49.040 有关航空航天制造用镀涂和有关工艺 标准查询与下载

ASTM F1105-09(2014) 制备贮藏稳定性试验用液态, 温度敏感性或基于溶剂的飞行器清洁化合物标准实践规程

4.1 This practice determines the procedure to be used to ensure the long-term storage stability of aircraft cleaning and maintenance products in order to ensure their ability to meet the shelf-life requirements called up in specifications or contract documents. The subsequent testing requirements are detailed in the specification or contract. 1.1 This practice covers the determination of the stability in storage of liquid enzyme-based, terpene-based, and solvent-based chemical cleaning compounds used to clean the exterior surfaces of aircraft. 1.2 The values stated in SI units are to be regarded as the standard. The values given in parentheses are for information only. 1.3 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 Preparing Aircraft Cleaning Compounds, Liquid-Type, Temperature-Sensitive, or Solvent-Based, for Storage Stability Testing

SAE AMS2471G-2008 铝合金的阳极化处理.未染色镀层的硫酸处理

This specification establishes the engineering requirements for undyed anodic coatings on aluminum alloys. This process has been used typically to increase corrosion resistance and to provide surfaces which will promote adherence of paint and other organic finishes, but usage is not limited to such applications. AMS 2472 should be specified for coatings colored by dyeing. This process is not suitable for parts which contain joints or recesses in which the anodizing solution may be retained.

Anodic Treatment of Aluminum Alloys Sulfuric Acid Process, Undyed Coating

SAE AMS2408J-2008 镀锡

This specification covers the requirements for electrodeposition of tin on metals and the properties of the deposit. This process has been used typically to prevent galling or seizing of metal surfaces, to provide a surface for soft soldering, or to improve corrosion resistance, but usage is not limited to such applications.

Plating, Tin

SAE AMS2753C-2008 液体盐浴铁素体硝基渗碳无氰化物浴

This specification covers the requirements for an epsilon-iron nitride case on ferrous parts produced by immersion in a low-temperature, agitated, fused salt bath.1.2 ApplicationNitrocarburized surfaces have been used typically for increasing the resistance to wear and fatigue on ferrous alloys including carbon steels, low-alloy steels, tool steels, and corrosion-resistant steels, cast irons, and ferrous powder metalproducts, but usage is not limited to such applications.1.2.1 This process is not recommended for use on parts that have been plated with silver, copper, zinc, or cadmium or on parts having copper alloy inserts.1.3 Safety - Hazardous MaterialsWhile the materials, methods, applications, and processes described or referenced in this specification may involve the use 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 to take necessary precautionary measures to ensure the health and safety of all personnel involved.

Liquid Salt Bath Ferritic Nitrocarburizing Non-Cyanide Bath

DIN EN 4170:2008 航空航天系列.涂料和清漆.防冷裂缝温度循环测量的试验方法

This standard describes a procedure of ageing to assess the resistance of a coated panel (metallic or organic substrate) to a temperature cycle (cold, hot, hot and wet) for aerospace purposes. This test deals with the assessment of the capability of the paint to support modification of internal stresses without any crack formation, peeling or other defects due to modification of the mechanical properties of the paint system.

Aerospace series - Paints and varnishes - Test method for measurement of resistance to cold crack temperature cycle; German and English version EN 4170:2007

SAE AMS2430N-2008 自动喷丸加工处理

1.1 FormThis specification covers the engineering requirements for automatic peening of surfaces of parts by impingement of metallic shot, glass beads, or ceramic shot.1.2 ApplicationTo induce residual compressive stress in surface layers of parts, thereby increasing fatigue strength and resistance to stress-corrosion cracking but usage is not limited to such applications.

Shot Peening, Automatic

SAE AMS1528D-2008 飞行器外表面用压力喷洒式乳状清洁剂

This specification covers an emulsion-type, low-foaming cleaner in the form of a liquid. This cleaner has been used typically for removing soils from painted and unpainted exterior surfaces of aircraft by pressure spray or manual applications, but usage is not limited to such applications.

Cleaner for Aircraft Exterior Surfaces, Emulsion, Pressure-Spray Type

SAE AMS1523B-2008 飞行器外表面用水基凝胶清洁剂

This specification covers a thickened, water-base, type cleaner in the form of a gel. This cleaner has been used typically for removing soils from exterior surfaces of aircraft, such as landing gears, wheel wells, and flap cavities but usage is not limited to such applications.

Cleaner for Exterior Aircraft Surfaces Thickened or Gel-Type, Water-Base

SAE AMS1526C-2008 压力喷洒式水混溶的飞行器外表面用清洁剂

This specification covers a water-miscible, low-foaming cleaner in the form of a liquid. Primarily for removing soils from painted and unpainted exterior surfaces of aircraft by pressure spray or manual application.

Cleaner for Aircraft Exterior Surfaces Water-Miscible, Pressure-Spraying Type

SAE AMS1532D-2008 涂和擦洗飞行器外表面用胶状清洁剂

This specification covers an emulsion-type cleaner in the form of a liquid. This cleaner has been used typically for removing soils from painted and unpainted exterior metal surfaces of aircraft by a wipe-on, wipe-off procedure not requiring a water rinsing operation, but usage is not limited to such applications.

Cleaner for Aircraft Exterior Surfaces Wipe-On, Wipe-Off, Emulsion-Type

SAE AMS1540C-2008 推力反向装置用水基清洁剂

This specification covers a water-base cleaner in the form of a liquid. This cleaner has been used typically for removing thrust reverser stains and deposits from corrosion and heat resistant steel and aluminum alloy exterior surfaces of aircraft, but usage is not limited to such applications.

Cleaner, Thrust Reverser Water-Base

SAE AMS1531D-2008 涂和擦洗飞行器外表面用含悬浮擦洗固体颗粒的清洁剂

This specification covers a water-soluble cleaner containing suspended abrasive solids in the form of a ready-to-use liquid. This cleaner has been used typically for removing resistant soils from exhaust areas of exterior metal and painted surfaces of aircraft by a wipe-on, wipe-off procedure not requiring a water rinsing operation, but usage is not limited to such applications. NOT recommended for use on stretched or cast acrylic plastic.

Cleaner for Aircraft Exterior Surfaces Wipe-On, Wipe-Off, Containing Suspended Abrasive Solids

SAE AMS1547A-2008 钢材用箱式碱性电解阳极清洁剂

This specification covers an electrolytic alkaline cleaner in the form of a water soluble powder. Primarily for removing grease, oil, and loose surface contamination from steel components by immersion in a solution of the cleaner at elevated temperature with anodically applied current. This cleaner should not be used on titanium and other non-ferrous components.

Cleaner, Anodic, Electrolytic, Alkaline For Steel, Tank Type

SAE AMS1545B-2008 推力反向装置用碱性水基清洁剂

This specification covers an alkaline-type, water-base cleaner in the form of a liquid. This cleaner has been used typically for removing stains and carbon deposits from corrosion and heat resistant steel and titanium alloy thrust reverser parts removed from the aircraft, but usage is not limited to such applications. This cleaner will etch aluminum. If an aluminum-safe cleaner is required, SAE AMS 1540 should be used.

Cleaner, Thrust Reverser Alkaline, Water-Base

SAE AMS1529D-2008 飞行器外表面用压力喷洒式泡沫乳状清洁剂

This specification covers an emulsion-type, foam-on, pressure-spraying cleaner in the form of a liquid. This cleaner has been used typically for removing soils from painted and unpainted exterior surfaces of aircraft using foam-forming equipment, but usage is not limited to such applications.

Cleaner for Aircraft Exterior Surfaces Emulsion, Foam-On, Pressure-Spray Type

SAE AMS1370A-2008 采用浸没法的飞行器和航空航天元部件用液态除锈剂混合物

This specification covers a concentrated rusk removing compound in the form of a liquid to be diluted with water for use either at ambient or elevated temperature. This compound has been used typically for the removal of oxides from ferrous components during manufacturer or at overhaul, but usage is not limited to such applications. This product may be acidic or highly alkaline and may not be suitable for processing aluminum components. Avoid mixed metals during processing.

Compound, Rust Remover, Liquid Aircraft and Aerospace Components, Immersion Tank Method

SAE AMS1533B-2008 外部航空器表面溶剂基凝胶用清洁剂

1.1 FormThis specification covers a solvent-base cleaner in the form of a gel.1.2 ApplicationThis product has been used typically for removing soils from exterior surfaces of aircraft, such as landing gears, wheelwells, and flap cavities, but usage is not limited to such applications.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 to takenecessary precautionary measures to ensure the health and safety of all personnel involved.

Cleaner for Exterior Aircraft Surfaces Gel-Type, Solvent-Base

SAE AMS2415J-2008 铅和铟涂层

This specification covers the requirements for electrodeposited and diffused lead and indium plate. This process has been used typically to improve the performance and prevent corrosion of bearings or of other parts, but usage is not limited to such applications.

Plating, Lead and Indium

SAE AMS2411G-2008 高温设施用镀银工艺

This specification covers the engineering requirements for silver deposited on metal parts with a nickel strike between the basis metal and the silver deposit. This process has been used typically to prevent galling or seizing of surfaces of parts, such as fasteners, made of low-alloy steel, corrosion and heat resistant steel, and nickel alloys for use up to 1400 ?F (760 ?C).

Plating, Silver for High Temperature Applications

SAE AMS-C-27725C-2008 用于250℉(121℃)的航空器整体燃料箱用聚亚安酯防腐蚀涂层

This specification covers two types of polyurethane coatings. The coating materials covered by this specification have been used typically for the protection of aircraft integral fuel tanks against corrosion from fuel contaminants but usage is not limited to such applications. They are suitable for use in a service temperature range from -65 to +250 ?F (-54 to +121 ?C).

Coating, Corrosion Preventative, for Aircraft Integral Fuel Tanks for Use to 250 °F (121 °C)