FIELD: aviation.
SUBSTANCE: invention relates to a system and method of control and monitoring of aircraft. An air tapping system of an aircraft comprising of at least one air tapping valve, configured to tap an air flow on the aircraft configured to tap an air flow on the aircraft, a first temperature information module, a second temperature information module, at least one management module and at least one data processing module, coupled to the management module.
EFFECT: invention claims to improve reliability of control and monitoring and data processing.
10 cl, 8 dwg
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