MIL-STD-6866 Base Document:1985
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
INSPECTION, LIQUID PENETRANT
22-11-1996
1 Scope
1.1 Purpose
1.2 Application
1.3 Classification
1.3.1 Penetrant systems
1.3.2 Developers
1.3.3 Solvent removers
2 Referenced documents
2.1 Government documents
2.1.1 Specifications and standards
2.2 Other publications
2.3 Order of precedence
3 Definitions
3.1 Background
3.2 Black light
3.3 Black light filter
3.4 Bleedout
3.5 Component
3.6 Contaminant
3.7 Contracting agency
3.8 Dark adaptation
3.9 Defect
3.10 Developer
3.11 Developer, dry
3.12 Developer, nonaqueous
3.13 Developer, wet (aqueous) soluble
3.14 Developer, wet (aqueous) suspendible
3.15 Drain time
3.16 Drying oven
3.17 Dwell time
3.18 Emulsifier
3.19 Emulsifier, hydrophilic
3.20 Emulsifier, lipophilic
3.21 Etching
3.22 Evaluation
3.23 Fluorescence
3.24 Government procurement agency
3.25 Hydro-air nozzle
3.26 Indication
3.27 In-process
3.28 In-service
3.29 Inspection
3.30 Interpretation
3.31 Linear indication
3.32 NDT facility
3.33 Penetrant
3.34 Penetrant, post emulsifiable
3.35 Penetrant, solvent removable
3.36 Penetrant, water-washable
3.37 Postcleaning
3.38 Precleaning
3.39 Prime contractor
3.40 Relevant indication
3.41 Reprocess
3.42 Solvent remover
4 General requirements
4.1 Responsibility for inspection
4.2 Specifying
4.3 Personnel qualification
4.4 Materials
4.4.1 Qualified materials
4.4.2 LOX compatible materials
4.5 Equipment and facilities
4.5.1 Processing
4.5.2 Viewing
4.6 Written procedure
4.7 Inspection sequence
4.7.1 Surface treatment
4.7.2 Surface coatings
4.8 Materials and process limitations
4.9 Records
5 Specific requirements
5.1 Surface preparation
5.1.1 Solvent cleaning
5.1.2 Chemical cleaning
5.1.3 Mechanical cleaning
5.1.4 Etching
5.2 Penetrant application and dwell
5.3 Penetrant removal
5.3.1 Method A process
5.3.1.1 Manual spray
5.3.1.2 Automated spray
5.3.1.3 Manual wipe
5.3.2 Method B process
5.3.2.1 Lipophilic emulsifier application and dwell
5.3.2.2 Rinsing
5.3.3 Method C process
5.3.4 Method D process
5.3.4.1 Prerinse
5.3.4.2 Hydrophilic emulsifier application and dwell
5.3.4.3 Postrinse
5.4 Drying
5.4.1 Sequence
5.4.2 Drying parameters
5.5 Developing
5.5.1 Dry developers
5.5.2 Nonaqueous developers
5.5.3 Aqueous developers, soluble and suspendible
5.6 Inspection
5.6.1 Type I processes
5.6.2 Type II processes
5.6.3 Evaluation
5.6.3.1 Mechanical evaluation
5.7 Postcleaning
5.8 Quality assurance provisions
5.8.1 Black lights
5.8.2 White light
5.8.3 System performance
5.8.3.1 Known defect standards
5.8.4 Materials
5.8.4.1 Penetrants
5.8.4.1.1 Brightness
5.8.4.1.2 Water content (Method A penetrants only)
5.8.4.1.3 Removability (Method A penetrants only)
5.8.4.1.4 Sensitivity
5.8.4.2 Emulsifiers
5.8.4.2.1 Removability
5.8.4.2.2 Water content (lipophilic emulsifier)
5.8.4.2.3 Concentration (hydrophilic emulsifier)
5.8.4.3 Developers
5.8.4.3.1 Dry developer
5.8.4.3.2 Aqueous developer (soluble and suspended)
5.8.5 Inspection area
5.8.6 Operating pressures/temperatures
5.9 Marking
5.9.1 Impression stamping
5.9.2 Etching
5.9.3 Dyeing
5.9.4 Other identification
5.9.5 Symbols
6 Notes
6.1 Intended use
6.2 Nonmetallic components
Describes liquid penetrant inspection of non-porous, non-metal and metal components. Coverage includes referenced documents, definitions, materials, surface treatment, personnel qualifications, processing, surface treatment, records, inspection sequence, solvent cleaning, mechanical cleaning, dry developers, black lights, white lights, penetrant removal, and rinsing.
Committee |
AREA NDTI
|
DevelopmentNote |
SUPERSEDED BY ASTM E 1417-
|
DocumentType |
Standard
|
Pages |
29
|
PublisherName |
US Military Specs/Standards/Handbooks
|
Status |
Superseded
|
Supersedes |
MIL-STD-2175 Revision A:1993 | CASTING, CLASSIFICATION AND INSPECTION OF |
MIL-A-83577 Revision B:1988 | ASSEMBLIES, MOVING MECHANICAL, FOR SPACE AND LAUNCH VEHICLES, GENERAL SPECIFICATION FOR |
SAE MAM4131B | Aluminum Alloy, Die and Hand Forgings 5.6zn 2.5mg 1.6cu 0.23cr Solution Heat Treated and Aged |
MIL-C-47269 Revision A:1992 | CASTINGS, INSPECTION OF (FOR GUIDED MISSILE AND ROCKET MATERIAL) |
NASA MSFC SPEC 560 : 1988 | THE FUSION WELDING OF STEEL, CORROSION AND HEAT RESISTANT ALLOYS |
MIL-B-85667 Revision A:1991 | BOLT, SLEEVE, STRAIGHT SHANK, PROTRUDING AND FLUSH HEAD GENERAL SPECIFICATION FOR |
MIL-P-87988 Base Document:1989 | PIN-RIVET, THREADED WITH HEX SOCKET |
SAE MAM5401B | Nickel Alloy, Corrosion and Heat Resistant, Investment Castings 62ni 21.5cr 9.0mo 3.6cb Vacuum Melted, Vacuum Cast as Cast |
MIL-B-87114 Revision A:1978 | BOLTS, RECESS DRIVE, GENERAL SPECIFICATION FOR |
DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-S-21472 Revision C:1988 | SCREW, SHOULDER, HEXAGON SOCKET-HEAD AND SLOTTED-HEAD GENERAL SPECIFICATION FOR |
MIL-S-45909 Revision C:1989 | STUD, LOCKED IN - RING LOCKED SERRATED |
MIL-B-23964 Revision D:1981 | BOLT, SELF-RETAINING, POSITIVE LOCKING |
DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-B-85604 Revision A:1988 | BOLT, NICKEL ALLOY 718, TENSION, HIGH STRENGTH, (125 KSI FSU & 220 KSI FTU) HIGH TEMPERATURE, SPLINE DRIVE, GENERAL SPECIFICATION FOR |
DEFSTAN 00-970(PT0)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-N-85730 Base Document:1988 | NUT, SELF-LOCKING, SPLINE DRIVE, ASSEMBLED WASHER, NICKEL ALLOY 718, 220 KSI FTU, 900 DEGREES F, GENERAL SPECIFICATION FOR |
DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-S-45915 Revision A:1967 | STUD, LOCKED IN - KEY LOCKED - GENERAL SPECIFICATION FOR |
MIL-N-7873 Revision B:1994 | NUT, SELF-LOCKING 1,200 DEG F |
MIL-P-71012 Revision A:1994 | PISTOL, SEMIAUTOMATIC, COMPACT, 9MM: M11 |
MIL-F-60445 Revision C:1991 | FIN AND NOZZLE ASSEMBLY, FOR ROCKET MOTOR 2.75 INCH MARK 4 AND MARK 40 PARTS FOR |
SAE AMS 2680 : 2010 | ELECTRON-BEAM WELDING, FOR FATIGUE CRITICAL APPLICATIONS |
MIL-B-85598 Base Document:1988 | BEARINGS, ELASTOMERIC GENERAL SPECIFICATION FOR |
MIL-STD-1261 Revision C:1988 | ARC WELDING PROCEDURES FOR CONSTRUCTIONAL STEELS |
SAE MA2060A | Fittings, Welded, Hydraulic, Titanium and Corrosion Resistant Steel, 21 000 kPa, Metric |
NEMA XR 14-1990 (R1995, R2000) | RECOMMENDED PRACTICES FOR LOAD-BEARING MECHANICAL ASSEMBLIES USED IN DIAGNOSTIC IMAGING |
SAE AMS5340E | Steel, Corrosion Resistant, Investment Castings 14Cr - 4.25Ni - 2.25Mo - 0.25Cb - 3.25Cu Homogenization and Solution Heat Treated |
SAE AMSF7190B | Forging, Steel, For Aircraft/Aerospace Equipment and Special Ordnance Applications |
NASA KSC SPEC Z 0005 : 1995 | BRAZING - STEEL, COPPER, ALUMINIUM, NICKEL, AND MAGNESIUM ALLOYS, SPECIFICATION FOR |
MIL-I-45914 Revision A:1991 | INSERT, SCREW THREAD - LOCKED IN, KEY LOCKED |
NASA MSFC SPEC 504 : 1990 | WELDING, ALUMINIUM ALLOYS |
MIL-S-58112 Base Document:1989 | SLING, MULTI LEG, HELICOPTER, EXTERNAL CARGO |
FF-N-836 Revision E:1994 | Nut: Square, Hexagon, Cap, Slotted, Castle, Knurled, Welding and Single Ball Seat |
SAE AS7100/1B | National Aerospace and Defense Contractors Accreditation Program (NADCAP) Survey Checklists for the NDT Suppliers Accreditation Program |
MIL-F-18280 Revision F:1995 | FITTING, FLARELESS TUBE, FLUID CONNECTION |
MIL-A-11356 Revision F:1987 | ARMOR, STEEL, CAST, HOMOGENEOUS, COMBAT-VEHICLE TYPE (1/4 TO 8 INCHES, INCLUSIVE) |
MIL-C-14613 Revision A:1972 | CHARGER, BOLT, CALIBER .50 BROWNING MACHINE GUN, M10 |
MIL-STD-1891 Base Document:1992 | BOLTS AND SCREWS, INSPECTION OF |
NAVSEA T9074 AS GIB 010/271 : 0 | REQUIREMENTS FOR NONDESTRUCTIVE TESTING METHODS |
MIL-N-85729 Base Document:1988 | NUT, SELF-LOCKING, A-286, 160 KSI FTU, 450 DEGREES F, GENERAL SPECIFICATION FOR |
SAE AMST81915B | Titanium and Titanium-Alloy Castings, Investment |
SAE AIR4728 | References, Spacecraft and Spacecraft Servicing, Fluid System Components (Abbreviations, Acronyms, Definitions, Applicable Documents and Environmental Conditions) |
MIL A 5503 : E | ACTUATOR, AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
MIL-G-63343 Base Document:1980 | GRENADE XM74, HEMISPHERES FOR |
SAE AS4488 | Tubular Assemblies, Fusion Welded, Inspection Processes and Acceptance Standards For |
MIL-F-7190 Revision B:1985 | FORGING, STEEL, FOR AIRCRAFT AND AEROSPACE EQUIPMENT AND SPECIAL ORDNANCE APPLICATIONS |
NASA STD 6002 : 2008 | APPLYING DATA MATRIX IDENTIFICATION SYMBOLS ON AEROSPACE PARTS |
MIL-S-70335 Revision A:1990 | SCREW THREADS, INTERNAL COLD FORMED, GENERAL SPECIFICATION FOR |
MIL-W-5013 Revision L:1991 | WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-I-25135 Revision E:1984 | INSPECTION MATERIALS, PENETRANTS |
MIL-STD-40002 Base Document:1991 | HEAT TREATMENT CODING SYSTEM, GENERAL |
SAE AS13572A | Springs, Helical, Compression and Extension |
SAE AMSSTD2175A | Castings, Classification and Inspection of |
PREN 6052 : 200P1 | AEROSPACE SERIES - RIVETS - COLLAR - SYSTEM IN ALUMINIUM ALLOY SHEAR TYPE INCH SERIES - TECHNICAL SPECIFICATION |
MIL-STD-410 Revision E:1991 | NONDESTRUCTIVE TESTING PERSONNEL QUALIFICATION AND CERTIFICATION (EDDY CURRENT, LIQUID PENETRANT, MAGNETIC PARTICLE, RADIOGRAPHIC AND ULTRASONIC) |
MIL-STD-45662 Revision A:1988 | CALIBRATION SYSTEMS REQUIREMENTS |
MIL-STD-792 Revision F:2006 | IDENTIFICATION MARKING REQUIREMENTS FOR SPECIAL PURPOSE COMPONENTS |
MIL-P-47158 Base Document:1974 | PENETRANT INSPECTION, SOUNDNESS REQUIREMENTS FOR MATERIALS, PARTS AND WELDMENTS |
ASTM D 2512 : 2017 | Standard Test Method for Compatibility of Materials with Liquid Oxygen (Impact Sensitivity Threshold and Pass-Fail Techniques) (Withdrawn 2023) |
MIL-I-25135 Revision E:1984 | INSPECTION MATERIALS, PENETRANTS |
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