共找到 185 条与 航空器维护与管理 相关的标准,共 13 页
This document contains the minimum requirements for supplier inspection and test quality system. It is emphasized that the quality system requirements specified in this standard are complementary (not alternative) to the contractual and applicable law and regulatory requirements.
Inspection and Test Quality System
本标准规定了飞机除冰/防冰液(ISO I型)的技术要求、试验方法、质量检验规定、包装、标志、运输、储存和使用。 本标准适用于清除和防止停泊飞机表面的冰、雪或霜的牛顿流体。
Deicing/anti-icing fluid for aircraft(ISO Type I)
This specification covers 14 ounce capacity grease cartridges. They are designed for use with cartridge-type grease guns conforming to MIL-G-3859.
Cartridges, Grease, 14 Ounce (for Cartridge-Type Grease Gun) FSC 4930; Should Be Used Instead of MIL-C-22587B, Which Was Cancelled on 30 August 1999
This specification establishes the requirements for a liquid cleaning compound intended for use in steam cleaning machines to clean metallic and painted, soiled surface.
Cleaning Compound, High Pressure Cleaner, Liquid FSC 6850; Should Be Used Instead of MIL-C-22542B(AS), Which Was Cancelled on 21 September 1998
Training syllabus for civil aircraft maintenance personnel
This specification covers the requirements for two types of anti-icing and deicing-defrosting fluids for use on aircraft.
Anti-Icing and Deicing-Defrosting Fluids FSC 6850
SHELTER, COMPLEXING KIT FOR
SHELTER, COMPLEXING KIT FOR
MIL-S-29413B, dated 20 January 1988, is inactive for new design and is no longer used, except for replacement purposes.
SHELTER, JOINING CORRIDOR FOR
PRINCIPLES OF INSPECT, REPAIR ONLY AS NECESSARY (IROAN) PROCEDURES AND PREPARATION OF IROAN PUBLICATIONS
PRINCIPLES OF INSPECT, REPAIR ONLY AS NECESSARY (IROAN) PROCEDURES AND PREPARATION OF IROAN PUBLICATIONS
Notification of Foreign/Regional Maintenance License Issuance
Aircraft Systems Manufacturer磗 Requirements for a Solution
Aircraft Systems Manufacturer磗 Requirements for a Solution
本标准规定了空空导弹维修性设计准则的一般要求和详细要求。 本标准适用于空空导弹(以下简称导弹)的维修性设计,是制定型号维修性设计准则的主要依据。具体型号维修性设计准则可根据需要对本标准进行适当剪裁。
Air-to-Air Missile Maintainability Design Criteria
Time Control Management for Civil Aircraft
This International Standard specifies the interface requirements for tow bar attachment fittings on the nose gear (when towing operations are normally done from the nose gear) in conventional tricycle type landing gears of civil transport aircraft as defined by FAR Part 25 or equivalent national airworthiness regulations. It covers tow bar attachment fittings for aircraft with a maximum ramp mass greater than 50 000 kg (110 000 Ib). This International Standard does not cover tow bar attachment fittings for aircraft with a ramp mass between 13 600 kg and 50 000 kg.
Specification for interface requirements for aircraft noseleg to towbar attachment fittings - Transport aircraft with a maximum ramp mass over 50000 kg (110000 lb)
This specification covers the technical content requirements for the preparation of technical manuals in work package concept for the maintenance of aircraft and related systems.
MANUALS, TECHNICAL: AIRCRAFT MAINTENANCE INSTRUCTIONS, TECHNICAL CONTENT REQUIREMENTS (WORK PACKAGE CONCEPT)
This specification prescribes the technical content requirements for preparation of technical manuals for repair, corrosion control, and nondestructive inspection of aircraft structure and structural components at organizational, intermediate, and depot maintenance levels.
MANUALS, TECHNICAL: AIRCRAFT STRUCTURE REPAIR; PREPARATION OF (WORK PACKAGE CONCEPT)
Notice on Issuance of Domestic Maintenance License
Interpretation of some clauses in "Regulations on Certification of Civil Aircraft Maintenance Personnel"
Maintenance Permit Application Guide
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