6S2.390.126 Series 4 / PU-126
control panel
Description
6S2.390.126 Series 4 PU-126 control panel
6S2.390.126 Series 4 is the decimal number of the PU-126 aircraft control panel. The unit is used as a cockpit control and switching panel in helicopter flight control and autopilot-related systems. It is associated with Russian-made civil and military helicopters, including Mi and Ka helicopter types, where the relevant flight control, stabilization or autopilot equipment is installed according to aircraft documentation.
Full descriptionCollapse description
PU-126 function in helicopter control systems
The PU-126 control panel is intended for selection of operating modes, switching of control functions and generation of command signals for helicopter stabilization and semi-automatic control systems. The panel supports crew interaction with the connected autopilot / flight control equipment and allows control of flight stabilization functions in several channels. It is not a standalone autopilot computer; it operates as a cockpit interface unit within a larger flight control system.
Application with PKV-252 and VUAP-1 systems
The 6S2.390.126 Series 4 panel may be used as part of PKV-252 / PKV-252-1 flight control complexes and VUAP-1 unified helicopter autopilot systems, depending on aircraft configuration. It may operate together with related equipment such as 6S2.390.125 series panels, BK-252 switching units, VDU-252 director control computers and feedback sensors. Exact compatibility should be confirmed by the aircraft equipment list, autopilot documentation and product passport.
Control channels of PU-126
The PU-126 panel supports control and switching functions related to the main helicopter stabilization channels. These include roll channel control, pitch channel control and altitude channel control. Through these channels, the connected system can support angular stabilization, longitudinal balancing and barometric altitude hold functions. The exact functions available from the panel depend on the installed autopilot system, wiring and aircraft modification.
Cockpit installation of 6S2.390.126 Series 4
The panel is designed as an aircraft cockpit instrument panel unit. It may be installed on the central console, side console or other cockpit control area according to helicopter layout. The front panel includes operating controls and indication elements for crew use. Depending on modification, the panel may include red-white or green-compatible illumination for operation in day, night or NVG-related cockpit lighting environments.
Identification and ordering of 6S2.390.126 Series 4
The product may be referenced as 6S2.390.126 Series 4, 6С2.390.126 сер. 4, PU-126 or ПУ-126. For correct supply, it is useful to specify the aircraft type, installed flight control complex, required series, illumination version, connector configuration, condition, documentation requirements and whether the unit must be supplied with a passport, tag or test record.
Technical details
- Product Type
- Aircraft control panel / remote control panel
- Designation
- 6S2.390.126 Series 4
- Alternative Designations
- 6С2.390.126 сер. 4, PU-126, ПУ-126, control panel PU-126
- Function
- Mode selection, switching and generation of control signals for helicopter stabilization and semi-automatic control systems
- Purpose
- Cockpit control interface for flight control / autopilot equipment
All specificationsCollapse specifications
- Application / Where Used
- Helicopter flight control, stabilization and autopilot systems
- Associated Systems
- PKV-252, PKV-252-1, VUAP-1 where applicable by documentation
- Related Equipment
- 6S2.390.125 series control panel; BK-252 switching units; VDU-252 director control computers; feedback sensors
- Compatible Aircraft
- Mi-8 / Mi-17, Ka-226, Ka-32 and related Mi / Ka helicopters where applicable by documentation
- System / Installation Area
- Helicopter cockpit flight control / autopilot control area
- Installation Location
- Central console, side console or cockpit control panel according to aircraft documentation
- Controlled Channels
- Roll, pitch and altitude channels
- Roll Channel Function
- Stabilization and control of angular position
- Pitch Channel Function
- Longitudinal balancing / pitch control
- Altitude Channel Function
- Barometric altitude stabilization where applicable
- DC Power Supply
- 27 V DC ±10%
- AC Power Supply
- 36 V / 115 V AC, 400 Hz for illumination and related circuits where applicable by aircraft modification
- Current Consumption
- Not more than 1.5 A through DC circuit, according to supplied data
- Operating Mode
- Continuous
- Design
- Modular cockpit panel unit
- Panel Illumination
- Built-in red-white or green-compatible illumination depending on modification
- Controls
- Rotary knobs / trimmers for roll and pitch signal input; push-button switches for automatic hold modes
- Indication
- Channel status, autopilot readiness and trim-related indication where applicable
- Approximate Weight
- About 1.8–2.2 kg depending on series and mounting frame
- Technical Documentation
- Product passport, aircraft installation documentation, test documentation upon request
Payment & delivery
Orders ship from our hub in Dubai. Partner stock is first transferred to Dubai, then shipped to you.
Dubai stock: 100% before dispatch. Partner stock (Remote stock) and Pre-order: 50% advance payment to start the order and 50% before shipment from Dubai to you.
Availability, lead time, delivery cost and payment terms are confirmed for your order before payment.
Payment & delivery terms




