attitude indicator
Price on request
attitude indicator
Out of stock
The AGB-98R is an autonomous gyroscopic attitude indicator designed to determine and display aircraft spatial position relative to the horizon using a “view from aircraft to ground” indication format within flight and navigation instrument systems.
The instrument provides indication of roll, pitch, and lateral slip angles, as well as deviations from localizer and glide path equal-signal zones and control commands generated by automatic control systems, ensuring comprehensive attitude and navigation reference.
The unit is used as part of aircraft flight and navigation systems and automatic control systems, providing pilots and onboard equipment with essential attitude and guidance information during various flight regimes.
The instrument is designed as an autonomous unit with a built-in gyroscope and mechanical correction system, including correction disconnect and monitoring functions, and incorporates protection against tumbling. The product is also known under alternative designations AGB-98R and 6Sh2.511.022.
Product Type: Autonomous gyroscopic attitude indicator
Function: Indication of roll, pitch, lateral slip, LOC/GS deviations; generation of control command signals
Application / Where Used: Flight and navigation instrument systems; automatic control systems
Display Type: View from aircraft to ground
Roll Range: ±360°
Pitch Range: ±85°
Power Supply (DC): 27 V DC
Power Supply (AC): Single-phase AC 36 V, 400 Hz
Additional AC Power Supply: Single-phase AC 6 V, 400 Hz
Gyroscope: Built-in
Correction System: Mechanical correction with integrated correction disconnect
Monitoring System: Built-in
Tumble Resistance: Pitch stop protection scheme
Illumination: Built-in white backlight
Weight: 1.8 kg
Standard Compliance: ENLGS compliant
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-98R is an autonomous gyroscopic attitude indicator designed to determine and display aircraft spatial position relative to the horizon using a “view from aircraft to ground” indication format within flight and navigation instrument systems.
The instrument provides indication of roll, pitch, and lateral slip angles, as well as deviations from localizer and glide path equal-signal zones and control commands generated by automatic control systems, ensuring comprehensive attitude and navigation reference.
The unit is used as part of aircraft flight and navigation systems and automatic control systems, providing pilots and onboard equipment with essential attitude and guidance information during various flight regimes.
The instrument is designed as an autonomous unit with a built-in gyroscope and mechanical correction system, including correction disconnect and monitoring functions, and incorporates protection against tumbling. The product is also known under alternative designations AGB-98R and 6Sh2.511.022.
Product Type: Autonomous gyroscopic attitude indicator
Function: Indication of roll, pitch, lateral slip, LOC/GS deviations; generation of control command signals
Application / Where Used: Flight and navigation instrument systems; automatic control systems
Display Type: View from aircraft to ground
Roll Range: ±360°
Pitch Range: ±85°
Power Supply (DC): 27 V DC
Power Supply (AC): Single-phase AC 36 V, 400 Hz
Additional AC Power Supply: Single-phase AC 6 V, 400 Hz
Gyroscope: Built-in
Correction System: Mechanical correction with integrated correction disconnect
Monitoring System: Built-in
Tumble Resistance: Pitch stop protection scheme
Illumination: Built-in white backlight
Weight: 1.8 kg
Standard Compliance: ENLGS compliant
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.