Combined control actuator
KAU-115AM
Price on request
Combined control actuator
Out of stock
Description
KAU-115AM combined hydraulic actuator for helicopter controls
The KAU-115AM is a combined hydraulic control actuator used in helicopter flight control systems. It moves the working elements of the main rotor control system and is connected with the mechanical control linkage from the pilot. This is not a simple hydraulic cylinder. The unit works as a powered control actuator where mechanical input, hydraulic pressure, and electrical correction signals meet in one assembly. In Mi-family helicopters, this type of actuator is used where the control system requires hydraulic force and automatic correction.
Mechanical and combined control through KAU-115AM
In mechanical-hydraulic mode, the KAU-115AM transmits pilot input from the control linkage and uses hydraulic pressure to move the connected mechanism. In combined mode, the same actuator also receives correction signals from the flight-navigation complex. These signals are added to the mechanical control path and allow the system to correct the position of the controlled element. The actuator itself does not create pressure. It uses hydraulic supply from the helicopter system and converts control input into movement of the output rod.
Flight control channels with KAU-115AM installed
The KAU-115AM operates in the longitudinal, lateral, directional, and collective pitch control channels. In these channels it works with control rods, bellcranks, hydraulic supply and drain lines, feedback elements, and correction circuits. If one control channel behaves incorrectly, the cause is not always the actuator. Maintenance checks normally include supply pressure, drain pressure, output rod travel, fluid condition, linkage adjustment, electrical signal wiring, and the condition of connected mechanical parts.
Helicopter application of actuator KAU-115AM
The KAU-115AM is used on Mi-family helicopters, including Mi-8, Mi-10, Mi-6, and Mi-171 helicopters. Technical references describe it as an actuator for the main rotor control elements in longitudinal, lateral, directional, and collective pitch channels. In Mi-8AMT documentation, KAU-115AM is listed with KAU-30B and RA-60B as part of the irreversible flight control system. Exact installation and quantity should still be checked by the aircraft parts catalog and maintenance documentation.
Identification and ordering checks for KAU-115AM
Before ordering, the marking on the installed actuator should be compared with the helicopter passport, parts catalog, or official technical documentation. The product may appear in supply documents as KAU115AM, KAU 115AM, KAU-115-AM, or KAU115-AM. In Russian documentation, the same product is written as КАУ-115АМ, КАУ115АМ, or КАУ 115АМ. A clear request should include the helicopter type, channel of installation, full designation, and a photo of the data plate if available.
Details
Product Type: Combined hydraulic control actuator
Function: Actuation of helicopter flight control mechanisms
Application / Where Used: Helicopter flight control systems
System / Installation Area: Hydraulic flight control system
Compatible Aircraft / Equipment: Mi-8, Mi-10, Mi-6, Mi-171 helicopters
Working Medium: AMG-10 hydraulic oil
Supply Line Pressure: 4.2 to 8.5 MPa
Drain Line Pressure: 0 to 0.5 MPa
Operating Temperature Range (Hydraulic Fluid): −10 to +80 °C operating; −60 to +80 °C limit
Operating Temperature Range (Ambient): −60 to +60 °C
Nominal Control Signal: 3 mA
Maximum Output Rod Stroke: 74 ± 0.5 mm
Maximum Developed Force: Not less than 17,000 N
Weight: Not more than 11 kg
Interchangeability / Replaceability: Interchangeable with KAU-30B and RA-60B
Assigned Resource: 1,500 h before first overhaul
Inter-Overhaul Resource: 1,500 h
Assigned Service Life: 30 years
Storage Life: 10 years
Scope of Supply: Combined hydraulic control actuator, passport
Technical Documentation: Passport KAU115AM-000 PS
Payment & delivery
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.
- Description
- Details
- Payment & delivery
KAU-115AM combined hydraulic actuator for helicopter controls
The KAU-115AM is a combined hydraulic control actuator used in helicopter flight control systems. It moves the working elements of the main rotor control system and is connected with the mechanical control linkage from the pilot. This is not a simple hydraulic cylinder. The unit works as a powered control actuator where mechanical input, hydraulic pressure, and electrical correction signals meet in one assembly. In Mi-family helicopters, this type of actuator is used where the control system requires hydraulic force and automatic correction.
Mechanical and combined control through KAU-115AM
In mechanical-hydraulic mode, the KAU-115AM transmits pilot input from the control linkage and uses hydraulic pressure to move the connected mechanism. In combined mode, the same actuator also receives correction signals from the flight-navigation complex. These signals are added to the mechanical control path and allow the system to correct the position of the controlled element. The actuator itself does not create pressure. It uses hydraulic supply from the helicopter system and converts control input into movement of the output rod.
Flight control channels with KAU-115AM installed
The KAU-115AM operates in the longitudinal, lateral, directional, and collective pitch control channels. In these channels it works with control rods, bellcranks, hydraulic supply and drain lines, feedback elements, and correction circuits. If one control channel behaves incorrectly, the cause is not always the actuator. Maintenance checks normally include supply pressure, drain pressure, output rod travel, fluid condition, linkage adjustment, electrical signal wiring, and the condition of connected mechanical parts.
Helicopter application of actuator KAU-115AM
The KAU-115AM is used on Mi-family helicopters, including Mi-8, Mi-10, Mi-6, and Mi-171 helicopters. Technical references describe it as an actuator for the main rotor control elements in longitudinal, lateral, directional, and collective pitch channels. In Mi-8AMT documentation, KAU-115AM is listed with KAU-30B and RA-60B as part of the irreversible flight control system. Exact installation and quantity should still be checked by the aircraft parts catalog and maintenance documentation.
Identification and ordering checks for KAU-115AM
Before ordering, the marking on the installed actuator should be compared with the helicopter passport, parts catalog, or official technical documentation. The product may appear in supply documents as KAU115AM, KAU 115AM, KAU-115-AM, or KAU115-AM. In Russian documentation, the same product is written as КАУ-115АМ, КАУ115АМ, or КАУ 115АМ. A clear request should include the helicopter type, channel of installation, full designation, and a photo of the data plate if available.
Product Type: Combined hydraulic control actuator
Function: Actuation of helicopter flight control mechanisms
Application / Where Used: Helicopter flight control systems
System / Installation Area: Hydraulic flight control system
Compatible Aircraft / Equipment: Mi-8, Mi-10, Mi-6, Mi-171 helicopters
Working Medium: AMG-10 hydraulic oil
Supply Line Pressure: 4.2 to 8.5 MPa
Drain Line Pressure: 0 to 0.5 MPa
Operating Temperature Range (Hydraulic Fluid): −10 to +80 °C operating; −60 to +80 °C limit
Operating Temperature Range (Ambient): −60 to +60 °C
Nominal Control Signal: 3 mA
Maximum Output Rod Stroke: 74 ± 0.5 mm
Maximum Developed Force: Not less than 17,000 N
Weight: Not more than 11 kg
Interchangeability / Replaceability: Interchangeable with KAU-30B and RA-60B
Assigned Resource: 1,500 h before first overhaul
Inter-Overhaul Resource: 1,500 h
Assigned Service Life: 30 years
Storage Life: 10 years
Scope of Supply: Combined hydraulic control actuator, passport
Technical Documentation: Passport KAU115AM-000 PS
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.