Swash plate assembly
Price on request
Swash plate assembly
8-1950-000 is a helicopter swash plate assembly used in the main rotor control system of Mi-8 family helicopters and related variants. The unit converts control inputs from the cockpit and hydraulic booster system into controlled changes of main rotor blade pitch. Through this mechanism, the helicopter can change collective pitch for lift control and cyclic pitch for maneuvering. The swash plate works between the non-rotating control system and the rotating rotor head, so it is one of the main mechanical interfaces between pilot command and rotor blade response.
The 8-1950-000 assembly changes the pitch of the main rotor blades in two ways. Collective movement changes the pitch of all blades together, which affects lift and allows the helicopter to climb, descend or maintain hover. Cyclic movement changes blade pitch depending on the blade’s azimuth position during rotation, which allows the rotor disc to tilt and the helicopter to maneuver. The swash plate must transmit these inputs smoothly and accurately, because any play, binding, bearing wear or incorrect adjustment can affect control response and rotor stability.
The 8-1950-000 swash plate assembly includes stationary and rotating components connected through bearings. The stationary part receives motion from the flight control system and hydraulic boosters, while the rotating part follows the main rotor rotation and transmits movement to the blade pitch links. This arrangement allows non-rotating cockpit commands to be passed into the rotating rotor head. The assembly must maintain correct geometry while operating under continuous rotation, vibration and changing aerodynamic loads. For this reason, bearing condition, lubrication, slider movement and pitch link guide condition are important during inspection.
The 8-1950-000 assembly consists of a rotating plate, stationary plate, bearing elements, pitch link guides and a linear slider. These parts work together to provide axial movement and tilting of the swash plate according to pilot inputs. The slider travel and tilt limits define the permitted control movement range of the assembly. Since the mechanism is connected directly with main rotor blade pitch control, its adjustment must correspond to aircraft maintenance documentation. Incorrect installation or deviation from permitted movement limits may affect blade incidence, control range and flight safety.
The 8-1950-000 swash plate assembly is used on Mi-8, Mi-17, Mi-171 and corresponding modifications equipped with compatible main rotor control systems. It operates as part of the primary flight control system and main rotor pitch-control transmission. Because helicopters may differ by modification, overhaul history, control system configuration and service bulletin status, applicability should be confirmed by the aircraft parts catalog and technical documentation before ordering or installation. A visually similar swash plate should not be treated as interchangeable without confirming the exact designation and approved configuration.
The assembly may be referenced under designations 8-1950-000, 8-1950-000 PS and 81950000. These references relate to the same swash plate assembly, but the passport designation, condition and documentation set should still be confirmed before supply. For correct ordering, it is useful to specify the helicopter type, required condition, passport availability, overhaul status, completeness and whether the unit is needed for operational replacement, overhaul stock or repair support. Since the swash plate is a flight-control component, traceable documentation and maintenance records are important for acceptance.
Product Type: Swash plate assembly
Designation: 8-1950-000
Alternative Designations: 8-1950-000 PS, 81950000
Function: Collective and cyclic pitch control of main rotor blades
Application / Where Used: Main rotor flight control system
System / Installation Area: Main rotor control and swash plate transmission system
Compatible Aircraft / Equipment: Mi-8, Mi-17, Mi-171 and corresponding modifications
Operating Role: Conversion of pilot and hydraulic booster inputs into main rotor blade pitch changes
Main Components: Rotating plate, stationary plate, bearings, pitch link guides, linear slider
Main Rotor Direction, Referenced: Clockwise when viewed from above, according to passport reference
Nominal Rotor Speed: 192 rpm
Pitch Plate Tilt Limit, Forward: 9°30′
Pitch Plate Tilt Limit, Back: 7°00′
Pitch Plate Tilt Limit, Right: 6°30′
Pitch Plate Tilt Limit, Left: 6°30′
Swash Plate Slider Travel: 8.5 mm
Lubrication: CIATIM-201 grease
Lubrication Standard: GOST 6267-74
Mass with Grease: 122 kg
Measured Mass, Factory Logged: 122 kg
Precious Metals Content: None
Material Composition: Aluminum approx. 27.04 kg; bronze approx. 1.538 kg
Condition: As applicable
Documentation: Factory passport, operating forms, maintenance forms, aircraft parts catalog
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.
8-1950-000 is a helicopter swash plate assembly used in the main rotor control system of Mi-8 family helicopters and related variants. The unit converts control inputs from the cockpit and hydraulic booster system into controlled changes of main rotor blade pitch. Through this mechanism, the helicopter can change collective pitch for lift control and cyclic pitch for maneuvering. The swash plate works between the non-rotating control system and the rotating rotor head, so it is one of the main mechanical interfaces between pilot command and rotor blade response.
The 8-1950-000 assembly changes the pitch of the main rotor blades in two ways. Collective movement changes the pitch of all blades together, which affects lift and allows the helicopter to climb, descend or maintain hover. Cyclic movement changes blade pitch depending on the blade’s azimuth position during rotation, which allows the rotor disc to tilt and the helicopter to maneuver. The swash plate must transmit these inputs smoothly and accurately, because any play, binding, bearing wear or incorrect adjustment can affect control response and rotor stability.
The 8-1950-000 swash plate assembly includes stationary and rotating components connected through bearings. The stationary part receives motion from the flight control system and hydraulic boosters, while the rotating part follows the main rotor rotation and transmits movement to the blade pitch links. This arrangement allows non-rotating cockpit commands to be passed into the rotating rotor head. The assembly must maintain correct geometry while operating under continuous rotation, vibration and changing aerodynamic loads. For this reason, bearing condition, lubrication, slider movement and pitch link guide condition are important during inspection.
The 8-1950-000 assembly consists of a rotating plate, stationary plate, bearing elements, pitch link guides and a linear slider. These parts work together to provide axial movement and tilting of the swash plate according to pilot inputs. The slider travel and tilt limits define the permitted control movement range of the assembly. Since the mechanism is connected directly with main rotor blade pitch control, its adjustment must correspond to aircraft maintenance documentation. Incorrect installation or deviation from permitted movement limits may affect blade incidence, control range and flight safety.
The 8-1950-000 swash plate assembly is used on Mi-8, Mi-17, Mi-171 and corresponding modifications equipped with compatible main rotor control systems. It operates as part of the primary flight control system and main rotor pitch-control transmission. Because helicopters may differ by modification, overhaul history, control system configuration and service bulletin status, applicability should be confirmed by the aircraft parts catalog and technical documentation before ordering or installation. A visually similar swash plate should not be treated as interchangeable without confirming the exact designation and approved configuration.
The assembly may be referenced under designations 8-1950-000, 8-1950-000 PS and 81950000. These references relate to the same swash plate assembly, but the passport designation, condition and documentation set should still be confirmed before supply. For correct ordering, it is useful to specify the helicopter type, required condition, passport availability, overhaul status, completeness and whether the unit is needed for operational replacement, overhaul stock or repair support. Since the swash plate is a flight-control component, traceable documentation and maintenance records are important for acceptance.
Product Type: Swash plate assembly
Designation: 8-1950-000
Alternative Designations: 8-1950-000 PS, 81950000
Function: Collective and cyclic pitch control of main rotor blades
Application / Where Used: Main rotor flight control system
System / Installation Area: Main rotor control and swash plate transmission system
Compatible Aircraft / Equipment: Mi-8, Mi-17, Mi-171 and corresponding modifications
Operating Role: Conversion of pilot and hydraulic booster inputs into main rotor blade pitch changes
Main Components: Rotating plate, stationary plate, bearings, pitch link guides, linear slider
Main Rotor Direction, Referenced: Clockwise when viewed from above, according to passport reference
Nominal Rotor Speed: 192 rpm
Pitch Plate Tilt Limit, Forward: 9°30′
Pitch Plate Tilt Limit, Back: 7°00′
Pitch Plate Tilt Limit, Right: 6°30′
Pitch Plate Tilt Limit, Left: 6°30′
Swash Plate Slider Travel: 8.5 mm
Lubrication: CIATIM-201 grease
Lubrication Standard: GOST 6267-74
Mass with Grease: 122 kg
Measured Mass, Factory Logged: 122 kg
Precious Metals Content: None
Material Composition: Aluminum approx. 27.04 kg; bronze approx. 1.538 kg
Condition: As applicable
Documentation: Factory passport, operating forms, maintenance forms, aircraft parts catalog
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.