Code of China Chinese Classification Professional Classification ICS Classification Latest Value-added Services

Title Standard No. Implemented On
General technical requirements of propeller for aircraftHB 7809-20062007-5-1
General requirements of gas turbine assembly enclosureHB 7812-20062007-5-1
Oil consumption measurements for oil system of aircraft gas turbine engineHB 7810-20062007-5-1
General specification for detector ice of air intake duct aircraft engines and airframe systemsHB 7800-20062007-5-1
General requirements for gas turbine supercharging unitHB 7813-20062007-5-1
General requirements for inlet and exhaust system of gas turbine Turnkey installationHB 7811-20062007-5-1
Specification for flow regulator of Lox/Kerosene rocket engineQJ 3235-20052006-5-1
Testing and evaluation method for recrystallization on directionlly solidified bladesHB 7782-20052006-5-1
Ignition system aircraft turbine engine general specification forHB 7783-20052006-5-1
General specification for electro-pneumatic valve of liquid propellant rocket engineQJ 3264-20052006-5-1
Specification for precious metals of catalytic netty pipe for aeroengineHB 7781-20052006-5-1
General spacification for bladder tank of low-thrust liquid propulsion systemQJ 3265-20052006-5-1
General specification for surface tension tank of low-thrust liquid propulsion systemQJ 3203-20052005-7-1
Test method for hydraulics of liquid rocket engine pumpQJ 3202-20052005-7-1
General specification for aircraft engine gearboxHB 7719-20022003-2-1
Specification for the disks of FGH95 powder metallurgy superalloy for turbine shaft eddyingHB 7727-20022003-2-1
Requirements for oil systems aircraft installattion and testHB 7708-20022003-2-1
Low-Pressure Oil Strainer HB 920-20002001-1-1
High Pressure Oil FilterHB 919-20002001-1-1
Performance Test of Fuel Nozzle on Aero-EngineHB 7667-20002001-1-1
Inlet Filter for Lightweight Gas Turbine HB 7257-19951996-1-1
Basic Requirements for Product Standard Preparation of Lightweight Gas Turbine Complete Equipment HB 7258-19951996-1-1
Oil Nipple Head of Aircraft for GreaseHB 6661-19921993-5-1
Design Requirements for Start-up System of Aviation Turbine Engine HB 6630-19921992-12-1
Design Guideline for thes ynchro moter of Aero-engine fuel oil and control system HB/Z 201-19911991-12-1
Design Guideline for rotary-vane type fuel pump of aero-engine fuel oil and control system HB/Z 200-19911991-12-1
Design Guideline for layer plate limiter of aero-engine fuel oil and control system HB/Z 202-19911991-12-1
General technical specifications for airborne starting motor HB 6205-19891989-12-1
Terms of fuel and control systems of aero-engine HB 6367-19891989-12-1
Guideline for design of aero-engine fuel oil and control system plunger type fuel pump HB/Z 151-19891989-12-1
Guidline on design of circular section fixed value flow nipple for aero-engine fuel oil and control system HB/Z 153-19891989-12-1
Guideline for design of aero-engine fuel oil and control system nozzle - baffle hydraulic parts HB/Z 152-19891989-12-1
Guideline on the Design of Gear Type Fuel Pump of Engine Fuel Control SystemHB/Z 134-19881988-9-1
Guideline on the Design of Differential Pressure Valve of Engine Fuel Control SystemHB/Z 133-19881988-9-1
General Technical Specification of Air Turbine Starter for Aircraft EngineHB 5946-19861986-12-1
Oil Seal Equipment of Engine (Drawings Unprovided) HB 3650-19851986-3-1
Serial Number of Repeat Components and Elements for Aviation Turbine Engine HB 5860-19841985-1-1
Specifications for Professional Technology of Aero-engine Tachometer HB 5621-19801981-10-1
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