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attitude indicator
Price on request
attitude indicator
Partner Stock
The AGB-3K Series 2 is a gyroscopic aircraft attitude indicator designed to provide visual and electrical information on aircraft position relative to the true horizon within flight and navigation instrument systems.
The instrument provides stabilized indication of roll and pitch angles and generates proportional electrical output signals for transmission to onboard systems, ensuring reliable attitude reference during various flight conditions.
The unit is installed on helicopters and fixed-wing aircraft, including Mi-8, Mi-17, Yak-40, An-24, An-26, An-30, and Il-76, as part of standard flight instrument systems supporting pilot orientation and system integration.
The instrument operates on a gyroscopic assembly with a correction system and includes a power failure indication function providing visual warning in case of electrical supply disruption. The product is also known under alternative designations AGB-3K Series 2, AGB-3K, and AGB-3K Series 3.
Product Type: Gyroscopic attitude indicator
Function: Visual indication of roll and pitch angles; generation of proportional electrical output signals
Application / Where Used: Aircraft flight and navigation instrument systems
System / Installation Area: Flight instrument panel and onboard avionics systems
Interchangeability / Replaceability: Interchangeable with AGB-3K and AGB-3K Series 3
Compatible Aircraft / Equipment: Mi-8, Mi-17, Yak-40, An-24, An-26, An-30, Il-76
Roll Range: ±360°
Pitch Range: ±80°
Warm-Up Time: ≤ 1.5 min
AC Power Supply: 36 V, 400 Hz
AC Current Consumption: Phase III — ≤ 0.8–0.9 A
DC Power Supply: 27 V
DC Current Consumption: ≤ 0.3 A
Indication Error (0–30°): ≤ ±1°
Gyroscope Precession Rate: 1.8–5 °/min
Gyroscope Drift without Correction (5 min): Roll ≤ ±2.5°; Pitch ≤ ±4°
Power Failure Indication: Warning flag for DC circuit failure and single AC phase loss
Weight: ≤ 4.7 kg
Technical Documentation: Technical documentation available upon request
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 AGB-3K Series 2 is a gyroscopic aircraft attitude indicator designed to provide visual and electrical information on aircraft position relative to the true horizon within flight and navigation instrument systems.
The instrument provides stabilized indication of roll and pitch angles and generates proportional electrical output signals for transmission to onboard systems, ensuring reliable attitude reference during various flight conditions.
The unit is installed on helicopters and fixed-wing aircraft, including Mi-8, Mi-17, Yak-40, An-24, An-26, An-30, and Il-76, as part of standard flight instrument systems supporting pilot orientation and system integration.
The instrument operates on a gyroscopic assembly with a correction system and includes a power failure indication function providing visual warning in case of electrical supply disruption. The product is also known under alternative designations AGB-3K Series 2, AGB-3K, and AGB-3K Series 3.
Product Type: Gyroscopic attitude indicator
Function: Visual indication of roll and pitch angles; generation of proportional electrical output signals
Application / Where Used: Aircraft flight and navigation instrument systems
System / Installation Area: Flight instrument panel and onboard avionics systems
Interchangeability / Replaceability: Interchangeable with AGB-3K and AGB-3K Series 3
Compatible Aircraft / Equipment: Mi-8, Mi-17, Yak-40, An-24, An-26, An-30, Il-76
Roll Range: ±360°
Pitch Range: ±80°
Warm-Up Time: ≤ 1.5 min
AC Power Supply: 36 V, 400 Hz
AC Current Consumption: Phase III — ≤ 0.8–0.9 A
DC Power Supply: 27 V
DC Current Consumption: ≤ 0.3 A
Indication Error (0–30°): ≤ ±1°
Gyroscope Precession Rate: 1.8–5 °/min
Gyroscope Drift without Correction (5 min): Roll ≤ ±2.5°; Pitch ≤ ±4°
Power Failure Indication: Warning flag for DC circuit failure and single AC phase loss
Weight: ≤ 4.7 kg
Technical Documentation: Technical documentation available upon request
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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