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Gyro Unit
Price on request
Gyro Unit
Available on back-order
The GA-6 is the central gyro unit used in GMK-1 aircraft heading systems, including GMK-1A and GMK-1AE versions. It works as the main heading reference element of the system and keeps course information stable while the aircraft is moving, turning or briefly yawing. In the GMK-1 set, the GA-6 is not used alone. It operates together with the ID-3 induction detector, correction mechanism, control panels and course indicators. Its output is then used by cockpit instruments, autopilot channels and other navigation equipment that require continuous heading information.
The main value of the GA-6 is its ability to smooth out short-term aircraft heading fluctuations. The gyro inside the unit keeps a stable reference direction, so momentary yawing, vibration or small heading disturbances do not immediately disturb the transmitted course signal. This is especially important for aircraft and helicopters where a magnetic heading signal alone may be too unstable for direct use. The GA-6 helps the system produce a usable heading reference for indication and control, while correction signals from the magnetic channel keep long-term drift within the required limits.
The GA-6 supports the main operating modes of the GMK-1 heading system. In magnetic heading mode, the gyro unit is corrected through the magnetic channel, where the ID-3 induction detector and correction mechanism compensate the natural drift of the gyro. In gyro heading mode, magnetic correction is disconnected and the aircraft heading is maintained by the gyro reference itself. This mode is used when magnetic information is unreliable or unsuitable, for example in high latitudes, during certain maneuvers or when the crew needs the system to work as a directional gyro.
Heading information from the GA-6 is taken from the built-in synchro transmitter and sent to aircraft consumers. These may include UGR-4UK course indicators, pilot navigation instruments, autopilot equipment and radio navigation systems, depending on aircraft configuration. On Mi-8 helicopters, heading data may also be used by autopilot systems such as AP-34B for course stabilization and control functions. Because several systems may depend on the same heading reference, the condition of the GA-6 affects not only the course indicator, but also connected navigation and control channels.
The GA-6 contains a three-degree-of-freedom astatic gyroscope with a horizontal rotor axis. The assembly is placed in a sealed, vibration-resistant metal housing suitable for installation in aircraft equipment compartments. Course signals are transmitted electrically through the built-in synchro elements. The unit must reach operating speed before the heading system is ready for normal use, so warm-up and readiness time are part of the system check. Mechanical condition, gyro run-up, power supply quality and correct signal transmission all matter when assessing serviceability.
The GA-6 was used on a wide range of Soviet and Russian aircraft fitted with GMK-1 heading systems. Typical applications include Mi-8, Mi-8T, Mi-8MTV, Mi-171, Mi-26, Ka-27, Ka-32, An-24, An-26, An-30, Yak-40, L-410 and other aircraft depending on avionics configuration. The unit belongs to a complete heading system, so replacement should always be checked against the aircraft parts catalog, the installed GMK-1 modification and wiring documentation. Similar gyro units from related systems should not be treated as interchangeable without technical confirmation.
When ordering the GA-6, it is useful to specify the drawing number, system version, required condition and documentation status. The unit may be requested for repair, replacement, restoration of a GMK-1 set or stock replenishment. During maintenance, technicians normally check power supply, warm-up time, course transmission, drift behavior, connector condition and agreement with cockpit indicators. Since the GA-6 is a precision gyro unit, external appearance is not enough to judge it. Storage history, test results, passport data and remaining serviceability are important for aircraft use.
Product Type: Aircraft gyro unit / heading gyro assembly
Designation: GA-6
Drawing Number: 6D2.562.010
Associated System: GMK-1 aircraft heading system
Applicable System Versions: GMK-1A, GMK-1AE and related GMK-1 versions depending on aircraft installation
Function: Measurement, stabilization, storage and transmission of aircraft heading information
Application / Where Used: Aircraft heading reference, navigation and autopilot systems
System / Installation Area: GMK-1 heading system equipment group; aircraft avionics or instrument equipment compartment
Main System Role: Central gyro reference unit of the heading system
Associated Components: ID-3 induction detector, KM-8 correction mechanism, BS-1 communication unit, AS-1 matching unit, PU-26 / PU-27 control panels, UGR-4UK indicator
Output Consumers: Course indicators, pilot navigation instruments, autopilot systems, radio navigation equipment and other heading-data users
Supported Modes: Magnetic heading mode and gyro heading / directional gyro mode
Gyroscope Type: Three-degree-of-freedom astatic gyroscope with horizontal rotor axis
Azimuth Drift: Not more than ±2.5° per hour in free gyro / gyro heading mode
Remote Transmission Error: Not more than ±0.6°
Readiness / Run-Up Time: Up to 5 minutes
DC Power Supply: 27 V DC ±10%
AC Power Supply: 36 V AC ±10%, 400 Hz
Signal Transmission: Built-in synchro transmitter
Typical Autopilot Application: AP-34B on Mi-8 helicopters, depending on configuration
Compatible Aircraft / Equipment: Mi-8, Mi-8T, Mi-8MTV, Mi-171, Mi-26, Ka-27, Ka-32, An-24, An-26, An-30, Yak-40, L-410 and other aircraft fitted with GMK-1 systems
Housing: Sealed vibration-protected metal housing with flange mounting
Technical Documentation: GMK-1 system documentation, aircraft maintenance manual, wiring diagrams, product passport / label when available
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.
The GA-6 is the central gyro unit used in GMK-1 aircraft heading systems, including GMK-1A and GMK-1AE versions. It works as the main heading reference element of the system and keeps course information stable while the aircraft is moving, turning or briefly yawing. In the GMK-1 set, the GA-6 is not used alone. It operates together with the ID-3 induction detector, correction mechanism, control panels and course indicators. Its output is then used by cockpit instruments, autopilot channels and other navigation equipment that require continuous heading information.
The main value of the GA-6 is its ability to smooth out short-term aircraft heading fluctuations. The gyro inside the unit keeps a stable reference direction, so momentary yawing, vibration or small heading disturbances do not immediately disturb the transmitted course signal. This is especially important for aircraft and helicopters where a magnetic heading signal alone may be too unstable for direct use. The GA-6 helps the system produce a usable heading reference for indication and control, while correction signals from the magnetic channel keep long-term drift within the required limits.
The GA-6 supports the main operating modes of the GMK-1 heading system. In magnetic heading mode, the gyro unit is corrected through the magnetic channel, where the ID-3 induction detector and correction mechanism compensate the natural drift of the gyro. In gyro heading mode, magnetic correction is disconnected and the aircraft heading is maintained by the gyro reference itself. This mode is used when magnetic information is unreliable or unsuitable, for example in high latitudes, during certain maneuvers or when the crew needs the system to work as a directional gyro.
Heading information from the GA-6 is taken from the built-in synchro transmitter and sent to aircraft consumers. These may include UGR-4UK course indicators, pilot navigation instruments, autopilot equipment and radio navigation systems, depending on aircraft configuration. On Mi-8 helicopters, heading data may also be used by autopilot systems such as AP-34B for course stabilization and control functions. Because several systems may depend on the same heading reference, the condition of the GA-6 affects not only the course indicator, but also connected navigation and control channels.
The GA-6 contains a three-degree-of-freedom astatic gyroscope with a horizontal rotor axis. The assembly is placed in a sealed, vibration-resistant metal housing suitable for installation in aircraft equipment compartments. Course signals are transmitted electrically through the built-in synchro elements. The unit must reach operating speed before the heading system is ready for normal use, so warm-up and readiness time are part of the system check. Mechanical condition, gyro run-up, power supply quality and correct signal transmission all matter when assessing serviceability.
The GA-6 was used on a wide range of Soviet and Russian aircraft fitted with GMK-1 heading systems. Typical applications include Mi-8, Mi-8T, Mi-8MTV, Mi-171, Mi-26, Ka-27, Ka-32, An-24, An-26, An-30, Yak-40, L-410 and other aircraft depending on avionics configuration. The unit belongs to a complete heading system, so replacement should always be checked against the aircraft parts catalog, the installed GMK-1 modification and wiring documentation. Similar gyro units from related systems should not be treated as interchangeable without technical confirmation.
When ordering the GA-6, it is useful to specify the drawing number, system version, required condition and documentation status. The unit may be requested for repair, replacement, restoration of a GMK-1 set or stock replenishment. During maintenance, technicians normally check power supply, warm-up time, course transmission, drift behavior, connector condition and agreement with cockpit indicators. Since the GA-6 is a precision gyro unit, external appearance is not enough to judge it. Storage history, test results, passport data and remaining serviceability are important for aircraft use.
Product Type: Aircraft gyro unit / heading gyro assembly
Designation: GA-6
Drawing Number: 6D2.562.010
Associated System: GMK-1 aircraft heading system
Applicable System Versions: GMK-1A, GMK-1AE and related GMK-1 versions depending on aircraft installation
Function: Measurement, stabilization, storage and transmission of aircraft heading information
Application / Where Used: Aircraft heading reference, navigation and autopilot systems
System / Installation Area: GMK-1 heading system equipment group; aircraft avionics or instrument equipment compartment
Main System Role: Central gyro reference unit of the heading system
Associated Components: ID-3 induction detector, KM-8 correction mechanism, BS-1 communication unit, AS-1 matching unit, PU-26 / PU-27 control panels, UGR-4UK indicator
Output Consumers: Course indicators, pilot navigation instruments, autopilot systems, radio navigation equipment and other heading-data users
Supported Modes: Magnetic heading mode and gyro heading / directional gyro mode
Gyroscope Type: Three-degree-of-freedom astatic gyroscope with horizontal rotor axis
Azimuth Drift: Not more than ±2.5° per hour in free gyro / gyro heading mode
Remote Transmission Error: Not more than ±0.6°
Readiness / Run-Up Time: Up to 5 minutes
DC Power Supply: 27 V DC ±10%
AC Power Supply: 36 V AC ±10%, 400 Hz
Signal Transmission: Built-in synchro transmitter
Typical Autopilot Application: AP-34B on Mi-8 helicopters, depending on configuration
Compatible Aircraft / Equipment: Mi-8, Mi-8T, Mi-8MTV, Mi-171, Mi-26, Ka-27, Ka-32, An-24, An-26, An-30, Yak-40, L-410 and other aircraft fitted with GMK-1 systems
Housing: Sealed vibration-protected metal housing with flange mounting
Technical Documentation: GMK-1 system documentation, aircraft maintenance manual, wiring diagrams, product passport / label when available
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.
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