attitude indicator
Price on request
attitude indicator
Available on back-order
AGR-29 attitude indicator is a gyroscopic flight instrument designed to indicate the aircraft spatial position in roll and pitch, lateral slip indication, display of roll and pitch control commands, and generation of roll and pitch electrical output signals.
The instrument belongs to gyroscopic flight and navigation equipment and is used as part of aircraft instrument systems. AGR-29 provides roll indication within ±360° and pitch indication according to the climb mode limits defined by the instrument design.
AGR-29 is based on a gyroscopic assembly with correction and indication systems. The instrument ensures specified accuracy under various operating conditions, including operation on rocking and vibrating bases, as well as after aircraft maneuvers with specified angular velocities. The design allows mechanical adjustment of the pitch scale via a rack control mechanism.
The attitude indicator is powered by a 27 V DC power supply and includes a separate lighting circuit. The instrument is designed for operation over a wide ambient temperature range.
Purpose: Indication of roll, pitch, lateral slip, roll and pitch control commands, and generation of roll and pitch output signals
Systems: Flight and navigation instrument systems
Product Type: Gyroscopic attitude indicator
Power Supply: 27 V DC
Current Consumption from 27 V DC: 1.2 A
Lighting Circuit Current Consumption: 1 A
Warm-Up Time at standard conditions and +55 °C: 2 min
Warm-Up Time at −30 °C: 5 min
Precession Rate at standard conditions and bank angles below 8°: 1–5 °/min
Precession Rate at −30 °C and +70 °C with bank angles below 8°: 0.8–6 °/min
Precession Rate at temperatures from −30 °C to +70 °C with bank angles above 8°: 0–2.5 °/min
Roll Range: ±360°
Pitch Range: During climb (90 − α) ±5°
Indication Error on rocking base (5 min and steady flight): Not more than ±1.5°
Indication Error on vibrating base: Not more than ±2.5°
Indication Error after turn at angular rates ωx=(240±4.8)°/s and ωz=(18±2)°/s: Not more than ±5°
Pitch Scale Travel via rack control: Not less than ±10°
Overall Dimensions: 105 × 105 × 250 mm
Weight: Not more than 3.1 kg
Condition: As applicable
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.
AGR-29 attitude indicator is a gyroscopic flight instrument designed to indicate the aircraft spatial position in roll and pitch, lateral slip indication, display of roll and pitch control commands, and generation of roll and pitch electrical output signals.
The instrument belongs to gyroscopic flight and navigation equipment and is used as part of aircraft instrument systems. AGR-29 provides roll indication within ±360° and pitch indication according to the climb mode limits defined by the instrument design.
AGR-29 is based on a gyroscopic assembly with correction and indication systems. The instrument ensures specified accuracy under various operating conditions, including operation on rocking and vibrating bases, as well as after aircraft maneuvers with specified angular velocities. The design allows mechanical adjustment of the pitch scale via a rack control mechanism.
The attitude indicator is powered by a 27 V DC power supply and includes a separate lighting circuit. The instrument is designed for operation over a wide ambient temperature range.
Purpose: Indication of roll, pitch, lateral slip, roll and pitch control commands, and generation of roll and pitch output signals
Systems: Flight and navigation instrument systems
Product Type: Gyroscopic attitude indicator
Power Supply: 27 V DC
Current Consumption from 27 V DC: 1.2 A
Lighting Circuit Current Consumption: 1 A
Warm-Up Time at standard conditions and +55 °C: 2 min
Warm-Up Time at −30 °C: 5 min
Precession Rate at standard conditions and bank angles below 8°: 1–5 °/min
Precession Rate at −30 °C and +70 °C with bank angles below 8°: 0.8–6 °/min
Precession Rate at temperatures from −30 °C to +70 °C with bank angles above 8°: 0–2.5 °/min
Roll Range: ±360°
Pitch Range: During climb (90 − α) ±5°
Indication Error on rocking base (5 min and steady flight): Not more than ±1.5°
Indication Error on vibrating base: Not more than ±2.5°
Indication Error after turn at angular rates ωx=(240±4.8)°/s and ωz=(18±2)°/s: Not more than ±5°
Pitch Scale Travel via rack control: Not less than ±10°
Overall Dimensions: 105 × 105 × 250 mm
Weight: Not more than 3.1 kg
Condition: As applicable
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.