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MILITARY SPECIFICATION军用规范ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS铝和铝合金的阳极氧化涂层This specification is approved for use by all Departments and Agencies of the Department of Defense.本规范可以用于国防部的所有部门及机构。
1. SCOPE 范围1.1 Scope. This specification covers the requirements for six types and two classes of electrolytically formed anodic coatings on aluminum and aluminum alloys for non-architectural applications (see 6.1).1.1范围本标准包括非建筑用途的铝和铝合金的6类和2级电解生产的阳极氧化膜的要求(见6.1)1.2 Classification. The anodic coating Types and Classes covered by this specification are as specified herein (see 6.2 and6.21):1.2 分类本标准所列阳极氧化膜的类型和级别如下：1.2.1 Types类型Type I- Chromic acid anodizing, conventional coatings produced from Chromic I 类---铬酸阳极氧化，在铬酸槽生成的常规氧化膜(见3.4.1)Type IB- Chromic acid anodizing, low voltage process, 22 ± 2V,(see 3.4.1)IB类---铬酸阳极氧化，低电压工艺，22±2V(见3.4.1)Type IC- Non-chromic acid anodizing, for use as a non-chromateIC类---非铬酸阳极氧化，应用非铬酸的配方生成的I和IB类氧化膜(见3.4.1)和(6.1.2)Type II- Sulfuric acid anodizing, conventional coatings produced fromsulfuric II类---硫酸阳极氧化，在硫酸槽生成的常规的氧化膜(见3.4.2)Type IIB- Thin sulfuric acid anodizing, for use as a non-chromateIIB类---硫酸阳极氧化膜，应用非铬酸的配方生成的I和IB类氧化膜(见3.4.1和6.1.2)Type IIIIII类---硬质阳极氧化膜(见3.4.3)1.2.2 Classes.等级Class 1 - Non-dyed (see 3.5.)1级-无染色(见3.5)Class 2 - Dyed (see 3.6.)2级-染色的(见3.6)Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be of use in improving this document should bead dressed to: Commanding Officer, Naval Air Warfare Center Aircraft Division Lakehurst, CodeSR3, Lakehurst, NJ 08733-5100, by using the Self-addressed Standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document or by letter有用备注(建议书、添加、删除)及任何相应资料都可以用于本文件的改进，可以将资料通过本文件末尾的标准化文件改进策划书(DD 格式1426)或信件的形式发给：新泽西08733-5100，莱克赫斯特，代码SR3，莱克赫斯特海军空战中心航空分部。
1993年9月10日替代旧规范MIL-A-8625E1988年4月25日铝及铝合金阳极氧化镀层的军用规范本规范经国防部各部门和机构批准使用1.范围1.1范围. 本标准包括非建筑用途的铝及铝合金的 6 个类型和 2 个等级电解生成的阳极氧化镀层的要求（见6.1）。
1.2分类. 本规范涵盖的阳极镀层类型和等级如下所述（见6.2和6.21）：2.引用文件2.1政府文件.2.1.1规范和标准. 在本文件规定的范围内，以下规范和标准构成本文件的一部分。
除非另有规定，这些文件的版本是国防部规范和标准索引（DODISS）及其补充中所列的版本，并在招标书中引用。
军用规范MIL-P-23377 -底漆涂层，环氧聚酰胺，耐化学和溶剂MIL-C-81706 -铝及铝合金涂层用化学转化材料MIL-P-85582 -底漆：环氧树脂，水性MIL-STD-105 -检验抽样程序及抽样表联邦标准QQ-A-250/4 - 2024铝合金板材FED-STD-141 -油漆、清漆和相关材料：取样和试验方法FED-STD-151 -金属试验方法（除非另有说明，联邦和军用规范和标准的副本可从DODSP客户服务处获得，标准化文件订购处，地址：宾夕法尼亚州费城罗宾斯大道700号40号楼，19111-5094）2.2非政府出版物. 在本文件规定的范围内，以下文件构成本文件的一部分。
国防部采用招标书中引用的文件版本。
除非DODISS中未列出的文件为招标文件（见6.2）。
.美国材料试验协会（ASTM）ASTM B117 -盐雾试验方法ASTM B137 -铝上阳极镀层重量的测量ASTM B244 -用涡流仪测量铝和其他非磁性基体金属的阳极镀层厚度ASTM D822 -涂料、清漆和相关产品试验用光和水暴露装置（碳弧型），操作标准实施规程ASTM D2244 -不透明材料的色差，仪器评价ASTM G23 -非金属材料曝光用曝光装置（碳弧型）的操作规程ASTM G26 -非金属材料曝光用有水和无水的操作曝光装置（氙弧型）（副本的申请应寄往美国材料试验协会，地址：1916 Race Street，Philadelphia，PA 19103。
美国军用标准（MIL-PRF-13830B）性能标准军火控制设备用光学组件；监控生产、装配、检测的通用标准所有防御和代理部门可允许使用此种标准。
1.范围1.1 范围。
此标准包括精加工光学组件的生产、装配、检测，诸如：透镜，棱镜，面镜、光栅、窗口以及用于防火仪器或设备。
2.应用文件2.1本章列出的档需要满足本标准3、4、5章的要求。
本章不包括本标准其它章节的文件或其它信息推荐的文件。
为了保证本目录的完整性，文件使用者必须注意档须满足本标准3、4、5章列出的档要求，无论这些内容是否在本章中列出。
2.2 其它政府档，图纸及出版下列政府其它档、图纸和出版组成本档内容的一部分，扩大本文的范围。
除非另有规定，这些档、图纸和出版是征求引用的。
图纸C7641866---光学组件表面质量标准（立约人要求的其它政府档、图纸、出版复印件及具体的功能应该从签约事宜或签约指示得到。
）2.3 优先级本标准内容与其引出的参考有冲突时，以本标准内容为准。
本标准未述内容，可行法律法规代行除非有具体的免除通知。
（看附加有限标准合同条令）3.要求：3.1所有的光学组件，配件以及系统产品都必须符合这一标准的要求，除非具体的仪器标准或合同之可行图纸另有要求与定义。
3.2所用的材料也必须与图纸的说明以及使用档的标准相一致3.2.1玻璃光学组件在规格，以及级别必须与图纸要求相一致。
允许使用玻璃材料时，应提供给合同管理人员相关的玻璃光学特性及设计数据完整的信息。
3.2.1.1 放射性材料本文中要求的光学材料应不含钍或其它加入的超过0.05%重量的放射性材料。
3.2.2 粘着力除非合同和定单中有特殊说明，光学粘合剂必须同附录A的要求相一致。
3.2.3 粘连材料对于玻璃同金属相粘连，必须与附录D的要求相一致3.2.4密封材料用于密封的材料必须与附录E的要求相一致3.2.5 增透膜用于光学表面镀膜的增透膜必须与附录C的要求相一致3.2.5.1 反射表面铝化反射面必须与附录B的要求相一致3.3机械尺寸大小光学组件必须与合同以及图纸的要求的尺寸和光学数据相一致3.3.1边所有光学组件都应当倒边在（0.020-0.005英寸在45度+/-15度），沿面宽进行测量，除非有特殊指定。
MIL-A-8625F1998年4月25日美国军事标准铝和铝合金的阳极氧化膜此标准由由美国国防部所有部门和科室批准使用1.范围1.1范围本标准包括非建筑用途的铝和铝合金的6类和2级电解生成的阳极氧化膜的要求（见6.1）。
1.2分类本标准所列阳极氧化膜的类别和级别如下：1.2.1分类Ⅰ类- 铬酸阳极氧化，在铬酸槽生成的常规氧化膜（见3.4.1）ⅠB类- 铬酸阳极氧化，低电压工艺，22±2V（见3.4.1）ⅠC类- 非铬酸阳极氧化，应用非铬酸的配方生成的Ⅰ和ⅠB类氧化膜（见3.4.1和6.1.2）Ⅱ类- 硫酸阳极氧化，在硫酸槽生成的常规氧化膜（见3.4.2）ⅡB类- 硫酸阳极氧化薄膜，应用非铬酸的配方生成的Ⅰ和ⅠB类氧化膜（见3.4.1和6.1. 2）Ⅲ类- 硬质阳极氧化膜（见3.4.3）1.2.2级别1级- 不染色（见3.5）2级- 染色（见3.6）2.适用文件2.1政府文件2.1.1规范和标准下面的规范和标准构成本标准的组成部分。
（此处有删节）规范军事规范MIL-P-23377 耐化学和溶剂腐蚀的环氧聚酰胺涂层，MIL-C-81706 铝和铝合金的化学转化膜MIL-P-85582 水性环氧树脂涂层联邦规范QQ-A-250/4 2024铝合金的板和薄板标准联邦标准FED-STD-141 油漆，清漆，硝基漆和相关材料：取样和测试方法。
FED-STD-151 金属：测试方法军事标准MIL-STD-105 取样程序和质量检查表2.2非政府出版物下面的规范和标准构成本标准的组成部分。
（此处有删节）美国试验和材料学会(ASTM)ASTM B 117 盐雾试验方法ANSI/ASTM B 137 铝和铝合金的阳极氧化膜的重量测试ASTM B 224 利用涡流仪测试铝氧化膜厚度，以及其它非磁性材料上的非导电层的厚度 ASTM D 822 测定油漆，清漆，硝基漆和其它产品的曝光和曝水仪（碳-电弧型）的标准使用方法ASTM D 2244 不透明材料色差的仪器测试ASTM G 23 有水和无水的非金属材料曝光测试的曝光仪（碳-电弧型）的标准使用方法 ASTM G 26 有水和无水的非金属材料曝光测试的曝光仪（氙-电弧型）的标准使用方法2.3优先程序在本标准和所引用的参考文件有矛盾时，本标准具有优先权，但是本标准不能超越现行的相关法律和法规。
MIL美国军用标准标准2010年最新标准目录以下MIL美国标准化组织标准信息只供参考，具体情况，请咨询--中国标准信息网MIL-PRF-22684/8C (1) 2009.02.05 RESISTORS, FIXED, FILM, INSULATED, STYLE RL42鈥?TXMIL-PRF-19500/483D 2009.04.02 SEMICONDUCTOR DEVICE, SILICON, HIGH-POWER, THREE PHASE, FULL WAVE B RIDGE RECTIFIER, TYPES M19500/483-01 THROUGH M19500/483-04, JANTXMIL-PRF-27/111A 2009.09.29 TRANSFORMERS AND INDUCTORS, (AUDIO, POWER AND HIGH-POWER PULSE) INDU CTOR, AUDIOMIL-PRF-19500/169N 2009.11.02 SEMICONDUCTOR DEVICE, DIODE, SILICON, SWITCHING,TYPES 1N3070, 1N3070-1, 1N3070UR-1, 1N4938, 1N4938-1, 1N4938UR-1, JAN, JANTX, JANTXV, JANHC, AND JANKCMIL-PRF-27/79A 2009.11.09 TRANSFORMERS, AUDIO FREQUENCYMIL-DTL-3943/129C 2010.01.08 DECORATION, EXCEPTIONAL ENGINEERING ACHIEVEMENT MEDAL, NASAMIL-DTL-3943/145D 2010.01.15 DECORATION, MERITORIOUS CIVILIAN SERVICE AWARD, DEFENSE INFORMATION S YSTEMS AGENCYMIL-DTL-3943/139C 2010.01.26 DECORATION, NATIONAL COMMUNICATI***** SYSTEMS MEDALMIL-DTL-3943/153B 2010.01.15 DECORATION, SPECIAL ASSIGNMENT AWARD, U.S. PUBLIC HEALTH SERVICEMIL-DTL-3943/186A 2010.03.26 MEDAL, ARMY OF CUBAN OCCUPATIONMIL-PRF-55629/5G 2010.03.10 CIRCUIT BREAKERS, MAGNETIC, UNSEALED TRIP-FREE, THREE POLE (0.2 TO 50 A MPERES)MIL-DTL-11589/493A 2010.04.30 RIBBON, EXCEPTIONAL CIVILIAN SERVICE AWARD, CIVILIAN PERSONNEL MANAGE MENT SERVICE, DEPARTMENT OF DEFENSEMIL-DTL-3943/138D 2010.01.08 DECORATION, EXCEPTIONAL ACHIEVEMENT MEDAL, NASAMIL-DTL-11484/80E 2008.09.30 LAPEL BUTTON, DISTINGUISHED SERVICE AWARD, DEFENSE CONTRACT AUDIT AG ENCYMIL-DTL-11589/583 2003.03.20 RIBBON, EXCEPTIONAL ADMINISTRATIVE ACHIEVEMENT MEDAL, NASAMIL-PRF-914/4B (3) 2010.02.05 RESISTOR NETWORK, FIXED, FILM, SURFACE MOUNT, 20-PIN, LEADLESS CHIP CA RRIER, NONESTABLISHED RELIABILITY AND ESTABLISHED RELIABILITY, STYLE RNS040ARMY MIL-PRF-32271/14 2008.10.30 BATTERY, NON-RECHARGEABLE, LITHIUMMIL-PRF-62546C 2010.01.26 SENSOR, FIRE, OPTICALMIL-DTL-3922/62D 2010.01.08 FLANGES, WAVEGUIDE (CHOKE) (ROUND, 8 HOLE (2 HOLES CENTERED HORIZONTA LLY, 2 HOLES CENTERED VERTICALLY))MIL-DTL-8878K (1) 2009.02.17 TURNBUCKLES, POSITIVE SAFETYING, GENERAL SPECIFICATION FORMIL-DTL-21617/27 VALID NOTICE 1 2008.04.30 Connector, Female Plug Electrical, Rectangular, Polarized Shell, Miniature Type, Mixed Socket Contacts (Style 016C)MIL-M-38510/123B VALID NOTICE 1 2009.02.26 Microcircuits, Linear, Cmos, Negative Logic, Analog Switch, Monolithic SiliconMIL-PRF-19500/624D 2009.06.18 SEMICONDUCTOR DEVICE, DARLINGTON TRANSISTOR, NPN, SILICON, HIGH-POWE R, TYPE 2N7370, JAN, JANTX, JANTXV, AND JANSDOD-A-15707D (2) 1989.01.25 ANCHORS, NAVY, LIGHTWEIGHT TYPE (METRIC)DOD-A-17254A 1985.08.23 ANCHORS, NAVY, LIGHTWEIGHT (HADFIELD MANGANESE CAST STEEL LOW MAGNETIC PERMEABILITY) (METRIC)DOD-A-82720 NOTICE 3 2004.11.23 ADHESIVE, MODIFIED-EPOXY, FLEXIBLE, TWO-PART (METRIC)DOD-C-2687B VALID NOTICE 1 1987.06.02 COMPOUND, BATTERY-SEALING (METRIC)DOD-C-82656 (2) 1978.11.15 CARBON BLACK,THERMALMIL-C-82656 1977.01.31 CARBON BLACK,THERMALDOD-C-82660 (1) 1978.03.01 CHROMIUM 2 ETHYL HEXOATE, TECHNICALMIL-C-82660 1977.01.31 CHROMIUM 2 ETHYL HEXOATE, TECHNICALDOD-C-82665 (1) 1978.11.15 CARBON BLACKMIL-C-82665 1977.01.31 CARBON BLACKDOD-D-23443B (2) 1995.10.27 DI-(2-ETHYLHEXYL) ADIPATE, TECHNICAL (METRIC)DOD-E-8983C VALID NOTICE 1 1992.09.04 ELECTRONIC EQUIPMENT, AEROSPACE, EXTENDED SPACE ENVIRONM ENT, GENERAL SPECIFICATION FORDOD-G-24508A (4) 1998.09.23 GREASE, HIGH PERFORMANCE, MULTIPURPOSE (METRIC)DOD-G-82673 (1) 1978.06.15 GRAPHITE, NATURAL, POWERED, TECHNICALMIL-G-82673 1977.11.23 GRAPHITE, NATURAL, POWERED, TECHNICALDOD-L-25681D VALID NOTICE 2 1991.05.01 LUBRICANT MOLYBDENUM DISULFIDE, SILICONEDOD-L-81846B (2) 2000.03.02 LUBRICATING OIL, INSTRUMENT, BALL BEARING, HIGH FLASH POINTMIL-P-63464/6B VALID NOTICE 1 2005.07.01 PIN, GROOVED, HEADLESS-LONGITUDINAL CENTER GROOVE, CORRO SION-RESISTANT STEEL, METRICMIL-P-63464/6B 1992.01.17 PIN, GROOVED, HEADLESS-LONGITUDINAL CENTER GROOVE, CORROSION-RESISTANT STEEL, METRICDOD-R-23679F 1986.08.08 REAGENTS, STANDARD, WATER TEST CHEMICALS (METRIC)DOD-STD-1399 -301A 1986.07.21 INTERFACE STANDARD FOR SHIPBOARD SYSTEMS SECTION 301A SHIP MOTION AND ATTITUDE (METRIC)DOD-T-17412C 1978.09.20 TEST KIT, WATER, ENGINE COOLING SYSTEMS (METRIC)DOD-T-82666A VALID NOTICE 1 1987.05.13 TRIS-1-(2 METHYL AZIRIDINYL) PHOSPHINE OXIDEDOD-Z-82674 NOTICE 1 1999.07.10 ZIRCONIUM CARBIDE, POWERED, TECHNICALMIL-Z-82674 1977.11.23 ZIRCONIUM CARBIDE, POWERED, TECHNICALMIL-A-159D VALID NOTICE 1 1999.07.14 ANTIMONY SULFIDE (FOR USE IN AMMUNITION)MIL-A-159D 1972.05.16 ANTIMONY SULFIDE (FOR USE IN AMMUNITION)MIL-A-166C VALID NOTICE 2 1999.07.13 AMMONIUM PICRATE (EXPLOSIVE D)MIL-A-166C 1975.01.06 AMMONIUM PICRATE (EXPLOSIVE D)MIL-A-192B VALID NOTICE 2 1999.08.18 AMMONIUM PERCHLORATEMIL-A-192B 1965.09.02 AMMONIUM PERCHLORATEMIL-A-417G VALID NOTICE 1 1988.10.24 ADAPTER, PRIMING, M1A4MIL-A-417G 1983.02.27 ADAPTER, PRIMING, M1A4MIL-A-516J 1981.09.01 AUGER, EARTH, SKIDMOUNTED; AND AUGER, EARTH, TURNTABLE BASE MOUNTED, POWE R DRIVENMIL-A-2334J 1991.03.15 APRON, TOXICOLOGICAL AGENTS PROTECTIVE, M-2MIL-A-3316C (2) 1990.08.23 ADHESIVES, FIRE-RESISTANT, THERMAL INSULATIONMIL-A-3316C 1987.10.20 ADHESIVES, FIRE-RESISTANT, THERMAL INSULATIONMIL-A-3850 VALID NOTICE 1 1986.04.10 ACETYLENE BLACKMIL-A-3850 1952.12.24 ACETYLENE BLACKMIL-A-3962E 1986.05.19 ANCHORS, GROUND, ARROWHEAD WITH DRIVING EQUIPMENTMIL-A-5034B VALID NOTICE 1 1987.03.02 ADAPTER, BOMB RACK, 30 INCH, AERO 1AMIL-A-5034B 1979.11.02 ADAPTER, BOMB RACK, 30 INCH, AERO 1AMIL-A-6752A REINST NOTICE 2 1978.03.01 AMMETERS, VOLTMETERS, AND LOADMETERS; DIRECT CURRENTMIL-A-6752A (3) 1958.03.03 AMMETERS, VOLTMETERS, AND LOADMETERS; DIRECT CURRENTMIL-A-6752A 1953.12.24 AMMETERS, VOLTMETERS, AND LOADMETERS; DIRECT CURRENTMIL-A-6848 VALID NOTICE 1 1955.12.06 ACCELEROMETER; AIRCRAFTMIL-A-6848 1950.08.21 ACCELEROMETER; AIRCRAFTMIL-A-7237B (1) 1981.05.19 AIR INDUCTION SYSTEM, RECIPROCATING ENGINE, GENERAL SPECIFICATION FOR MIL-A-7237B 1975.02.04 AIR INDUCTION SYSTEM, RECIPROCATING ENGINE, GENERAL SPECIFICATION FORMIL-A-7647C VALID NOTICE 2 1971.10.12 AIR CONDITIONER, TRAILER MOUNTED, FREON CYCLE, GASOLINE ENGI NE DRIVEN, 4 TON REFRIGERATING CAPACITY, TYPE A-3MIL-A-7647C 1958.08.22 AIR CONDITIONER, TRAILER MOUNTED, FREON CYCLE, GASOLINE ENGINE DRIVEN, 4 TO N REFRIGERATING CAPACITY, TYPE A-3MIL-A-8625F (1) 2003.09.15 ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYSMIL-A-8625F 1993.09.10 ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYSMIL-A-8860B 1987.05.20 AIRPLANE STRENGTH AND RIGIDITY, GENERAL SPECIFICATION FORMIL-A-8861B (1) 1994.12.05 AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADSMIL-A-8861B 1986.02.07 AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADSMIL-A-8863C 1993.07.19 AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES MIL-A-8865B 1987.05.20 AIRPLANE STRENGTH AND RIGIDITY MISCELLANEOUS LOADSMIL-A-8866C VALID NOTICE 1 1994.10.03 AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCEMIL-A-8866C 1987.05.20 AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FA TIGUE AND DAMAGE TOLERANCEMIL-A-8867C VALID NOTICE 1 1994.10.03 AIRPLANE STRENGTH AND RIGIDITY GROUND TESTSMIL-A-8867C (1) 1993.03.25 AIRPLANE STRENGTH AND RIGIDITY GROUND TESTSMIL-A-8867C 1987.06.10 AIRPLANE STRENGTH AND RIGIDITY GROUND TESTSMIL-A-8869B VALID NOTICE 1 1994.06.20 AIRPLANE STRENGTH AND RIGIDITY NUCLEAR WEAP***** EFFECTSMIL-A-8869B 1987.05.20 AIRPLANE STRENGTH AND RIGIDITY NUCLEAR WEAP***** EFFECTSMIL-A-8870C 1993.03.25 AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCEMIL-A-9132 1953.11.02 AMPLIFIER, STABILIZATION, BOMBING NAVIGATIONAL COMPUTER, TYPE B-1MIL-A-9207B (1) 1956.04.20 ANALYZER, IGNITION AND VIBRATION, AIRCRAFT RECIPROCATING ENGINEMIL-A-9207B 1955.10.12 ANALYZER, IGNITION AND VIBRATION, AIRCRAFT RECIPROCATING ENGINEMIL-A-9410 (1) 1954.06.18 ANTENNAS, FM COMMUNICATION EQUIPMENT, GENERAL SPECIFICATION FOR DESIGN AND PLACEMENT OFMIL-A-9410 1954.04.05 ANTENNAS, FM COMMUNICATION EQUIPMENT, GENERAL SPECIFICATION FOR DESIGN AN D PLACEMENT OFMIL-A-9457A (1) 1959.04.27 AMPLIFIER, ELECTRONIC CONTROL, BOMBING NAVIGATIONAL COMPUTER, TYPE MD-1 MIL-A-9457A 1959.04.27 AMPLIFIER, ELECTRONIC CONTROL, BOMBING NAVIGATIONAL COMPUTER, TYPE MD-1 MIL-A-10516 1950.09.14 ADAPTER, SKATE TEST CLUSTER (100-LB. SIZE)MIL-A-10593A 1953.02.04 AIR SAMPLER MX-1191 ( )/TDQ-1MIL-A-10982F (1) 1969.04.01 ARMING WIRE ASSEMBLIESMIL-A-10982F 1968.08.19 ARMING WIRE ASSEMBLIESMIL-A-11221A NOTICE 2 1997.02.27 ARMING PLUG, MINE, ANTITANK M4 (PRACTICE) AND M4A1MIL-A-11221A VALID NOTICE 1 1988.05.20 ARMING PLUG, MINE, ANTITANK M4 (PRACTICE) AND M4A1MIL-A-11221A (2) 1964.02.14 ARMING PLUG, MINE, ANTITANK M4 (PRACTICE) AND M4A1MIL-A-11221A 1962.02.22 ARMING PLUG, MINE, ANTITANK M4 (PRACTICE) AND M4A1MIL-A-11356F 1987.05.22 ARMOR, STEEL, CAST, HOMOGENEOUS, COMBAT-VEHICLE TYPE (1/4 TO 8 INCHES, INCL USIVE)MIL-A-11557A 1954.08.09 ANTENNA ASSEMBLY AS-574( )/URR (COMPONENTS OF)MIL-A-13338E VALID NOTICE 1 1988.10.24 AIMING CIRCLE, M2 AND M2A2, WITH EQUIPMENTMIL-A-13338E (1) 1983.08.11 AIMING CIRCLE, M2 AND M2A2, WITH EQUIPMENTMIL-A-13338E 1982.03.22 AIMING CIRCLE, M2 AND M2A2, WITH EQUIPMENTMIL-A-13374E NOTICE 4 1998.03.03 ADHESIVE, DEXTRIN, FOR USE IN AMMUNITION CONTAINERSMIL-A-13374E REINST NOTICE 3 1998.03.03 ADHESIVE, DEXTRIN, FOR USE IN AMMUNITION CONTAINERSMIL-A-13374E VALID NOTICE 1 1988.10.31 ADHESIVE, DEXTRIN, FOR USE IN AMMUNITION CONTAINERSMIL-A-13374E 1983.08.25 ADHESIVE, DEXTRIN, FOR USE IN AMMUNITION CONTAINERSMIL-A-13479 1954.06.18 ANEMOMETER ML-497( )/PMMIL-A-14178 1955.10.14 AMPLIFIER, AUDIO FREQUENCY AM-719( )/UMIL-A-14457 1957.12.31 ANTENNA AT-640( )/ARNMIL-A-14641B NOTICE 5 2001.07.21 AIGUILLETTE, AF COMMAND BANDSMIL-A-14641B 1981.06.30 AIGUILLETTE, AF COMMAND BANDSMIL-A-14897 NOTICE 2 1999.07.10 ACTUATOR, ROTARY 1000-34 ASSEMBLYMIL-A-14897 VALID NOTICE 1 1988.08.29 ACTUATOR, ROTARY 1000-34 ASSEMBLYMIL-A-14897 1969.07.20 ACTUATOR, ROTARY 1000-34 ASSEMBLYMIL-A-14898 NOTICE 2 1999.07.10 ACTUATOR, ROTARY 1000-34 REMANUFACTURED METAL PARTS ASSEMBLY MIL-A-14898 VALID NOTICE 1 1986.06.20 ACTUATOR, ROTARY 1000-34 REMANUFACTURED METAL PARTS ASSEM BLYMIL-A-14898 1969.07.20 ACTUATOR, ROTARY 1000-34 REMANUFACTURED METAL PARTS ASSEMBLYMIL-A-15303P 1986.11.19 AUDIBLE SIGNALS: ALARMS, BELLS, BUZZERS, HORNS, AND SIRENS, ELECTRONIC, SHIP BOARDMIL-A-15344J (2) 1990.11.02 AMPLIFIER, SYNCHRO SIGNALMIL-A-15344J 1963.06.07 AMPLIFIER, SYNCHRO SIGNALMIL-A-16749E (2) 1968.06.17 AMPLIFIER, AUDIO FREQUENCY, SOUND POWERED TELEPHONE SYSTEMMIL-A-16749E 1963.05.15 AMPLIFIER, AUDIO FREQUENCY, SOUND POWERED TELEPHONE SYSTEMMIL-A-17196E 1977.10.07 ALARM SWITCHBOARDS, ALARM PANELS, REMOTE SENTRY ALARM SWITCH, SIGNAL UN ITS, AND SPECIAL ALARM CONNECTION BOX, NAVAL SHIPBOARDMIL-A-17367D (1) 1978.09.11 ARMOR, BODY, FRAGMENTATION PROTECTIVE: UPPER TORSO (WITH COLLAR, M-195 5)MIL-A-17367D 1977.10.03 ARMOR, BODY, FRAGMENTATION PROTECTIVE: UPPER TORSO (WITH COLLAR, M-1955) NAVY MIL-A-18001K INT AMD 3 NOTICE 1 2008.08.28 ANODES, SACRIFICIAL ZINC ALLOYMIL-A-18194 1954.09.17 ATTACK DIRECTOR MARK 5 MOD 2MIL-A-18455C VALID NOTICE 1 1991.06.07 ARGON, TECHNICALMIL-A-18455C 1986.12.23 ARGON, TECHNICALMIL-A-18717C 1993.09.20 ARRESTING HOOK INSTALLATION, AIRCRAFTMIL-A-18924 1955.06.29 ARMING CELLS MK 1 MODS 5, 6, 7, AND 8MIL-A-19521B 1992.05.04 ANODE RETAINING SUPPORT PLUGS AND ANODE SELECTION AND INSTALLATION DESI GN CRITERIA FOR SHIPBOARD CONDENSERS AND HEAT EXCHANGERSMIL-A-19736A (2) 1966.03.16 AIR REFUELING SYSTEMS, GENERAL SPECIFICATION FORMIL-A-19736A 1960.08.05 AIR REFUELING SYSTEMS, GENERAL SPECIFICATION FORMIL-A-19865C 1990.03.20 AIR CONDITIONER, MECHANICALLY REFRIGERATEDMIL-A-19879B 1977.11.23 ARMOR, BODY, FRAGMENTATION PROTECTIVE: LOWER TORSOMIL-A-21016F 1990.05.21 ADHESIVE, RESILIENT DECK COVERINGMIL-A-21165A NOTICE 2 2004.08.23 ADAPTER, QUICK DISCONNECT, PASSENGER SEAT TO FLOORMIL-A-21165A 1965.08.27 ADAPTER, QUICK DISCONNECT, PASSENGER SEAT TO FLOORMIL-A-22262B (2) 1996.03.21 ABRASIVE BLASTING MEDIA SHIP HULL BLAST CLEANINGMIL-A-22262B 1993.04.05 ABRASIVE BLASTING MEDIA SHIP HULL BLAST CLEANINGMIL-A-23054A VALID NOTICE 1 1990.12.24 ACOUSTIC ABSORPTIVE BOARD, FIBROUS GLASS PERFORATED FIBRO US GLASS CLOTH FACEDMIL-A-23054A (1) 1984.06.25 ACOUSTIC ABSORPTIVE BOARD, FIBROUS GLASS PERFORATED FIBROUS GLASS CL OTH FACED。
MIL-A-8625E3.3.1.2 复杂工件阳极氧化：对形状复杂的工件进行阳极氧化时，电解质可能包埋工件孔穴。
所以，如采用本工艺，则须确保不会因电解质包埋而引发后续损伤（除指定特定镀层外，应采用I类或IA类镀层）。
3.3.2 处置及清洗应在前处理、阳极氧化及后处理中处置工件，以避免机械损耗及污染。
工件上不得有任何杂质、氧化物或土，包括：油脂、油污、涂料及助焊剂。
应采取适当清洗工序去除工件表面的氧化层及其它干扰层，以确保表面清洁且无水膜残痕。
因为磨料中含有铁、钢丝棉、粗糙的铁氧化物及钢线，这些物质都可能嵌进金属，加速铝及其合金的腐蚀，故阳极氧化前禁止采取机械清洗。
如要求进行特定清洗，则应在合同或订单中表明（见6.2）。
3.3.3 镜面表面处理如合同或订单中已指定（见6.2），则需在阳极氧化前将需要取得高反射性表面的工件进行化学或电化学光亮处理(见6.9）。
3.3.4 修整（机械损耗、接触痕）除非另有规定，否则任何机械损耗区域（阳极氧化层磨损，但未伤及工件的区域）应采用化学转化材料（参见1A类镀层QPL-81760）及其它可实施的方法进行修整。
本修整条例只适用于不慎导致的机械损伤，如划痕。
针对III类镀层，只能对后期不会遭受研磨的区域进行修整（见6.1.1）。
受损区域应小于总阳极氧化面积5%,否则不予整修。
如在合同或订单中有明确规定（见6.2），可采用上述用于修整机械损伤的方法来修整接触痕。
3.4 镀层正如合同、订单及可实施提款中所指定，可通过任何工艺或操作在铝和铝合金表面形成特定膜，以制得传统阳极氧化层。
3.5 I、IB和IC类镀层I和IB类镀层：在含有铬酸的槽液中电解处理铝和铝合金，从而在金属表面生成均一阳极氧化膜。
IC类镀层：在含有矿物质或含有矿物质和有机酸混合物（不含铬酸）的槽液中电解处理铝和铝合金，从而在金属表面生成均一的阳极氧化膜。
除非在合同、订单或可实施的条款中已明确，否则，不得采用标定铜含量>5%，或标定硅含量>7%，或标定合金成分的总含量>7.5%的铝合金来制取I类镀层。
MILITARY SPECIFICATIONANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYSThis specification is approved for use by all Departments and Agencies of the Department of Defense.1. SCOPE1.1 Scope. This specification covers the requirements for six types andtwo classes of electrolytically formed anodic coatings on aluminum andaluminum alloys for non-architectural applications (see 6.1). ~1.2 Classification. The anodic coating Types and Classes covered by thisspecification are as specified herein (see 6.2 and 6.21):1.2.1 TypesTYPE I --Chromic acid anodizing, conventional coatings produced from chromic acid bath (see 3.4.1)TYPE II --Sulfuric acid anodizing, conventional coatings produced from sulfuric acid bath (see 3.4.2)3.4.1 Type I, IB, and IC coatinqs. Type I and IB coatings shall be theresult of treating aluminum and aluminum alloys electrolytically in a bathcontaining chromic acid to produce a uniform anodic coating on the metalsurface. Type IC coatings shall be the result of treating aluminum andaluminum alloys electrolytically in a bath containing mineral or mixedmineral/organic acids (non-chromic acid) to produce a uniform anodic coatingon the metal surface. Unless otherwise specified in”the contract, purchaseorder or applicable drawing, Type I coatings shall not be applied to aluminumalloys with a nominal copper content in excess of 5.0 percent; nominal siliconcontents in excess of 7.0 percent; or when the total allowable contents ofnominal alloying elements exceed 7.5 percent. Heat treatable alloys which areto receive a Type I, IB, or IC coating shall be in the required temperobtained by heat treatment, such as -T4, -T6, or T73, prior to anodizing.3.4.2 Type II and 116 coatlnqs. Type II and 116 coatings shall be theresult of treating aluminum and aluminum alloys electrolytically in a bathcontaining sulfuric acid to produce a uniform-anodic coating on-the metalsurface. Heat treatable alloys shall be in the required temper obtained byheat treatment, such as -T4, -T6,or T73, prior to anodizing.Class 1 -Non-dyed (see 3.5.)Beneficial comments (recommendations, additions, deletions) and anypertinent data which may be of use tn improving this document should beaddressed to: commanding Officer, Naval Air Warfare Center AircraftOivtslon Lakehurst, Code SR3, Lakehurst, NJ 08733-5100, by using theself-addressed Standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document or by letter.3.5 Class 1. When class 1 is specified in the contract or purchase order(see 6.2), the anodic coating shall not be dyed or pigmented. Any naturalcoloration resulting from anodic treatment with the various alloy compositionsshall not be considered coloration. The characteristic color Imparted by thesealing process shall also be considered as non-dyed.6.2 Acquisition requirements. Acquisition documents should specify the following:a. Title, number and date of this specification.b. Type of anodic coating (see 1.2.11).c. Class of anodic coatinq (see 1.2.21).d. Special process operatinq conditions, if applicable ( see 3.2).e. Special cleaning and fabrication requirements (see 3.3.1, 3.3.2,and 3.3.3).f. If coating weight for Type IC can exceed the maximum specified inTable I.g. Color and uniformity of Class 2 coatings, if applicable (see 3.6.1 and 3.12}.h. Degree of non-uniformity of dyed casting alloys (see 3.6.1.1).i. Light fastness resistance, if applicable, and a Delta E value if different than 3 (see3.7.1.3).j. Type III coating thickness, if applicable (see 3.7.2.1).k. Coating weight for thickness, Type III, if substituted (see 3.7.2.1.1).l. Special sealing requirements (see 3.8).m. When applicable, the allowable difference in anodic coating appearance resulting from inherent base metal differences (see 3.13).n. Provide the specific location of contact marks if important to the function of the part (see 3.13.1 and 6.14).o. Acceptance criteria for quality conformance inspections (see 4.4.2 and 6.20).P. If paint adhesion testing is required for quality conformance testing (see 4.4) and the required paint system (if different than that in 4.4.3.1).MMC（MultiMedia Card）卡由西门子公司和首推CF的SanDisk于1997年推出。
Type1—铬酸阳极Type2硫酸阳极Type3—低温硬质氧化軍用規格說明鋁和鋁合金的陽極氧化塗層这些说明以经过所有防卫部门和代理处的批准。
范围1.1 范围。
这些说明包话六种类型和两种电流形成的铝胶片阳极电镀和非建筑物的铝合金的一些具体要求1.2 分类：阳极氧化涂层的形式和分类的一些具体事项也在此说明（见6.2和6.21）1.2.1 类型TYPE I---含三价铬酸阳极电镀，常规胶片是从铬酸盐中提炼出来。
TYPE IB-含三价铬酸阳极电镀，低电压工序22±2V（见3.4.1）TYPE IC--- 非三价铬阳极电镀，用作一种转换TYPE I和IB涂层的非铬酸盐（见3.4.1和6.1.2）TYPEII---- 硫磺酸阳极电镀。
常规的涂层是从硫磺酸提炼出来的TYPEIII----薄硫磺酸阳极电镀，用作一种非铬酸盐来转换TYPE I和IB涂层的。
TYPEIII--- 坚硬的阳极氧化涂层处理。
1.2.2 分类.类别1 非染色（见3.5）类别2 染色（见3.6）2.可应用文件2.1官方文件2.1.1 详细说明和标准.以下具体要求和标准形成文件一部份。
除非有特别要求。
这些文件的问题争端已在防卫部门争端问题上列举出来。
具体说明军方MIL-P-23377 初次涂层，环氧聚酰胺和化学溶剂低抗。
MIL-C-81706 铝胶片和铝合金的材质化学转换MIL-P-85582 初次涂层，环氧化和水上处理。
联邦QQ-A –250/4 铝合金2024标准联邦FED-STD-141- 印刷、清漆、以及一些相关材质的取样和测试方法FED-STD-151- 金属检测方法军方MIL-STD-105—通过分配来对取样工序和表格来检测2.2 非官方发行物，在某中程度上要求已特别注名在内，除非有特别要求，DOD采纳的文件争端问题已在DODISS争端上列举出来。
美国检测材质方法ATMS B 117----盐喷射检测方法ANSI/ASTM B 137----测量铝在阳极电镀重量ASTM B 244 铝胶片在阳极电镀上的浓度和另一种非导体胶片在无磁性金属基础上旋转仪器上量。
NOT MEASUREMENTSENSITIVEMIL-A-8625FAMENDMENT 115 September 2003MILITARY SPECIFICATIONANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS This amendment forms a part of MIL-A-8625F, dated 10 September 1993, and is approved for use by all Departments and Agencies of the Department of Defense.PAGE 22.1.1, under SPECIFICATIONS, MILITARY: Delete “MIL-C-81706 – Chemical Conversion Materials for Coating Aluminum and Aluminum Alloys.”PAGE 33.3.1.2, line 7: Delete “IA…” and substitute “IB.”PAGE 43.3.1.2: Change paragraph number to “3.3.1.3.” In line 4, delete “IA” and substitute “IB.”PAGE 5Add: “3.4.2.2 Photosensitized (identification) nameplates. When type II anodic coatings are specified for use in photosensitized nameplates, oxalic acid anodizing may be used in lieu of sulfuric acid anodizing. If oxalic acid anodizing is used, the resultant coating shall meet the requirements of this specification for type II anodic coatings. If copy and background color are added to photosensitive nameplates, silver compounds or dyes shall be used. Unprocessed photosensitive aluminum shall be classified as class 1. Nameplates made from photosensitive aluminum shall be classified as class 2.”AMSC N/A 1 of 3 AREA MFFP DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited.PAGE 63.7.1.2c: Delete and substitute:“c. In addition to the requirements in a and b above, types I and IB test specimens that exhibit large areas of gross discoloration (dark grey areas) shall meet the following additional requirement. The total number and per panel number of pits used to verify that the requirements of a and b above are met shall be determined by adding the number of pits found with the unaided eye to the number of pits found in the areas of gross discoloration determined when examined at a magnification of 10X. This requirement does not apply to areas of slight discoloration or fading such as those areas that may result from chromate leaching during salt spray exposure.”PAGE 9TABLE II: Add “2/ III” to column 2, row 3, Applicable type I, IB, IC, II, IIB.Add the following footnote below the table “2/ Type III coatings shall be tested for corrosion resistance only when it is specified that the coating is sealed.”PAGE 104.3.3.2.3: Delete and substitute: “4.3.3.2.3 Test specimens for corrosion and light fastness resistance. Corrosion resistance shall be determined on undyed and sealed production parts or specimen panels (see 4.3.3.2). When light fastness testing is specified (see 6.2), it shallbe performed on dyed and sealed (class 2) production parts or specimen panels (see 4.3.3.2). When specimen panels are used, they shall have a width of not less than 3 inches, a length of not less than 10 inches, and a nominal thickness of not less than 0.032 inch.PAGE 136.1, line 2: Delete “yipvide” and substitute “provide.”6.1.1, line 7: Change “MIL-C-81706” to “MIL-DTL-81706.”PAGE 186.16, lines 2 and 4: Change “silicone” to “silicon.”PAGE 19Delete 6.23 and substitute:“6.23 Subject term (key word) listing.AnodizingChromatesChromic acidPhosphoric acidPotassium dichromateSodium dichromateSulfuric acidCustodians: Preparing activity:Army – MR Navy - ASNavy – AS (Project MFFP-0698) Air Force – 11Review activities:Army – AR, AV, AT, CR, CR4, MINavy – OS, SHAir Force – 70, 71, 99ÚÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄ¿ ³NOT MEASUREMENT³ ³ SENSITIVE ³ ÀÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÙ MIL-A-8625F10 September 1993 SUPERSEDINGMIL-A-8625E25 April 1988MILITARY SPECIFICATIONANODIC COATINGS, FOR ALUMINUM AND ALUMINUM ALLOYSThis specification is approved for use by all Departments and Agencies of the Department of Defense.1. SCOPE1.1 Scope. This specification covers the requirements for six types and two classes of electrolytically formed anodic coatings on aluminum and aluminum alloys for non-architectural applications (see 6.1).1.2 Classification. Anodic coating Types and Classes covered by this specification are as specified herein (see 6.2 and 6.21):1.2.1 TypesType I - Chromic acid anodizing, conventional coatings producedfrom chromic acid bath, (see 3.4.1)Type IB - Chromic acid anodizing, low voltage process, 22 +/- 2V,(see 3.4.1)Type IC - Non-chromic acid anodizing, for use as a non-chromatealternative for Type I and IB coatings (see 3.4.1 and 6.1.2) Type II - Sulfuric acid anodizing, conventional coatings producedfrom sulfuric acid bath, (see 3.4.2)Type IIB - Thin sulfuric acid anodizing, for use as a non-chromatealternative for Type I and IB coatings (see 3.4.2 and 6.1.2) Type III - Hard Anodic Coatings (see 3.4.3)1.2.2 Classes.Class 1 - Non-dyed (see 3.5.)Class 2 - Dyed (see 3.6.)ÚÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄ¿³Beneficial comments (recommendations, additions, deletions) and any ³³pertinent data which may be of use in improving this document should be ³³addressed to: Systems Engineering and Standardization Department (Code ³³53), Naval Air Engineering Center, Lakehurst, NJ 08733-5100, by using the ³³self-addressed Standardization Document Improvement Proposal (DD Form 1426)³³appearing at the end of this document or by letter. ³ÀÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÙ AMSC N/A AREA MFFP DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited.MIL-A-8625F2. APPLICABLE DOCUMENTS2.1 Government documents.2.1.1 Specifications, and standards. The following specifications and standards form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents shall be those listed in the issue of the Department of Defense Index of Specifications and Standards (DODISS) and supplement thereto, cited in the solicitation.SPECIFICATIONSMILITARYMIL-C-23377 - Primer Coating, Epoxy-Polyamide, Chemical and Solvent ResistantMIL-C-81706 - Chemical Conversion Materials for Coating Aluminumand Aluminum AlloysMIL-P-85582 - Primer Coatings: Epoxy, WaterborneFEDERALQQ-A-250/4 - Aluminum Alloy 2024, Plate and SheetSTANDARDSFEDERALFED-STD-141 - Paint, Varnish, Lacquer, and Related Materials:Method For Sampling and TestingFED-STD-151 - Metals; Test MethodsMILITARYMIL-STD-105 - Sampling Procedures and Tables for Inspectionby Attributes(Unless otherwise indicated, copies of federal and military specifications and standards are available from DODSSP-Customer Service, Standardization Documents Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA 19111-5094.)2.2 Non-Government publications. The following documents form a part of this document to the extent specified herein. Unless otherwise specified, the issues of the documents which are DOD adopted are those listed in the issue of the DODISS cited in the solicitation. Unless otherwise specified, the issues of documents not listed in the DODISS are the issues of the documents cited in the solicitation (see 6.2).AMERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM)ASTM B 117 - Method of Salt Spray (Fog) TestingANSI/ASTM B 137 - Weight of Coating on Anodically Coated Aluminum,Measurement ofASTM B 244 - Thickness of Anodic Coatings on Aluminum and ofRelated Products, Standard Practice for Operating 2ASTM D 2244 - Color Differences of Opaque Materials,Instrumental Evaluation ofASTM G 23 - Standard Practice for Operating Light ExposureApparatus (Carbon-Arc Type) With and Without Waterfor Exposure of Non-metallic MaterialsASTM G 26 - Operating Light-Exposure Apparatus (Xenon-ArcType) With and Without Water for Exposure ofNon-metallic Materials(Application for copies should be addressed to the American Society forTesting and Materials, 1916 Race Street, Philadelphia, PA 19103.)2.3 Order of precedence. In the event of a conflict between the text ofthis document and the references cited herein, the text of this documenttakes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained.3. REQUIREMENTS3.1 Materials. The materials used shall be such as to produce coatingswhich meet the requirements of this specification.3.1.1 Base metal. The base metal shall be sufficiently free from surface defects, caused by machining, cutting, scratching, polishing, buffing, roughening, bending, stretching, deforming, rolling, sandblasting, vaporblasting, etching, heat treatment condition, alloy chemistry imbalanceand inclusions, that will cause test panels or parts to fail any of the requirements of this specification. The base metal shall be subject to cleaning, etching, anodizing and sealing procedures as necessary to yield coatings meeting all requirements of this specification.3.2 Equipment and processes. The equipment and processes employed shallbe such as to produce coatings which meet the requirements of this specification. Unless otherwise specified in the contract, purchase order or applicable drawing (see 6.2), process operating conditions shall be at the option of the supplier.3.3 General.3.3.1 Anodizing of parts and assemblies.3.3.1.1 Anodizing of parts. Unless otherwise specified in the contract, purchase order or applicable drawing (see 6.2), parts shall be anodized after all heat treatment, machining, welding, forming and perforating have been completed.3.3.1.2 Anodizing of assemblies. Unless otherwise specified in the contract, purchase order or applicable drawing, anodic coatings shall not be appliedto assemblies which will entrap the electrolyte in joints or recesses (components shall be anodized separately prior to assembly). When anodizing of assemblies is authorized by the contract, purchase order or applicabledrawing, the processing method used shall not result in subsequent damage tothe assembly from electrolyte entrapment (Type I or IA coatings shall be used unless another coating Type is specified). Assemblies which containnon-aluminum parts such as steel, brass or organic substances, which would be attacked by pretreatment or anodizing solutions or would prevent uniform3.3.1.2 Anodizing of complex shapes. When anodizing complex shapes which will entrap the electrolyte in recesses, the processing method used shall not result in subsequent damage to the part from electrolyte entrapment (Type I or IA coatings shall be used unless another coating Type is specified).3.3.2 Handling and cleaning. Parts shall be so handled during all pretreatments, anodizing and post treatments that mechanical damage or contamination will be avoided. Parts shall be free of all foreign substances, oxides and soils, such as greases, oil, paint and welding flux. Parts shall have oxide and other interfering films removed by the use of proper cleaning procedures so as to be clean and have water break free surfaces. Abrasives containing iron, such as steel wool, iron oxide rouge and steel wire, which may become embedded in the metal and accelerate corrosion of aluminum and aluminum alloys, are prohibited as a means of mechanical cleaning, prior to anodizing. If special cleaning requirements are required they shall be specified in the contract or order (see 6.2).3.3.3 Reflective surfaces. When specified in the contract or purchase order (see 6.2), parts fabricated to produce a highly reflective surface shall be chemically or electrochemically brightened, prior to anodic coating (see 6.9). 3.3.4 Touch up (mechanical damage and contact marks). Unless otherwise specified (see 6.2), mechanically damaged areas from which the anodic coating has been removed without damage to the part may be touched up using chemical conversion materials approved on QPL-81706 for Class 1A coatings and the applicable method of application. Touch up shall apply only to inadvertent mechanical damage such as scratch marks. For Type III coatings, touch up shall only be allowed in areas which will not be subjected to abrasion (see 6.1.1). The mechanically damaged area(s) shall not exceed 5 percent of total anodized area of the item or touch up shall not be permitted. When specified in the contract or purchase order (see 6.2), contact marks shall be touched up using the above method required for mechanical damage.3.4 Coatings. Conventional anodic coatings as specified in the contract, purchase order or applicable drawings (see 6.2), shall be prepared by any process or operation to produce the specified coating on aluminum and aluminum alloys.3.4.1 Type I, IB and IC coatings. Type I and IB coatings shall be theresult of treating aluminum and aluminum alloys electrolytically in a bath containing chromic acid to produce a uniform anodic coating on the metal surface. Type IC coatings shall be the result of treating aluminum and aluminum alloys electrolytically in a bath containing mineral or mixed mineral/ organic acids (non-chromic acid) to produce a uniform anodic coating on the metal surface. Unless otherwise specified in the contract, purchase order or applicable drawing, Type I coatings shall not be applied to aluminum alloys with a nominal copper content in excess of 5.0 percent; nominal silicon contents in excess of 7.0 percent; or when the total allowable contents of nominal alloying elements exceed 7.5 percent. Heat treatable alloys which are to receive a Type I, IB or IC coating shall be in the required temper obtained by heat treatment, such as -T4, -T6, or T73 prior to anodizing.3.4.1.1 Type IC coatings. Type IC coatings provide a non-chromate alternative to Type I and IB coatings. Unless approved by the procuring activity, substitution of a Type IC coating where Type I or IB is specified shall be prohibited.3.4.2 Type II and IIB coatings. Type II and IIB coatings shall be the result of treating aluminum and aluminum alloys electrolytically in a bath containing sulfuric acid to produce a uniform anodic coating on the metal surface. Heat treatable alloys shall be in the required temper obtained by heat treatment, such as -T4, -T6, or T73, prior to anodizing.3.4.2.1 Type IIB coatings. Type IIB coatings provide a non-chromate alternative to Type I and IB coatings. Unless approved by the procuring activity, substitution of a Type IIB coating where Type I or IB is specified shall be prohibited.3.4.3 Type III coatings. Type III coatings shall be the result of treating aluminum and aluminum alloys electrolytically to produce a uniform anodic coating on the metal surface. Type III coatings shall be prepared by any process operation to produce a heavy dense coating of specified thickness on aluminum alloys (see 3.7.2.1). Unless otherwise specified in the contract, purchase order or applicable drawing, Type III coatings shall not be applied to aluminum alloys with a nominal copper content in excess of 5 percent or a nominal silicon content in excess of 8.0 percent. Alloys with a nominalsilicon content higher than 8.0 percent may be anodized subject to approval of the procuring activity. Heat treatable alloys shall be in a temper obtained by heat treatment, such as -T4, -T6 or T73, prior to anodizing.3.5 Class 1. When class 1 is specified in the contract or purchase order, (see 6.2), the anodic coating shall not be dyed or pigmented. Any natural coloration resulting from anodic treatment with the various alloy compositions shall not be considered coloration. The characteristic color imparted by the sealing process shall also be considered as non-dyed.3.6 Class 2. When class 2 is specified in the contract or purchase order, (see 6.2), the anodic coating shall be uniformly dyed or pigmented by exposure to a solution of a suitable type dye or stain. The color on wrought alloysshall be uniform. Cast alloys may exhibit dye bleed-out or lack of color (or color uniformity) associated with the inherent porosity of the casting. The dyes and pigments used shall not be damaging to the anodic coatings.3.6.1 Dye color. When dyed or pigmented coatings are required, the colorand color uniformity requirements shall be as specified by the contract, purchase order or applicable drawing (see 6.2).3.6.1.1 Casting alloys. Dyed casting alloys may show a slight lack of color uniformity. The degree of non-uniformity that is acceptable shall be established by the procuring activity (see 6.2).3.7 Detail requirements.3.7.1 Types I, IB, IC, II, and IIB coatings.3.7.1.1 Weight of coating. Prior to dyeing or sealing, Type I, IB, IC, II, and IIB coatings shall meet the coating weight requirements of Table I when tested in accordance with4.5.2 (see6.10.6).5TABLE I. Types I, IB, IC, II, and IIB unsealed anodic coating weights.ÚÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÂÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄ¿³ Coating Type ³ Coating Weight (mg/ftÀ2Ù) ³ÃÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÅÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄ´³ I and IB ³ 200 minimum ³ÃÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÅÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄ´³ IC [1] ³ 200 minimum - 700 maximum ³ÃÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÅÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄ´³ II ³ 1000 minimum ³ÃÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÅÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄ´³ IIB ³ 200 minimum - 1000 maximum ³ÀÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÁÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÙ[1] Coating weights over 700 mg/ftÀ2Ù may be used if specified inthe contract or purchase order (see 6.1.2 and 6.2).3.7.1.2 Corrosion resistance. After exposure to the salt spray test specified in4.5.3, specimens shall be visually examined to determine that all of the following conditions are met:a. Test specimens shall show no more than a total of 15 isolated pits(see 6.19), none larger than 0.031 inch in diameter, in a total of 150 square inches of test area grouped from five or more test pieces. Areas within 0.062 inch from identification markings, edges and electrodecontact marks remaining after processing shall be excluded.b. Test specimens shall show no more than 5 isolated pits, none larger than0.031 inch in diameter, in a total of 30 square inches from one or more test pieces. Areas within 0.062 inch from identification markings,edges and electrode contact marks remaining after processing shall beexcluded.c. In addition to the requirements in (a) and (b) above, Type I and IBtest specimens shall not exhibit patchy dark gray areas (spots, streaks, or marks).3.7.1.3 Light fastness resistance. Class 2, dyed anodic coatings, shallshow no more fading or discoloration than would be equivalent to a Delta (E) value of 3 when subjected to the light fastness resistance test (see 4.5.4), unless otherwise specified in the contract or purchase order (see 6.2). Light fastness resistance shall be determined only when specified in the contract, purchase order or applicable drawing (see 6.2).3.7.1.4 Paint adhesion. When tested in accordance with4.5.6, no intercoat separation shall occur between the paint system and the anodic coating or between the anodic coating and the base metal. Paint adhesion shall be determined only when specified in the contract, purchase order or applicable drawing (see6.2).3.7.2 Type III coatings.3.7.2.1 Thickness of coating. Unless otherwise specified in the contract, purchase order, or applicable drawing (see 6.2), the nominal thickness of the coating shall be 0.002 inch (2 mils) (see 6.16, 6.17 and 6.10 through 6.10.5). Unless otherwise specified, the thickness of the coating shall not vary by more than +/- 20 percent for coatings up to 0.002 inches thick (2 mils) when testedin accordance with 4.5.1. Coatings over 0.002 inches (2 mils) shall not vary3.7.2.1.1 Weight of coating. The coating weight may be determined in lieu of the coating thickness (see 3.7.2.1), at the option of the procuring activity. Unsealed Type III coatings shall have a minimum coating weight of 4320 milligrams per square foot for every 0.001 inch of coating when tested in accordance with4.5.2 (see6.2).3.7.2.2 Abrasion resistance. When tested in accordance with4.5.5, unsealed Type III coatings shall provide a hard abrasion resistant finish as specified herein (see6.17). The anodic coating shall have a maximum wear index of3.5mg/1000 cycles on aluminum alloys having a copper content of 2 percent or higher (see 6.13). The wear index for all other alloys shall not exceed 1.5mg/ 1000 cycles.3.8 Sealing.3.8.1 Types I, IB, IC, II, and IIB. All Types I, IB, IC, II and IIB anodic coatings shall be completely sealed, unless otherwise specified in the contract, purchase order or applicable drawing (see 6.2). They shall be sealed in accordance with 3.8.1.1 or 3.8.1.2, as applicable. If wetting agents are used they shall be of the non-ionic type.3.8.1.1 Class 1. When class 1 is specified, sealing shall be accomplished by immersion in a sealing medium such as a 5 percent aqueous solution of sodiumor potassium dichromate (pH 5.0 to 6.0) for 15 minutes at 90 deg. C to 100 deg.C (194 deg. F to 212 deg. F), in boiling deionized water, cobalt or nickel acetate, or other suitable chemical solutions (see 6.15).3.8.1.2 Class 2. When class 2 is specified, sealing shall be accomplished after dyeing by immersion in a sealing medium, such as a hot aqueous solution containing 0.5 percent nickel or cobalt acetate (pH 5.5 to 5.8), boiling deionized water, duplex sealing with hot aqueous solutions of nickel acetate and sodium dichromate (see 6.11), or other suitable chemical solutions.3.8.2 Type III. Type III coatings shall not be sealed where the main function of application is to obtain the maximum degree of abrasion or wear resistance. Where Type III coatings are used for exterior non-maintained applications requiring corrosion resistance but permitting reduced abrasion resistance, the contract or purchase order shall specify that sealing is required. Sealing for such Type III coatings shall be accomplished by immersion in a medium, such as boiling deionized water, in a hot aqueous 5 percent sodium dichromate solution, in a hot aqueous solution containing nickel or cobalt acetate or other suitable chemical solutions (see 6.2). When Type III coatings are provided unsealed, parts shall be thoroughly rinsed in cold, clean water and dried after anodizing.3.9 Dimensions of coated articles. Articles or parts shall comply with the dimensional requirements of the applicable drawings after application of the anodic coating (see 6.10.1). (For interference in close fits of parts or assemblies see 6.10.5).3.10 Toxicity. The coatings and electrical/chemical processes used to develop these anodic coatings shall have no adverse effect on the health of personnel when used for their intended purposes. Questions pertinent to this effectshall be referred by the contracting activity to the appropriate departmental medical service who will act as an advisor to the contracting agency.73.11 Painting/coating. Painting/coating operations shall be performed as soon as practical after the anodizing process on clean coatings. If parts require storage prior to painting/coating, they shall be stored in a manner that will avoid contamination. If the parts become contaminated, they shall be cleanedin a manner that will not be detrimental to the anodic coating or the basis metal, (see 6.3).3.12 Dyeing or coloring. Anodic coatings shall not be allowed to dry before dyeing or coloring. Items to be dyed or colored should be preferably coated by the Type II anodizing treatment (see 6.12). Dyed or colored coatings shall not be allowed to remain in rinse waters for more than 5 minutes before sealing.3.13 Workmanship. Except for touch up areas in accordance with 3.3.4 and as noted below, the applied anodic coating shall be continuous, smooth, adherent, uniform in appearance, free from powdery areas, loose films, breaks, scratches and other defects which will reduce the serviceability of anodized parts or assemblies. Differences in anodic coating appearance resulting from inherent base metal differences in a component such as the presence of welds, components containing cast and machined surfaces, and differences in grain size within a forging shall not be cause to reject the anodic coating unless otherwise specified in the contract or purchase order (see 6.2). Slight discolorationfrom dripping or rundown of the sealing solution from designed crevices in a component shall be allowed.3.13.1 Contact marks. The size and number of contact marks shall be at a minimum consistent with good practice (see 6.14). If a specific location for contact marks is desired, the location shall be specified on the contract or purchase order (see 6.2).4. QUALITY ASSURANCE PROVISIONS4.1 Responsibility for inspection. Unless otherwise specified in the contract or purchase order, the contractor is responsible for the performance of all inspection requirements (examinations and tests) as specified herein. Exceptas otherwise specified in the contract or purchase order, the contractor mayuse his own or any other facilities suitable for the performance of the inspection requirements specified herein, unless disapproved by the Government. The Government reserves the right to perform any of the inspections set forthin the specification where such inspections are deemed necessary to ensure supplies and services conform to prescribed requirements.4.1.1 Responsibility for compliance. All items must meet all requirements of Section 3. The inspection set forth in this specification shall become a part of the contractor's overall inspection system or quality program. The absence of any inspection requirements in the specification shall not relieve the contractor of the responsibility of ensuring that all products or supplies submitted to the Government for acceptance comply with all requirements of the contract. Sampling inspection, as part of manufacturing operations, is an acceptable practice to ascertain conformance to requirements, however, thisdoes not authorize submission of known defective material, either indicated or actual, nor does it commit the Government to acceptance of defective material. 4.2 Classification of inspection. The Inspection requirements specifiedherein are classified as follows:8。
NOT MEASUREMENTSENSITIVEMIL-A-8625FAMENDMENT 115 September 2003MILITARY SPECIFICATIONANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS This amendment forms a part of MIL-A-8625F, dated 10 September 1993, and is approved for use by all Departments and Agencies of the Department of Defense.PAGE 22.1.1, under SPECIFICATIONS, MILITARY: Delete “MIL-C-81706 – Chemical Conversion Materials for Coating Aluminum and Aluminum Alloys.”PAGE 33.3.1.2, line 7: Delete “IA…” and substitute “IB.”PAGE 43.3.1.2: Change paragraph number to “3.3.1.3.” In line 4, delete “IA” and substitute “IB.”PAGE 5Add: “3.4.2.2 Photosensitized (identification) nameplates. When type II anodic coatings are specified for use in photosensitized nameplates, oxalic acid anodizing may be used in lieu of sulfuric acid anodizing. If oxalic acid anodizing is used, the resultant coating shall meet the requirements of this specification for type II anodic coatings. If copy and background color are added to photosensitive nameplates, silver compounds or dyes shall be used. Unprocessed photosensitive aluminum shall be classified as class 1. Nameplates made from photosensitive aluminum shall be classified as class 2.”AMSC N/A 1 of 3 AREA MFFP DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited.PAGE 63.7.1.2c: Delete and substitute:“c. In addition to the requirements in a and b above, types I and IB test specimens that exhibit large areas of gross discoloration (dark grey areas) shall meet the following additional requirement. The total number and per panel number of pits used to verify that the requirements of a and b above are met shall be determined by adding the number of pits found with the unaided eye to the number of pits found in the areas of gross discoloration determined when examined at a magnification of 10X. This requirement does not apply to areas of slight discoloration or fading such as those areas that may result from chromate leaching during salt spray exposure.”PAGE 9TABLE II: Add “2/ III” to column 2, row 3, Applicable type I, IB, IC, II, IIB.Add the following footnote below the table “2/ Type III coatings shall be tested for corrosion resistance only when it is specified that the coating is sealed.”PAGE 104.3.3.2.3: Delete and substitute: “4.3.3.2.3 Test specimens for corrosion and light fastness resistance. Corrosion resistance shall be determined on undyed and sealed production parts or specimen panels (see 4.3.3.2). When light fastness testing is specified (see 6.2), it shallbe performed on dyed and sealed (class 2) production parts or specimen panels (see 4.3.3.2). When specimen panels are used, they shall have a width of not less than 3 inches, a length of not less than 10 inches, and a nominal thickness of not less than 0.032 inch.PAGE 136.1, line 2: Delete “yipvide” and substitute “provide.”6.1.1, line 7: Change “MIL-C-81706” to “MIL-DTL-81706.”PAGE 186.16, lines 2 and 4: Change “silicone” to “silicon.”PAGE 19Delete 6.23 and substitute:“6.23 Subject term (key word) listing.AnodizingChromatesChromic acidPhosphoric acidPotassium dichromateSodium dichromateSulfuric acidCustodians: Preparing activity:Army – MR Navy - ASNavy – AS (Project MFFP-0698) Air Force – 11Review activities:Army – AR, AV, AT, CR, CR4, MINavy – OS, SHAir Force – 70, 71, 99。
美军标简介United States Military Standard2010-06—11 15：54主要分类:Acronym Type Definition [1]MIL—HDBK DefenseHandbook A guidance document containing standard procedural， technical，engineering， or design information about the materiel, processes， practices， and methods covered by the DSP。
MIL—STD-962 covers the content and format for defense handbooks.MIL-SPEC DefenseSpecification A document that describes the essential technical requirements for purchased material that is military unique or substantially modified commercial items。
MIL-STD-961 covers the content and format for defense specifications.MIL—STD DefenseStandard A document that establishes uniform engineering and technical requirements for military—unique or substantially modified commercial processes, procedures，practices， and methods。
There are five types of defense standards：interface standards, design criteria standards，manufacturing process standards，standard practices， and test method standards。
铝阳极氧化MIL-A-8625F标准中文版时间: 2011-4-19 14:49:28/ 作者: 青岛精良机械有限公司铝阳极氧化MIL-A-8625F标准中文版美国军事标准铝和铝合金的阳极氧化膜此标准由由美国国防部所有部门和科室批准使用1.范围1.1范围本标准包括非建筑用途的铝和铝合金的6类和2级电解生成的阳极氧化膜的要求（见6.1）。
1.2分类本标准所列阳极氧化膜的类别和级别如下：1.2.1分类Ⅰ类- 铬酸阳极氧化，在铬酸槽生成的常规氧化膜（见3.4.1）ⅠB类- 铬酸阳极氧化，低电压工艺，22±2V（见3.4.1）ⅠC类- 非铬酸阳极氧化，应用非铬酸的配方生成的Ⅰ和ⅠB类氧化膜（见3.4.1和6.1.2）Ⅱ类- 硫酸阳极氧化，在硫酸槽生成的常规氧化膜（见3.4.2）ⅡB类- 硫酸阳极氧化薄膜，应用非铬酸的配方生成的Ⅰ和ⅠB类氧化膜（见3.4.1和6.1.2）Ⅲ类- 硬质阳极氧化膜（见3.4.3）1.2.2级别1级- 不染色（见3.5）2级- 染色（见3.6）2.适用文件2.1政府文件2.1.1规范和标准下面的规范和标准构成本标准的组成部分。
（此处有删节）规范军事规范MIL-P-23377 耐化学和溶剂腐蚀的环氧聚酰胺涂层，MIL-C-81706 铝和铝合金的化学转化膜MIL-P-85582 水性环氧树脂涂层联邦规范QQ-A-250/4 2024铝合金的板和薄板标准联邦标准FED-STD-141 油漆，清漆，硝基漆和相关材料：取样和测试方法。
FED-STD-151 金属：测试方法军事标准MIL-STD-105 取样程序和质量检查表2.2非政府出版物下面的规范和标准构成本标准的组成部分。
（此处有删节）美国试验和材料学会(ASTM)ASTM B 117 盐雾试验方法ANSI/ASTM B 137 铝和铝合金的阳极氧化膜的重量测试ASTM B 224 利用涡流仪测试铝氧化膜厚度，以及其它非磁性材料上的非导电层的厚度 ASTM D 822 测定油漆，清漆，硝基漆和其它产品的曝光和曝水仪（碳-电弧型）的标准使用方法ASTM D 2244 不透明材料色差的仪器测试ASTM G 23 有水和无水的非金属材料曝光测试的曝光仪（碳-电弧型）的标准使用方法 ASTM G 26 有水和无水的非金属材料曝光测试的曝光仪（氙-电弧型）的标准使用方法2.3优先程序在本标准和所引用的参考文件有矛盾时，本标准具有优先权，但是本标准不能超越现行的相关法律和法规。
MIL-A-8625F 鋁和鋁合金陽極化塗層軍用規范1.適應范圍1.1 范圍本規范說明了非建築性應用的鋁和鋁合金電解陽極化塗層的6種類型和2個等級的要求。
1.2 分類本規范所規定的陽極化塗層類型和等級如以下所述（見第6.2和6.21項）：類型類型I：經鉻酸溶液處理所形成的轉化塗層的鉻酸陽極化處理（見3.4.1）類型IB：低電壓（22±2V），鉻酸陽極化處理（見3.4.1）類型IC：非鉻酸陽極化處理，作為類型I和IB塗層的另一種選擇（見3.4.1和6.1.2）類型II：硫磺酸陽極化處理，經硫磺酸溶液生產而成的轉化塗層。
類型IIB：稀硫磺酸陽極化處理，用為類型I和IB塗層的另一種選擇（見3.4.2和6.1.2）類型III：硬質陽極化塗層（見第3.4.3項）等級等級1：不染色（見第3.5項）等級2：染色（見第3.6項）2.應用文件2.1 官方文件2.1.1 規范和標準：規范：軍用MIL-P-23377：底部塗層抗環氧聚酰胺化學物和溶劑特性MIL-C-81706：鋁和鋁合金化學轉化材料MIL-P-85582：環氧，水溶性底部塗層聯邦QQ-A-250/4：鋁合金2024板材標準：聯邦FED-STD-141：塗料、清漆、漆及相關材料的抽樣和測試方法FED-STD-151：金屬測試方法軍用MIL-STD-105：抽樣程序和特性檢查表（除另有說明以外，聯邦、軍用規范及標準的復制版均由美国宾西法尼亚州，费城，4D棟，700Robbin街DODSSP客服部提供標準化文件清單）。
2.2 非官方發行文件以下文件在一定的程度上構成此份文件的一部份。
除另有規定以外，DOD採用的發行文件都是DODISS申請中所列的發行文件（見6.2）美国材料实验协会（ASTM）：ASTM B 117 ：鹽霧測試ANSI/ASTM B 137：鋁陽極化塗層的重量測定ASTM B 244：鋁和其它帶有涡电流儀器的非磁性底材上電導性塗層的陽極化塗層的厚度測量。
