Designation: 065-00176-7703
Alternative Designations: KC140; KC-140; 065001767703; Bendix/King KC 140
Main Function: Pilot interface, mode annunciation and flight-control computation in a compatible KAP 140 installation
Associated System: KAP 140 automatic flight control system where approved
Installation Type: Panel-mounted cockpit flight control computer
Typical Signal Chain: Pilot selections and aircraft sensor inputs → KC 140 computer → compatible flight-control servos → aircraft control linkage
Front-Panel Controls: AP, HDG, NAV, APR, REV, ALT, ARM, UP and DN selections with rotary control
Maximum DC Input at 28 V: 28 V DC / 1.0 A according to the exact identification plate
Maximum DC Input at 14 V: 14 V DC / 1.5 A according to the exact identification plate
Qualification Markings: TSO C9c; RTCA DO-160C; DO-178B Level C according to the exact plate
Photographed Serial Number: 4534
Compatible Servos: Installation-specific BendixKing flight-control and trim servos only where approved
Exact Dimensions: Refer to the installation drawing applicable to 065-00176-7703
Connector and Pin Assignment: Verify through the applicable KC 140 / KAP 140 installation data
Interchangeability: Complete suffix, modification status, wiring and aircraft approval must be verified
Condition: Serviceable
Warranty: 6 Months
Delivery Set: Servos, mounting hardware, connector, sensors and harnesses only when expressly included in the quotation
Technical Documentation: KC 140 / KAP 140 installation, operating and maintenance data applicable to 065-00176-7703
All shipments are carried out from our international warehouse in Dubai (UAE), as well as from our partners’ remote warehouses.
In Stock — items available in stock at the Dubai warehouse are dispatched within 5–10 business days after receiving 100% prepayment.
Remote Stock — items available at our partners’ remote warehouses are supplied within an average of 30–45 business days after receiving 100% prepayment.
Pre-Order — made-to-order products are manufactured and delivered within an average of 45–60 business days. Payment terms: 50% advance payment to start production, with the remaining 50% paid before dispatch from the Dubai warehouse after full readiness for shipment.
Returns & Changes (Restocking Fee)
For selected items, a RESTOCKING FEE of 10% may apply in case of return, order cancellation, or changes to the order specifications. This condition applies only to certain products and is confirmed at the order approval stage.
Warranty
All products are covered by a standard 6-month warranty.
Extended warranty is available upon request and is agreed individually; it may affect the final product price.
065-00176-7703 is the exact BendixKing Part Number for this KC 140 flight control computer. The unit is a central cockpit component of a compatible KAP 140 automatic flight control installation. It combines the pilot control interface, mode annunciation and flight-control computing functions in a single panel-mounted assembly. The complete Part Number, including the -7703 suffix, should be matched to the aircraft equipment list and approved installation data before ordering.
The KC 140 is not a complete autopilot by itself. It receives pilot selections and system inputs, processes the applicable control logic and sends commands to compatible servos installed in the aircraft control system. Availability of individual modes depends on the aircraft configuration, installed sensors, trim equipment, wiring and approved software or modification status. Similar KC 140 units must not be treated as interchangeable solely because their front panels look alike.
The front panel provides the controls and annunciations used by the crew to engage and monitor the autopilot. The photographed unit includes dedicated AP, HDG, NAV, APR, REV, ALT and ARM controls together with UP and DN selections and a rotary control. These labels identify the functions presented by the exact unit, but actual operation remains governed by the aircraft flight manual supplement and the approved KAP 140 installation.
In a typical installation, the crew selects a lateral or vertical mode at the KC 140. The computer evaluates the selected command together with the available heading, navigation, altitude and attitude-related inputs. It then develops servo commands for the applicable control axis. The annunciation window reports selected or captured modes so that the pilot can supervise system operation. Manual trim requirements and disconnect logic remain part of the complete aircraft installation.
A practical system chain is pilot selection and aircraft sensor input → KC 140 flight control computer → compatible roll, pitch and trim servos → aircraft control linkage. The precise connected units vary by approved installation. A KS 270-series pitch servo or KS 272C trim servo may be present in compatible BendixKing systems, but their use with a particular aircraft must be verified by complete Part Number, wiring diagram and supplemental type-certificate data.
The computer also depends on correct aircraft power, grounding, circuit protection and connector wiring. Troubleshooting should therefore consider the whole system rather than the panel alone. A mode that will not engage can be caused by an external sensor, servo, trim circuit, disconnect switch, wiring fault or installation interlock. Bench testing and return-to-service decisions require the applicable BendixKing maintenance data and approved test equipment.
The original identification plate on the illustrated unit reads KC 140 Flight Control Computer and shows exact Part Number 065-00176-7703. It specifies maximum DC input of 28 V / 1.0 A or 14 V / 1.5 A. The plate also carries TSO C9c, RTCA DO-160C and DO-178B Level C references. These details are taken directly from the photographed equipment and are not transferred from another KC 140 suffix.
The photographed serial number is 4534. The face and plate images preserve the original Bendix/King markings, controls, display window, fasteners and case construction. Exact rear-connector pin assignments, mounting dimensions and clearance requirements should be taken from the installation drawing applicable to 065-00176-7703. No reliable suffix-specific dimensional values were added where the reviewed documentation did not provide them.
This 065-00176-7703 KC 140 is offered in Serviceable condition from partner stock with a six-month warranty. The price is based on the confirmed offer-list position and the comparable same-condition market check. The images show the exact photographed unit; release documentation, bench-test records and serial-number allocation are confirmed for the unit supplied with the quotation.
For an inquiry, state Part Number 065-00176-7703, model KC 140, quantity, aircraft type and required paperwork. Servos, mounting hardware, mating connector, sensors and associated harnesses are included only when expressly listed. Other identified flight-control components can be reviewed in the Garmin / BendixKing / Honeywell / Collins category. Related products may work in the same autopilot system, but they are not automatically interchangeable.
Product Type: Panel-mounted autopilot flight control computer
Manufacturer: BendixKing / Honeywell
Model: KC 140
Designation: 065-00176-7703
Alternative Designations: KC140; KC-140; 065001767703; Bendix/King KC 140
Main Function: Pilot interface, mode annunciation and flight-control computation in a compatible KAP 140 installation
Associated System: KAP 140 automatic flight control system where approved
Installation Type: Panel-mounted cockpit flight control computer
Typical Signal Chain: Pilot selections and aircraft sensor inputs → KC 140 computer → compatible flight-control servos → aircraft control linkage
Front-Panel Controls: AP, HDG, NAV, APR, REV, ALT, ARM, UP and DN selections with rotary control
Maximum DC Input at 28 V: 28 V DC / 1.0 A according to the exact identification plate
Maximum DC Input at 14 V: 14 V DC / 1.5 A according to the exact identification plate
Qualification Markings: TSO C9c; RTCA DO-160C; DO-178B Level C according to the exact plate
Photographed Serial Number: 4534
Compatible Servos: Installation-specific BendixKing flight-control and trim servos only where approved
Exact Dimensions: Refer to the installation drawing applicable to 065-00176-7703
Connector and Pin Assignment: Verify through the applicable KC 140 / KAP 140 installation data
Interchangeability: Complete suffix, modification status, wiring and aircraft approval must be verified
Condition: Serviceable
Warranty: 6 Months
Delivery Set: Servos, mounting hardware, connector, sensors and harnesses only when expressly included in the quotation
Technical Documentation: KC 140 / KAP 140 installation, operating and maintenance data applicable to 065-00176-7703
All shipments are carried out from our international warehouse in Dubai (UAE), as well as from our partners’ remote warehouses.
In Stock — items available in stock at the Dubai warehouse are dispatched within 5–10 business days after receiving 100% prepayment.
Remote Stock — items available at our partners’ remote warehouses are supplied within an average of 30–45 business days after receiving 100% prepayment.
Pre-Order — made-to-order products are manufactured and delivered within an average of 45–60 business days. Payment terms: 50% advance payment to start production, with the remaining 50% paid before dispatch from the Dubai warehouse after full readiness for shipment.
Returns & Changes (Restocking Fee)
For selected items, a RESTOCKING FEE of 10% may apply in case of return, order cancellation, or changes to the order specifications. This condition applies only to certain products and is confirmed at the order approval stage.
Warranty
All products are covered by a standard 6-month warranty.
Extended warranty is available upon request and is agreed individually; it may affect the final product price.