HB 8747-2023
Active
Standards
Current Category: CN-HB - Aviation
HB 8748-2023
Active
HB 8748-2023 Aerospace part selective melting lattice structure modeling process and requirements
HB 8751-2023
Active
HB 8751-2023 Aluminum coating specification for aircraft fasteners
HB 8752-2023
Active
HB 8752-2023 MoS2-based specification for fasteners used on aircraft
HB 8756-2023
Active
HB 8756-2023 HB 8756-2023 Aircraft self-locking nut general specification
HB 8758-2023
Active
HB 8758-2023 HB 8758-2023 Civil Unmanned Modification General Requirements for Personnel Helicopters
HB 8760-2023
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HB 8760-2023 HB 8760-2023 General Requirements for Vision-Inertial Flight-Time Navigation System for Civil Light Multi-Rotor Unmanned Aerial Vehicles
HB 9100-2023
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HB 9100-2023 Airline quality management system requirements
HB/Z 302-2023
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HB/Z 302-2023 HB/Z 302-2023 Guide for Design of Aircraft Power Supply System for Civil Aircraft
HB 5795-2023
Active
HB 5795-2023 aircraft wire current carrying capacity
This document specifies the calculation method and requirements for the load current of aviation wires. The data provided in this document is applicable to wires that comply with the GJB 773 standard. For other types of aviation copper core wires, the load current can be estimated according to their maximum allowable long-term operating temperature based on the data in this document.
HB 7086-2023
Active
HB 7086-2023 Airframe aerodynamic tolerances for civilian aircraft
This document specifies the aerodynamic edge tolerances of civil aircraft, mainly including: profile value, waviness, step difference, clearance, wing surface distortion, control surface fit, fastener flushness and other tolerance requirements. This document is applicable to civil aircraft, and other aircraft can refer to it for use.
HB 8677-2023
Active
HB 8677-2023 HB 8677-2023 Flight Load Calculation Method for Pressure Load of Integrated Tank of Aircraft
This document specifies the hydraulic pressure loads that should be considered for the overall fuel tanks of transport aircraft, as well as the calculation method for these hydraulic pressure loads. This document is applicable to the structural design and strength analysis of the overall fuel tanks of transport aircraft under the action of hydraulic pressure loads. Other types of aircraft may refer to this document for reference.