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altitude corrector
Price on request
altitude corrector
Available on back-order
The KV-11 is an aircraft altitude corrector designed as part of the AP-34B automatic flight control system, providing altitude-dependent correction signals for vertical stabilization.
The unit converts barometric altitude changes into proportional electrical signals used to stabilize vertical flight, maintain commanded altitude, and reduce pilot workload during various flight modes.
The corrector is used on Mi-8 / Mi-17 helicopter series, including Mi-8T, Mi-8MT, Mi-8AMT, Mi-8MTV-1 and related variants, within autopilot-controlled flight systems.
The unit operates within the AP-34B autopilot system as part of the vertical stabilization channel, interacting with onboard amplifiers and executive control elements. The product is also known under designations KV11, KV-11, KB-11.
Product Type: Altitude corrector
Function: Generation of altitude-dependent correction signals for vertical stabilization
Application / Where Used: Automatic flight control systems
System / Installation Area: AP-34B autopilot system, vertical channel
DC Power Supply: 27 ± 2.7 V
AC Power Supply: 36 ± 2 V, 400 ± 8 Hz (three-phase)
AC Current Consumption: ≤ 0.3 A per phase
DC Current Consumption: ≤ 0.1 A
Operating Altitude Range: 0 to 20,000 m
Maximum Tracking Rate: Equivalent to ~200 m/s
Potentiometer Stroke Range: 160–320 m span at 20,000 m
Potentiometer Accuracy Limits:
– At 1 km: ≤ 20 m
– At 12 km: ≤ 8 m
– At 20 km: ≤ 3 m
Mounting: Installed within autopilot equipment bay
Category: Aviation Technical Equipment (ATE)
Technical Documentation: Manufacturer passport and operation manual
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 KV-11 is an aircraft altitude corrector designed as part of the AP-34B automatic flight control system, providing altitude-dependent correction signals for vertical stabilization.
The unit converts barometric altitude changes into proportional electrical signals used to stabilize vertical flight, maintain commanded altitude, and reduce pilot workload during various flight modes.
The corrector is used on Mi-8 / Mi-17 helicopter series, including Mi-8T, Mi-8MT, Mi-8AMT, Mi-8MTV-1 and related variants, within autopilot-controlled flight systems.
The unit operates within the AP-34B autopilot system as part of the vertical stabilization channel, interacting with onboard amplifiers and executive control elements. The product is also known under designations KV11, KV-11, KB-11.
Product Type: Altitude corrector
Function: Generation of altitude-dependent correction signals for vertical stabilization
Application / Where Used: Automatic flight control systems
System / Installation Area: AP-34B autopilot system, vertical channel
DC Power Supply: 27 ± 2.7 V
AC Power Supply: 36 ± 2 V, 400 ± 8 Hz (three-phase)
AC Current Consumption: ≤ 0.3 A per phase
DC Current Consumption: ≤ 0.1 A
Operating Altitude Range: 0 to 20,000 m
Maximum Tracking Rate: Equivalent to ~200 m/s
Potentiometer Stroke Range: 160–320 m span at 20,000 m
Potentiometer Accuracy Limits:
– At 1 km: ≤ 20 m
– At 12 km: ≤ 8 m
– At 20 km: ≤ 3 m
Mounting: Installed within autopilot equipment bay
Category: Aviation Technical Equipment (ATE)
Technical Documentation: Manufacturer passport and operation manual
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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