BS EN 2133:2010
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Aerospace series. Cadmium plating of steels with specified tensile strength ≤ 1450 MPa, copper, copper alloys and nickel alloys
Available format(s)
Hardcopy , PDF
Superseded date
23-12-2020
Language(s)
English
Published date
28-02-2011
Publisher
Foreword
1 Scope
2 Normative references
3 Purpose of process
4 Limitations of process use
5 Terms and definitions
6 Coating thickness
7 Symbols
8 Information for the processor
9 Condition of parts prior to the treatment
10 Process schedule
11 Post-treatment
12 Removal of the plating
13 Required characteristics
14 Test methods
15 Quality assurance
16 Designation
Defines the electrolytic cadmium plating of parts in steel of tensile strength R[m] (max.) <= 1450 MPa, copper, copper alloys and nickel alloys, whose temperature in service does not exceed 235 degrees C.
| Committee |
ACE/65
|
| DevelopmentNote |
Supersedes 92/71701 DC. (09/2005) Supersedes 09/30207944 DC. (02/2011)
|
| DocumentType |
Standard
|
| Pages |
14
|
| PublisherName |
British Standards Institution
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
This European standard specifies the electrolytic cadmium plating of parts in steel of tensile strength Rm (max.) ≤ 1 450 MPa, copper, copper alloys and nickel alloys, whose temperature in service does not exceed 235 °C.
| Standards | Relationship |
| ONORM EN 2133 : 2011 | Identical |
| NEN EN 2133 : 2010 | Identical |
| EN 2133:2010 | Identical |
| I.S. EN 2133:2010 | Identical |
| NBN EN 2133 : 2010 | Identical |
| UNI EN 2133 : 2011 | Identical |
| UNE-EN 2133:1998 | Identical |
| NF EN 2133 : 2012 | Identical |
| DIN EN 2133:2011-05 | Identical |
| NS EN 2133 : 2010 | Identical |
| BS 6SP 4(2000) : 2000 | AEROSPACE SERIES - PINS HEADED, PLAIN SHANK, DRILLED, STEEL ALLOY AND CORROSION RESISTING STEEL WITH A STRENGTH CLASS 880 MPA |
| BS 2A173(1962) : 1962 | SPECIFICATION FOR 100 DEGREES COUNTERSUNK HEAD STEEL BOLTS (UNIFIED THREADS), CADMIUM PLATED, FOR AIRCRAFT |
| BS SP126 & SP127(1959) : 1959 | WASHERS FOR UNIFIED HEXAGONS FOR AIRCRAFT (PRIMARILY FOR FACING PURPOSES) |
| BS SP122-125(1958) : 1958 | WASHERS FOR UNIFIED HEXAGONS FOR AIRCRAFT (PRIMARILY FOR PACKING PURPOSES) |
| BS EN 2364:1989 | Specification for pins, shear headed, close tolerance |
| 11/30252412 DC : 0 | BS 4A 116 - STEEL PAN HEAD BOLTS (UNIFIED THREADS) (CADMIUM PLATED) FOR AIRCRAFT |
| BS SP 41-46(1951) : 1951 | SPECIFICATIONS FOR TAB WASHERS FOR B.A. AND B.S.W. HEXAGONS FOR AIRCRAFT |
| BS SP134-SP138(1968) : 1968 | AEROSPACE SERIES - SPECIFICATION FOR COPPER BERYLLIUM CRINKLE WASHERS |
| SBAC TS 120 : 6 | AGS2000 SERIES STIFFNUTS (INCLUDING CLINCH NUTS) BA & BSF THREADS FOR AIRCRAFT |
| 15/30329889 DC : 0 | BS A 266 TO 271 - BOLT, 100 DEGREES COUNTERSUNK HEAD, HI-TORQUE SPEED DRIVE RECESS, UNJF THREAD, SPLIT PIN HOLE OPTION, TITANIUM ALLOY, VARIOUS FINISHES, CLASSIFICATION: 80 TF/IN[2] (1100 MPA) AT TA/+315 DEGREES C |
| BS 4A 116:2012 | Steel pan head bolts (Unified threads), cadmium plated, for aircraft |
| BS 2SP91-92(1973) : 1973 | SPECIFICATION FOR CARBON STEEL WORM DRIVE CLAMPS FOR AIRCRAFT |
| BS 3SP 1:2013 | Specification. Shackles, carbon steel, cadmium plated for aircraft |
| BS SP22-27(1950) : 1950 | SPECIFICATION FOR BA WASHERS - FOR AIRCRAFT PURPOSES (PRIMARILY FOR FOR INSTRUMENT USE |
| 13/30274750 DC : 0 | BS 2A 204 ETC+A3 - SPECIFICATIONS FOR MACHINE SCREWS AND NUTS (UNIFIED THREADS) BELOW 1/4 INCH FOR AERONAUTICAL PURPOSES |
| 12/30256512 DC : 0 | BS SP 41-46+A5 - SPECIFICATIONS FOR TAB WASHERS FOR B.A. AND B.S.W. HEXAGONS FOR AIRCRAFT |
| 12/30266655 DC : DRAFT JULY 2012 | BS SP 139-140 A2 - SPECIFICATION FOR CORROSION-RESISTING STEEL CRINKLE WASHERS |
| BS 2SP81&2SP82(1973) : 1973 | SPECIFICATION FOR SNAP HEAD HIGH NICKEL-COPPER ALLOY RIVETS |
| BS 2A 266 to 2A 271:2016+A1:2019 | Aerospace Series. Bolt, 100° Countersunk head, Hi-Torque speed drive recess, close tolerance shank, UNJF thread, split pin hole option, titanium alloy, various finishes. Classification: R<sub>m</sub> 1100–1250 MPa (160 000–180 000 lbf/in<sup>2</sup>) at Ambient Temperature | +315 °C |
| BS 2SP87&2SP88(1973) : 1973 | AEROSPACE SERIES - 100 DEGREES COUNTERSUNK HEAD HIGH NICKEL-COPPER ALLOY RIVETS |
| BS 4A102(2002) : 2002 | AEROSPACE SERIES - SPECIFICATION FOR STEEL BOLTS (UNIFIED HEXAGONS AND UNIFIED THREADS) FOR AIRCRAFT |
| 15/30281806 DC : 0 | BS A 401 TO A 420 - AEROSPACE SERIES - SPECIFICATION FOR SCREWS, PAN AND 100 DEGREES COUNTERSUNK HEAD, HEXALOBULAR DRIVE RECESS (UNIFIED THREADS BELOW 1/4 INCH), VARIOUS MATERIALS |
| BS EN 2498:1990 | Specification for rod ends, adjustable self-aligning plain bearing, with self-lubricating liner and threaded shank. Dimensions and loads |
| 12/30264058 DC : DRAFT JULY 2012 | BS 4A 113 A1 - SPECIFICATION FOR CADMIUM-PLATED, MUSHROOM-HEADED, UNIFIED-THREAD, SLOTTED DRIVE, BOLTS |
| BS SP139 & SP140(1969) : 1969 | AEROSPACE SERIES - SPECIFICATION FOR CORROSION-RESISTING STEEL CRINKLE WASHERS |
| 12/30266661 DC : DRAFT JULY 2012 | BS SP 134-138 AMD1 - SPECIFICATION FOR COPPER BERYLLIUM CRINKLE WASHERS |
| BS SP10&11(1949) : 1949 | SPECIFICATION FOR WASHERS FOR AIRCRAFT PURPOSES (PRIMARILY FOR FACING PURPOSES) |
| BS 4A113(1999) : 1999 | AEROSPACE SERIES - SPECIFICATION FOR CADMIUM-PLATED, MUSHROOM-HEADED, UNIFIED-THREAD, SLOTTED DRIVE BOLTS |
| 11/30254199 DC : 0 | BS 3 SP 1 - SPECIFICATION - CARBON STEEL SHACKLES, CADMIUM PLATED |
| BS 2A 260-2A 265:2010 | Specification for pan and 100° countersunk slotted head screws with ISO metric screw threads |
| 12/30256515 DC : 0 | BS SP 107-112+A5 - SPECIFICATIONS FOR TAB WASHERS FOR UNIFIED HEXAGONS FOR AIRCRAFT |
| BS SP107-112(1954) : 1954 | SPECIFICATIONS FOR TAB WASHERS FOR UNIFIED HEXAGONS FOR AIRCRAFT |
| BS A 401-420:2015 | Specification for screws, pan and 100° countersunk head, hexalobular drive recess (unified threads below ¼ inch) in various materials |
| BS EN 2587:1990 | Specification for rod ends, adjustable double fork and threaded shank. Dimensions and loads |
| BS EN 2586:1991 | Specification for washers, lock for flight control rods. Dimensions |
| BS EN 2790:1991 | Rod ends, adjustable, self-aligning plain bearing with self-lubricating liner and threaded shank with engagement: 1.5 thread. Dimensions and loads |
| BS EN 2515:1990 | Specification for rod ends, adjustable single fork and threaded shank. Dimensions and loads |
| BS EN 2791:1991 | Rod ends, adjustable, single fork and threaded shank with engagement: 1.5 thread diameter. Dimensions and loads |
| 11/30251779 DC : 0 | BS 6SP 4:2000+A3 - PINS HEADED, PLAIN SHANK, DRILLED, STEEL ALLOY AND CORROSION RESISTING STEEL WITH A STRENGTH CLASS 880/1080 MPA |
| 12/30264056 DC : DRAFT JULY 2012 | BS 4A 102 A2 - SPECIFICATION FOR STEEL BOLTS (UNIFIED HEXAGONS AND UNIFIED THREADS) FOR AIRCRAFT |
| 10/30234053 DC : 0 | BS A 275-A 276 + A2 - HEXAGON SELF-LOCKING NUTS WITH NON-METALLIC LOCKING INSERTS - METRIC SERIES |
| BS 3A125 TO 3A[...](1981) : 1981 | AEROSPACE SERIES - SPECIFICATION FOR STIFFNUTS (UNIFIED THREADS) FOR AIRCRAFT |
| BS SP13, 14, 15 & 16(1949) : 1949 | SPECIFICATION FOR WASHERS FOR AIRCRAFT PURPOSES - (PRIMARILY FOR PACKING PURPOSES) |
| BS A275,A276,A277,A278,A279,A280(1981) : 1981 | AEROSPACE SERIES - SPECIFICATION FOR HEXAGON SELF-LOCKING NUTS WITH NON-METALLIC LOCKING INSERTS - METRIC SERIES |
| BS EN 2792:1991 | Rod ends, adjustable, double fork and threaded shank with engagement: 1.5 thread diameter. Dimensions and loads |
| EN 9100:2009 | Quality Management Systems - Requirements for Aviation, Space and Defense Organizations |
| EN 2832:1993 | Aerospace series - Hydrogen embrittlement of steels - Notched specimen test |
| ISO 2082:2017 | Metallic and other inorganic coatings — Electroplated coatings of cadmium with supplementary treatments on iron or steel |
| EN ISO 3497 : 2000 | METALLIC COATINGS - MEASUREMENTS OF COATING THICKNESS - X-RAY SPECTROMETRIC METHODS |
| ISO 1463:2003 | Metallic and oxide coatings Measurement of coating thickness Microscopical method |
| EN ISO 9227:2017 | Corrosion tests in artificial atmospheres - Salt spray tests (ISO 9227:2017) |
| EN ISO 2082:2017 | Metallic and other inorganic coatings - Electroplated coatings of cadmium with supplementary treatments on iron or steel (ISO 2082:2017) |
| ISO 2819:1980 | Metallic coatings on metallic substrates — Electrodeposited and chemically deposited coatings — Review of methods available for testing adhesion |
| ISO 3497:2000 | Metallic coatings Measurement of coating thickness X-ray spectrometric methods |
| ISO 4520:1981 | Chromate conversion coatings on electroplated zinc and cadmium coatings |
| ISO 2178:2016 | Non-magnetic coatings on magnetic substrates Measurement of coating thickness Magnetic method |
| EN ISO 2177 : 2004 | METALLIC COATINGS - MEASUREMENT OF COATING THICKNESS - COULOMETRIC METHOD BY ANODIC DISSOLUTION |
| ISO 9227:2017 | Corrosion tests in artificial atmospheres — Salt spray tests |
| EN 2831:1993 | Aerospace series - Hydrogen embrittlement of steels - Test by slow bending |
| ISO 2177:2003 | Metallic coatings — Measurement of coating thickness — Coulometric method by anodic dissolution |
| EN 2828:1993 | Aerospace series - Adhesion test for metallic coatings by burnishing |
| EN ISO 2178:2016 | Non-magnetic coatings on magnetic substrates - Measurement of coating thickness - Magnetic method (ISO 2178:2016) |
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