V36 总体技术要求 标准查询与下载

GJB 67.3A-2008 军用飞机结构强度规范 第3部分：其他载荷

本部分规定了军用飞机的其他载荷及其作用下的结构强度和刚度要求。 本部分适用于各类军用飞机（不含直升机）的订货、设计和验证。本部分也是签订合同的依据之一，对于具体型号应按合同条款执行。

Military airplane structural strength specification.Part 3: Miscellaneous loads

GJB 67.7A-2008 军用飞机结构强度规范 第7部分：气动弹性

本部分规定了在飞机设计和制造过程中，防止颤振、发散及其他气动弹性不稳定的要求和所需进行的分析、地面试验和飞行试验。本部分提供的分析及试验要求，用以确认和建立一些作为结构设计最低标准的准则和参数，飞机机体应能满足这些要求。 本部分适用于各类军用飞机（不含直升机）的订货、设计和验证。本部分也是签订合同的依据之一，对于具体型号应按合同条款执行。

Military airplane structural strength specigcation.Part 7: Aeroelasticity

GJB 67.8A-2008 军用飞机结构强度规范 第8部分：振动和航空声耐久性

本部分规定了军用飞机设计和制造中振动和航空声耐久性的一般和详细设计要求与准则： a）控制结构振动； b）防止在飞机使用寿命期内由于振动、航空声和其他动载荷引起的机体结构或结构部件的疲劳破坏； 保证空勤人员工效性和乘员舒适性的要求； d）规定为验证符合设计要求所需的振动和航空声分析、实验室试验、地面试验、飞行试验和结构动力学设计的工程要求。 本部分适用于各类军用飞机（不含直升机）的订货、设计和验证，也是签订合同的依据之一。对于具体型号应按合同条款执行。

Military airplane structural strength specification.Part 8: Vibration and aeroacoustic durability

GJB 67.10A-2008 军用飞机结构强度规范 第10部分：飞行试验

本部分规定了军用飞机载荷验证、结构强度验证、动响应验证和载荷/环境谱实测的飞行试验要求。 本部分适用于各类军用飞机（不含直升机）的订货、设计和验证。本部分也是签订合同的依据之一，对于具体型号应按合同条款执行。

Military airplane structural strength specification.Part 10: Flight tests

GJB 67.11A-2008 军用飞机结构强度规范 第11部分：结构生存力

本部分规定了飞机结构生存力的设计和验证要求。 本部分适用于各类军用飞机（不含直升机）的设计、验证和订货。本部分也是签订合同的依据之一，对于具体型号应按合同条款执行。

Military airplane structural strength specincation.Part 11: Structure Survivability

GJB 67.12A-2008 军用飞机结构强度规范 第12部分：文件和报告

本部分规定了用以证明所研制的飞机满足GJB 67.lA-2008～GJB 67.11A-2008及GJB 67.14-2008的资料要求。 本部分适用于各类军用飞机（不含直升机）的订货、设计和验证。本部分也是签订合同的依据之一，对于具体型号应按合同条款执行。

Military airplane structural strength sepcification.Part 12: Documents and reports

GJB 67.2A-2008 军用飞机结构强度规范 第2部分：飞行载荷

本部分规定了军用飞机在飞行受载情况下的结构强度和刚度的要求。 本部分适用于各类军用飞机（不含直升机）的订货、设计和验证。本部分也是签订合同的依据之一，对于具体型号应按合同条款执行。

Military airplane structural strength specification.Part 2:Flight loads

GJB 67.4A-2008 军用飞机结构强度规范 第4部分：地面载荷

本部分规定了军用飞机在起飞、弹射、着陆、（舰）、拦阻、滑行、地面操作和维护等情况下的载荷及其作用下的结构强度和刚度要求。 本部分适用于各类军用飞机（不含直升机）的订货、设计和验证。本部分也是签订合同的依据之一，对具体型号应按合同条款执行。

Military airplane structural strength specification .Part 4:Ground loads

GJB 67.5A-2008 军用飞机结构强度规范 第5部分：水上飞机的水载荷

本部分规定了水上飞机的水载荷及其作用下的结构强度和刚度要求。 本部分适用于各类军用水上飞机（不含直升机）的订货、设计和验证。本部分也是签订合同的依据之一，对于具体型号应按合同条款执行。

Military airplane structural strength specifiction.Part 5:Water loads for seaplanes

GJB 67.6A-2008 军用飞机结构强度规范 第6部分：重复载荷、耐久性和损伤容限

本部分规定了军用飞机结构的耐久性、损伤容限设计和验证要求以及作用于飞机上的重复载荷。 本部分适用于各类军用飞机（不含直升机）的订货、设计和验证。本部分也是签订合同的依据之一，对于具体型号应按合同条款执行。

Military airplane structural strength specification.Part 6:Repeated loads,dusrability and damage tolerance

SAE ARP4737H-2008 航空器除冰/防结冰方法

1.1 Field of Application1.1.1 This document establishes the minimum requirements for ground based aircraft deicing/anti-icing Methods andprocedures to ensure the safe operation of aircraft during icing conditions. This document does not specifyrequirements for particular airplane models.NOTE: Particular airline or aircraft manufacturers’ published manuals, procedures, or methods supplement theinformation contained in this document.1.1.2 Agreements and ContractsThis information is recommended as a basis for maintenance operations and service support agreements.1.1.3 Safety - Hazardous MaterialsWhile the materials, methods, applications, and processes described or referenced in this specification may involve theuse of hazardous materials, this specification does not address the hazards which may be involved in such use. It is thesole responsibility of the user to ensure familiarity with the safe and proper use of any hazardous materials and processesand to take necessary precautionary measures to ensure the health and safety of all personnel involved.1.1.4 All guidelines referred to herein are applicable only in conjunction with the referenced SAE specifications. Specificrequirements for airplane model type are not included. Due to aerodynamic and other concerns application ofdeicing/anti-icing fluids shall be carried out in compliance with engine and aircraft manufacturers’ requirements.

Aircraft Deicing/Anti-Icing Methods

HJB 411-2008 海军飞机结构腐蚀防护与控制通用设计要求

本标准规定了海军飞机结构腐蚀防护与控制通用设计要求。 本标准适用于海军飞机结构腐蚀防护与控制设计，包括生产制造和使用维护，其他类型飞机也可参照使用。

General design requirements of corrosion prevention and control for naval aircraft structures

HJB 412-2008 海军飞机结构防腐蚀密封通用设计要求

本标准规定了海军飞机结构防腐蚀密封通用设计要求。 本标准适用于海军飞机结构设计、生产制造与使用维护中的防腐蚀密封，其他类型飞机也可参照使用。

General design requirements of anticorrosion sealing for naval aircraft structures

ASTM F2585-08 液压气动无人航行器系统(UAS)发射系统设计和性能用标准规范

1.1 This specification covers the design and performance of unmanned aircraft system (UAS) launch system operating via a closed-loop pressurized hydraulic or pneumatic system with a hydraulic recovery, or both. 1.2 In instances where the launcher and UAS manufacturer are the same entity, compliance with this specification is the responsibility of the UAS manufacturer where applicable. 1.3 This standard does not purport to address all of the safety concerns associated with the USA launch system and its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.

Standard Specification for Design and Performance of Pneumatic-Hydraulic Unmanned Aircraft System (UAS) Launch System

ASTM F2636-08 用于自主/准自主远程控制单引擎无人机着陆的商业用无人机系统(UAS)飞行实践测试标准的标准实施规程

Unmanned aircraft present unique challenges for applicants and examiners. Unlike manned aircraft, in which, regardless of the size and complexity of the aircraft, there are still basic similarities in concepts and operations, unmanned aircraft are varied in both flight capability and pilot interaction. Many aspects of unmanned aircraft operations are automated, and the pilots may not have the same information available to them (that is, pitch and bank) that pilots flying manned aircraft have available to them. This will create a situation in which some unmanned aircraft systems (UAS) will not be capable of meeting all the requirements of this practice or will not require the same skill sets that manned aircraft require. The examiner will have to decide which tasks the applicant''s UAS will be capable of completing and test those tasks. As required, the examiner will note any limitations as a result of the UAS being incapable of performing a task on the applicant''s certificate per 14 CFR 61.45(b)(2). If the applicant desires to have a certificate with no restrictions or limitations, he/she will need to use a UAS that is capable of completing all the tasks in this practice. Information considered directive in nature is described in this practice by the use of “shall” and “must” indicating the actions are mandatory. Guidance information is described in terms such as “should” and “may” indicating the actions are desirable or permissive but not mandatory. A list of acronyms is in Section 3. This practice includes the areas of operation and tasks that will demonstrate the pilot''s ability to fly the unmanned aircraft safely and proficiently.1.1 This practice defines the knowledge, skills, and abilities required of unmanned aircraft pilots to be able to fly unmanned aircraft—single-engine land (SEL) in the national airspace system safely and for hire. 1.2 The commercial unmanned aircraft systems (UAS) pilot practical test standards (PTS)-unmanned aircraft include the areas of operation and tasks that will demonstrate the pilot''s ability to fly the unmanned aircraft safely and proficiently. 1.3 This practice does not apply to pilots who will fly mini/small unmanned aerial vehicles (UAVs) for hire within visual range of the pilot, mini/small UAVs being those UAVs listed as lightly regulated. 1.4 This practice provides a PTS intended to meet the Civil Aviation Authority’s (CAA) requirements for issuing commercial UAS pilot authorizations. 1.5 The values given in inch-pound units are to be regarded as the standard. The values in parentheses are for information only. 1.6 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.

Standard Practice for Commercial Unmanned Aircraft System (UAS) Pilot Practical Test Standards for Unmanned Aircraft Single-Engine Land (SEL) Remote Control and Autonomous/Semiautonomous

KS W ISO 8267-2:2007 航空器.牵引杆附属接头的接口要求.第2部分:地方飞行器

이 규격은 상업용 민간 여객기 또는 화물기에서 일반적인 삼륜형 착륙장치의 앞 착륙장치(앞

Aircraft－Tow bar attachment fittings interface requirements－Part 2：Regional aircraft

KS W ISO 8267-1:2007 航空器.牵引杆附属接头的接口要求.第1部分:干线飞行器

이 규격은 사업용(상업용) 민간 여객기 또는 화물기에서 일반적인 삼륜형 착륙장치의 앞 착륙

Aircraft－Tow bar attachment fittings interface requirements－Aircraft－Tow bar attachment fittings interface requirements－

GJB 5964-2007 军用直升机导弹发射装置通用规范

本规范规定了军用直升机导弹发射装置（以下简称“导弹发射装置”）的通用要求。 本规范适用于军用直升机空空、空地（舰）导弹发射装置。

General specification for missile launcher of military helicopter

GJB 5965-2007 军用直升机吊挂系统通用规范

本规范规定了军用直升机吊挂系统（以下简称吊挂系统）的通用技术要求。 本规范适用于军用直升机吊挂系统。

General specincation for suspension system of military helicopter

GJB 19B-2007 歼（强）击机座椅几何尺寸

本标准规定了歼（强）击机座椅几何尺寸。 本标准适用于歼击机、强击机、歼击轰炸机及上述飞机的教练机。

Aircrew seat geometry for fighter and attacker