Autopilot trim servo
$3315
Autopilot trim servo
Partner Stock
065-00180-2700 is the exact BendixKing Part Number for this KS 272C electric trim servo. The unit is used in compatible automatic flight control installations to operate the aircraft pitch-trim mechanism when commanded by the approved autopilot or manual electric-trim circuit. The complete -2700 suffix identifies the configuration and must be retained when comparing equipment lists, repair records and replacement stock.
The KS 272C is an actuator rather than an independent flight-control computer. It converts an electrical trim command into controlled mechanical movement at the aircraft trim system. Correct operation depends on the installed flight-control computer, switches, disconnect logic, circuit protection, clutch circuit, wiring and mechanical connection. A visually similar KS 272C with another suffix should not be assumed to have identical gearing, clutch arrangement or installation approval.
In a typical approved system, a pitch-related command is processed by the autopilot computer. When trim correction is required, the electrical command is routed to the KS 272C. The servo motor and transmission move the connected trim mechanism, while the clutch allows the unit to engage or release in accordance with the installed system logic. Manual electric-trim commands can also use the servo where the aircraft wiring provides this function.
A simplified functional chain is autopilot computer or manual trim switch → aircraft wiring and protection → KS 272C trim servo → trim cable, chain or mechanical linkage → pitch-trim surface or mechanism. The exact arrangement differs among aircraft installations. It must be checked against the aircraft maintenance manual and BendixKing installation data before replacing, rigging or functionally testing the unit.
The exact identification plate on the photographed 065-00180-2700 unit specifies 28 V DC input and a 4 A rating. Reviewed KS 272C maintenance information lists a manual-trim operating-voltage range of 18.5 to 25.5 V and identifies clutch control at connector pin F for the applicable test procedure. These figures describe controlled shop or system checks and do not replace aircraft-specific circuit limits.
The same maintenance data gives an output speed of one revolution in 17 to 20.5 seconds and a load reference of 80 lb, equivalent to 71 in-lb for the documented test. These values are useful for identifying correct servo response during approved bench testing. They should not be converted into installation limits without considering the specified fixture, supply voltage, clutch state and applicable revision of the maintenance manual.
The photographed plate reads KS 272C Trim Servo, Part Number 065-00180-2700 and serial number 3309. It also carries TSO C9c and DO-160C references and identifies Honeywell International. The gallery image preserves the actual plate rather than replacing it with a label from another KS 272C suffix. This is important because suffix-level configuration cannot be established from the housing alone.
Installation inspection should include the mounting points, output coupling, wiring condition, connector security, clutch operation, travel limits and trim-system rigging. Uncommanded movement, abnormal running time or clutch slip can originate outside the servo as well as inside it. Exact dimensions, connector pin functions and rigging values are therefore left to the approved KS 272C and aircraft documentation where the reviewed open sources did not provide dependable suffix-specific figures.
This 065-00180-2700 KS 272C is offered in Serviceable condition from partner stock with a six-month warranty. The price follows the agreed rule and uses the higher value between the offer list and 1.7 times the exact same-condition public comparison. Photographs show the authentic unit and exact plate; allocated serial number and release documents are reconfirmed before shipment.
For a quotation, specify Part Number 065-00180-2700, model KS 272C, quantity, aircraft application and paperwork requirement. Mounting brackets, cable or chain hardware, mating connector, controller and other autopilot units are supplied only when explicitly stated. Related flight-control equipment can be reviewed in the Garmin / BendixKing / Honeywell / Collins category. Related items may belong to the same system but are not automatically interchangeable.
Product Type: Electric pitch-trim servo
Manufacturer: BendixKing / Honeywell
Model: KS 272C
Designation: 065-00180-2700
Alternative Designations: KS272C; KS-272C; 065001802700; Bendix/King KS 272C
Main Function: Converts approved automatic or manual electric-trim commands into mechanical pitch-trim movement
Installation Type: Remotely mounted autopilot trim actuator
Typical Signal Chain: Autopilot computer or manual trim switch → KS 272C trim servo → aircraft pitch-trim linkage
DC Input: 28 V DC according to the exact identification plate
Current Rating: 4 A according to the exact identification plate
Manual Trim Test Voltage: 18.5 to 25.5 V according to reviewed KS 272C maintenance data
Output Speed: 1 revolution in 17 to 20.5 seconds under the documented test conditions
Documented Test Load: 80 lb / 71 in-lb
Clutch Test Reference: Connector pin F in the applicable KS 272C test procedure
Qualification Markings: TSO C9c and DO-160C according to the exact plate
Photographed Serial Number: 3309
Exact Dimensions: Refer to the installation drawing applicable to 065-00180-2700
Connector and Pin Assignment: Verify through the applicable KS 272C installation and maintenance data
Interchangeability: Complete suffix, gearing, clutch arrangement, mounting and aircraft approval must be verified
Condition: Serviceable
Warranty: 6 Months
Delivery Set: Mounting hardware, linkage parts, connector, controller and documentation only when expressly included in the quotation
Technical Documentation: KS 272C installation and maintenance data applicable to 065-00180-2700
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.
065-00180-2700 is the exact BendixKing Part Number for this KS 272C electric trim servo. The unit is used in compatible automatic flight control installations to operate the aircraft pitch-trim mechanism when commanded by the approved autopilot or manual electric-trim circuit. The complete -2700 suffix identifies the configuration and must be retained when comparing equipment lists, repair records and replacement stock.
The KS 272C is an actuator rather than an independent flight-control computer. It converts an electrical trim command into controlled mechanical movement at the aircraft trim system. Correct operation depends on the installed flight-control computer, switches, disconnect logic, circuit protection, clutch circuit, wiring and mechanical connection. A visually similar KS 272C with another suffix should not be assumed to have identical gearing, clutch arrangement or installation approval.
In a typical approved system, a pitch-related command is processed by the autopilot computer. When trim correction is required, the electrical command is routed to the KS 272C. The servo motor and transmission move the connected trim mechanism, while the clutch allows the unit to engage or release in accordance with the installed system logic. Manual electric-trim commands can also use the servo where the aircraft wiring provides this function.
A simplified functional chain is autopilot computer or manual trim switch → aircraft wiring and protection → KS 272C trim servo → trim cable, chain or mechanical linkage → pitch-trim surface or mechanism. The exact arrangement differs among aircraft installations. It must be checked against the aircraft maintenance manual and BendixKing installation data before replacing, rigging or functionally testing the unit.
The exact identification plate on the photographed 065-00180-2700 unit specifies 28 V DC input and a 4 A rating. Reviewed KS 272C maintenance information lists a manual-trim operating-voltage range of 18.5 to 25.5 V and identifies clutch control at connector pin F for the applicable test procedure. These figures describe controlled shop or system checks and do not replace aircraft-specific circuit limits.
The same maintenance data gives an output speed of one revolution in 17 to 20.5 seconds and a load reference of 80 lb, equivalent to 71 in-lb for the documented test. These values are useful for identifying correct servo response during approved bench testing. They should not be converted into installation limits without considering the specified fixture, supply voltage, clutch state and applicable revision of the maintenance manual.
The photographed plate reads KS 272C Trim Servo, Part Number 065-00180-2700 and serial number 3309. It also carries TSO C9c and DO-160C references and identifies Honeywell International. The gallery image preserves the actual plate rather than replacing it with a label from another KS 272C suffix. This is important because suffix-level configuration cannot be established from the housing alone.
Installation inspection should include the mounting points, output coupling, wiring condition, connector security, clutch operation, travel limits and trim-system rigging. Uncommanded movement, abnormal running time or clutch slip can originate outside the servo as well as inside it. Exact dimensions, connector pin functions and rigging values are therefore left to the approved KS 272C and aircraft documentation where the reviewed open sources did not provide dependable suffix-specific figures.
This 065-00180-2700 KS 272C is offered in Serviceable condition from partner stock with a six-month warranty. The price follows the agreed rule and uses the higher value between the offer list and 1.7 times the exact same-condition public comparison. Photographs show the authentic unit and exact plate; allocated serial number and release documents are reconfirmed before shipment.
For a quotation, specify Part Number 065-00180-2700, model KS 272C, quantity, aircraft application and paperwork requirement. Mounting brackets, cable or chain hardware, mating connector, controller and other autopilot units are supplied only when explicitly stated. Related flight-control equipment can be reviewed in the Garmin / BendixKing / Honeywell / Collins category. Related items may belong to the same system but are not automatically interchangeable.
Product Type: Electric pitch-trim servo
Manufacturer: BendixKing / Honeywell
Model: KS 272C
Designation: 065-00180-2700
Alternative Designations: KS272C; KS-272C; 065001802700; Bendix/King KS 272C
Main Function: Converts approved automatic or manual electric-trim commands into mechanical pitch-trim movement
Installation Type: Remotely mounted autopilot trim actuator
Typical Signal Chain: Autopilot computer or manual trim switch → KS 272C trim servo → aircraft pitch-trim linkage
DC Input: 28 V DC according to the exact identification plate
Current Rating: 4 A according to the exact identification plate
Manual Trim Test Voltage: 18.5 to 25.5 V according to reviewed KS 272C maintenance data
Output Speed: 1 revolution in 17 to 20.5 seconds under the documented test conditions
Documented Test Load: 80 lb / 71 in-lb
Clutch Test Reference: Connector pin F in the applicable KS 272C test procedure
Qualification Markings: TSO C9c and DO-160C according to the exact plate
Photographed Serial Number: 3309
Exact Dimensions: Refer to the installation drawing applicable to 065-00180-2700
Connector and Pin Assignment: Verify through the applicable KS 272C installation and maintenance data
Interchangeability: Complete suffix, gearing, clutch arrangement, mounting and aircraft approval must be verified
Condition: Serviceable
Warranty: 6 Months
Delivery Set: Mounting hardware, linkage parts, connector, controller and documentation only when expressly included in the quotation
Technical Documentation: KS 272C installation and maintenance data applicable to 065-00180-2700
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.