MIL-STD-2154 Base Document:1982
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Inspection, Ultrasonic, Wrought Metals, Process for (S/S by ASTM-E2375 and SAE-AMS-STD-2154)
30-09-1982
15-11-2004
1. SCOPE
1.1 Purpose
1.2 Application
1.3 Classification
2. REFERENCED DOCUMENTS
2.1 Issues of documents
2.2 Other publications
3. DEFINITIONS
3.1 A-scan presentation
3.2 Angle beam examination
3.3 Attenuation
3.4 Back surface resolution
3.5 C-scan presentation
3.6 Decibel (db)
3.7 Distance-amplitude correction (DAC)
3.8 Entry surface resolution
3.9 Far field
3.10 Horizontal linearity range
3.11 Horizontal limit
3.12 Lower linearity limit
3.13 Near field
3.14 Noise
3.15 Primary reference response
3.16 Signal to noise ratio
3.17 Straight beam examination
3.18 Transducer element
3.19 Ultrasonic sensitivity
3.20 Ultrasonic penetration
3.21 Upper linearity limit
3.22 Vee-path
3.23 Vertical limit
4. GENERAL REQUIREMENTS
4.1 Specifying
4.2 Personnel qualification
4.3 Written procedure
4.4 General procedures
5. DETAIL REQUIREMENTS
5.1 Materials
5.2 Equipment
5.3 Reference standards
5.4 Inspection procedures
5.5 Quality assurance provisions
5.6 Packaging
TABLES
FIGURES
Describes uniform methods for the ultrasonic inspection of wrought metals and wrought metal products.
| DevelopmentNote |
Supersedes MIL I 8950 (B). NOTICE 1 - Notice of Cancellation/Superseded by SAE AMS STD 2154. (12/2004) NOTICE 2 - Notice of Cancellation/Superseded by ASTM E 2375. (05/2008) NOTICE 3 - Notice of Cancellation/Superseded by ASTM E 2375 & SAE AMS STD 2154. (01/2009)
|
| DocumentType |
Standard
|
| Pages |
47
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
The purpose of the military standard is to provide uniform methods for the ultrasonic inspection of wrought metals and wrought metal products.
| DIN 65035:1993-11 | AEROSPACE; STEEL, NICKEL- AND COBALT-ALLOY STOCK, FORGINGS AND RINGS; TECHNICAL SPECIFICATION |
| QQ-A-200-13 Revision C:1983 | Aluminum Alloy 7178, Bar, Rod, Shapes, Tube and Wire, Extruded (Refer to SAE-AMS-QQ-A-200/13, ASTM-B241/B241M and ASTM-B221) |
| SAE AMST81556A | Titanium and Titanium Alloys, Extruded Bars and Shapes, Aircraft Quality |
| DIN 65038-1:1989-08 | AEROSPACE; STEEL, NICKEL- AND COBALT-ALLOYS BARS; TECHNICAL SPECIFICATION |
| MIL-A-22771 Revision D:1984 | Aluminum Alloy Forgings, Heat Treated (S/S by SAE-AMS-A-22771) |
| QQ-A-225 Revision G:1990 | ALUMINUM AND ALUMINUM ALLOY BAR, ROD, WIRE, OR SPECIAL SHAPES; ROLLED, DRAWN, OR COLD FINISHED; GENERAL SPECIFICATION FOR (S/S BY ASTM-B211 AND SAE-AMS-QQ-A-225) |
| NASA MSFC STD 1249 : 1985 | NDE GUIDELINES AND REQUIREMENTS FOR FRACTURE CONTROL PROGRAMS |
| MIL-T-81556 Revision A:1983 | Titanium and Titanium Alloys, Extruded Bars and Shapes, Aircraft Quality |
| MIL-S-8844 Revision D:1987 | STEEL BAR, REFORGING STOCK, AND MECHANICAL TUBING, LOW ALLOY, PREMIUM QUALITY (S/S BY SAE-AMS6414 AND SAE-AMS6257) |
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | 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 |
| 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)/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 |
| 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 |
| 94/712749 DC : 0 | PREN 4050-4 - AEROSPACE SERIES - TEST METHOD FOR METALLIC MATERIALS - ULTRASONIC INSPECTION OF BARS, PLATES, FORGING STOCK AND FORGINGS - PART 4: ACCEPTANCE CRITERIA |
| PREN 6071 : 200P1 | AEROSPACE SERIES - ALUMINIUM AND ALUMINIUM ALLOY WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PLATE |
| BS 5S 100:1993 | Procedure for inspection, testing and acceptance of wrought steels (other than plate, sheet, strip and tube) |
| SAE AS7114/3A | NADCAP Requirements for Nondestructive Testing Facility Ultrasonic Survey |
| SAE AS7100/1B | National Aerospace and Defense Contractors Accreditation Program (NADCAP) Survey Checklists for the NDT Suppliers Accreditation Program |
| NASA STD 5006 : 2015 | GENERAL FUSION WELDING REQUIREMENTS FOR AEROSPACE MATERIALS |
| DIN 29546:1990-10 | Aerospace; wrought aluminium alloys sheet, plate and strip; technical specification; inactive for new design |
| QQ-A-200-3 Revision F:1983 | Aluminum Alloy 2024, Bar, Rod, Shapes, Tube and Wire, Extruded (Refer to ASTM-B221, ASTM-B241/B241M and SAE-AMS-QQ-A-200/3) |
| QQ-A-200-14 Revision B:1984 | Aluminum Alloy Bar, Rod, Shapes, and Wire, Extruded, 7178-T76 (Improved Exfoliation Resistant) (Refer to SAE-AMS-QQ-A-200/14 and ASTM-B221) |
| DIN 65021:1986-11 | AEROSPACE; SHEET, PLATE AND STRIP OF STEEL, NICKEL ALLOYS AND COBALT ALLOYS; TECHNICAL SPECIFICATION |
| MIL-W-5013 Revision L:1991 | Wheel and Brake Assemblies, Aircraft General Specification For |
| QQ-A-200-11 Revision E:1983 | ALUMINUM ALLOY 7075, BAR, ROD, SHAPES, TUBE AND WIRE, EXTRUDED (REFER TO SAE-AMS-QQ-A-200/11, ASTM-B241/B241M AND ASTM-B221) |
| SAE MAM4141B | Aluminum Alloy, Die Forgings, 5.6zn 2.5mg 1.6cu 0.23cr Solution and Precipitation Heat Treated |
| MIL-T-82856 Base Document:1983 | TUNGSTEN, THORIATED, TWO PERCENT, FORGED (NO S/S DOCUMENT) |
| MIL-T-24766 Base Document:1992 | Titanium Forgings and Forgings Stock, High Quality For Ships Service |
| MIL T 82833 : NOTICE 1 | TUNGSTEN, THORIATED, TWO PERCENT, FORGED & CUPPED |
| QQ-A-225-9 Revision E:1982 | Aluminum Alloy 7075, Bar, Rod, Wire and Special Shapes; Rolled, Drawn or Cold Finished (S/S by SAE-AMS-QQ-A-225 and ASTM-B211) |
| ASTM E 127 : 2015 : REDLINE | Standard Practice for Fabrication and Control of Aluminum Alloy Ultrasonic Standard Reference Blocks |
| MIL-STD-410 Revision E:1991 | NONDESTRUCTIVE TESTING PERSONNEL QUALIFICATION AND CERTIFICATION (SEE NAS410 AS A POSSIBLE REPLACEMENT) |
| QQ A 225/6 : E | ALUMINUM ALLOY BAR, ROD, AND WIRE, ROLLED, DRAWN OR COLD FINISHED, 2024 |
| MIL-S-5000 Revision E:1982 | STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS, AND FORGING STOCK (S/S BY SAE-AMS-S-5000) |
| QQ-A-200-11 Revision E:1983 | ALUMINUM ALLOY 7075, BAR, ROD, SHAPES, TUBE AND WIRE, EXTRUDED (REFER TO SAE-AMS-QQ-A-200/11, ASTM-B241/B241M AND ASTM-B221) |
| ASTM E 317 : 2016 : REDLINE | Standard Practice for Evaluating Performance Characteristics of Ultrasonic Pulse-Echo Testing Instruments and Systems without the Use of Electronic Measurement Instruments |
| SAE AMS4928V | Titanium Alloy Bars, Wire, Forgings, Rings, and Drawn Shapes 6Al - 4V Annealed |
| QQ-A-200-3 Revision F:1983 | Aluminum Alloy 2024, Bar, Rod, Shapes, Tube and Wire, Extruded (Refer to ASTM-B221, ASTM-B241/B241M and SAE-AMS-QQ-A-200/3) |
Access your standards online with a subscription
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.
Important note : All end users must be registered with an Account prior to user licenses being assigned.Logging out.