HB 8756-2023
Active
Standards
Current Category: CN-HB - Aviation
HB 8758-2023
Active
HB 8758-2023 HB 8758-2023 Civil Unmanned Modification General Requirements for Personnel Helicopters
HB 8760-2023
Active
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
Active
HB 9100-2023 Airline quality management system requirements
HB/Z 302-2023
Active
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.
HB 8678-2023
Active
HB 8678-2023 The method for determining the allowable values of composite laminate structure design for aircraft HB 8678-2023
This document specifies the design philosophy and determination method for the allowable values of composite laminates for aircraft. This document is applicable to the determination of allowable values for composite laminates in civil aircraft, and other types of aircraft can refer to it for use.
HB 8689-2023
Active
HB 8689-2023 Common Requirements for Inerting Systems for Civil Aircraft Fuel Tanks HB 8689-2023
This document specifies the design requirements and verification requirements for the inerting system of civil aircraft fuel tanks (hereinafter referred to as the inerting system). This document applies to the inerting system of fuel tanks of civil transport aircraft based on air separation membrane-type onboard nitrogen generation systems. Other types of fuel tank inerting systems can be used for reference.
HB 8704-2023
Active
HB 8704-2023 Testing method for electromagnetic interference path loss of portable electronic devices in civil aircraft
This document specifies the general requirements, test methods, test data processing, and analysis and evaluation of test results for electromagnetic interference path loss tests of portable electronic devices on civil aircraft. This document is applicable to electromagnetic interference path loss tests of portable electronic devices on normal/transport category aircraft (referred to as "aircraft" in this document).
HB 8762-2023
Active
HB 8762-2023 Aircraft Maintainability Design Guidelines
This document specifies the general and detailed requirements for the maintainability, cost-effectiveness, error-prevention, and human factors of civil aircraft maintenance. This document is applicable to the maintainability design of civil aircraft in the preliminary design and detailed design phases. Other aircraft maintainability designs can refer to and use it for reference.