MIL-HDBK-6870 Revision B:2012
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
09-10-2020
English
1. SCOPE
2. APPLICABLE DOCUMENTS
3. DEFINITIONS
4. GENERAL REQUIREMENTS
5. DETAIL REQUIREMENTS FOR PRODUCTION
6. DETAIL REQUIREMENTS FOR TEST ARTICLES
7. DETAIL REQUIREMENTS FOR SUSTAINMENT
8. NOTES
APPENDIX A - Sample Charter for Nondestructive
Inspection Requirements Review Board
(NDIRRB)
Gives guidance to government personnel and contractors for defining the requirements for establishing an acceptable Nondestructive Inspection (NDI) program for the development, production, and sustainment phases of DoD aircraft and missile structural components when directly referenced in the item specification contract or order. Applies to structures for aircraft and missiles when the design activity or system specification requires nondestructive inspection for production acceptance, and recurring nondestructive inspection for long-term sustainment.
| Committee |
AREA NDTI
|
| DevelopmentNote |
Supersedes MIL I 6870 (E). (02/2012)
|
| DocumentType |
Standard
|
| Pages |
28
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| I.S. EN 16603-32-01:2014 | SPACE ENGINEERING - FRACTURE CONTROL |
| 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)/17(2016) : 2016 | 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)/15(2015) : 2015 | 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 |
| DEFSTAN 00-970(PT0)/16(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-STD-1587 Revision D:2017 | MATERIAL AND PROCESS REQUIREMENTS FOR AEROSPACE WEAPONS SYSTEMS |
| SAE AMS I 83387 : 2016 | INSPECTION PROCESS, MAGNETIC RUBBER |
| ASTM E 2981 : 2015 | Standard Guide for Nondestructive Testing of the Composite Overwraps in Filament Wound Pressure Vessels Used in Aerospace Applications |
| BS EN 16603-32-01:2014 | Space engineering. Fracture control |
| NASA STD 6016(INT) : 2006 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
| NASA STD 5005 : 2013 | STANDARD FOR THE DESIGN AND FABRICATION OF GROUND SUPPORT EQUIPMENT |
| NASA KSC DE 512-SM : 2012 | FACILITY SYSTEMS, GROUND SUPPORT SYSTEMS, AND GROUND SUPPORT EQUIPMENT GENERAL DESIGN REQUIREMENTS |
| NASA STD 5019 : 2016 | FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE |
| NASA STD 6016 : 2016 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
| NASA STD 8719.24 : 2011 | NASA EXPENDABLE LAUNCH VEHICLE PAYLOAD SAFETY REQUIREMENTS |
| NASA JSC 27301 : 2009 | MATERIALS AND PROCESSES SELECTION, CONTROL, AND IMPLEMENTATION PLAN FOR JSC FLIGHT HARDWARE |
| NASA GSFC STD 7000 : 2013 | GENERAL ENVIRONMENTAL VERIFICATION STANDARD (GEVS) FOR GSFC FLIGHT PROGRAMS AND PROJECTS |
| MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
| SAE AIR 4777 : 2013(R 2018) | NONDESTRUCTIVE INSPECTION (NDI) METHODS USED DURING PRODUCTION AND OPERATION OF AIRCRAFT WHEELS AND BRAKES |
| MIL-STD-1530 Revision D:2016 | AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP) |
| NASA STD 5005(INT) : 2007 | THE DESIGN AND FABRICATION OF GROUND SUPPORT EQUIPMENT |
| NASA STD 5019(INT) : 2006 | FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE |
| MIL-STD-1568 Revision D:2015 | Materials and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems |
| ASTM E 2982 : 2014 | Standard Guide for Nondestructive Testing of Thin-Walled Metallic Liners in Filament-Wound Pressure Vessels Used in Aerospace Applications |
| EN 16603-32-01:2014 | Space engineering - Fracture control |
| MIL-STD-1530 Revision D:2016 | AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP) |
| MIL-HDBK-1823 Revision A:2009 | NONDESTRUCTIVE EVALUATION SYSTEM, RELIABILITY ASSESSMENT |
| ASTM E 309 : 2016 : REDLINE | Standard Practice for Eddy Current Examination of Steel Tubular Products Using Magnetic Saturation |
| ASTM E 2698 : 2010 | Standard Practice for Radiological Examination Using Digital Detector Arrays |
| SAE AMS 2647 : 2014 | FLUORESCENT PENETRANT INSPECTION, AIRCRAFT AND ENGINE COMPONENT MAINTENANCE |
| NAS410:2003 | NAS CERTIFICATION & QUALIFICATION OF NONDESTRUCTIVE TEST PERSONNEL |
| ASTM E 2662 : 2015 : REDLINE | Standard Practice for Radiographic Examination of Flat Panel Composites and Sandwich Core Materials Used in Aerospace Applications |
| ASTM E 2581 : 2014 : REDLINE | Standard Practice for Shearography of Polymer Matrix Composites and Sandwich Core Materials in Aerospace Applications |
| MIL-STD-1537 Revision C:2002 | Electrical Conductivity Test for Verification of Heat Treatment of Aluminum Alloys, Eddy Current Method |
| ASTM E 2736 : 2010 | Standard Guide for Digital Detector Array Radiology |
| SAE AMS I 83387 : 2016 | INSPECTION PROCESS, MAGNETIC RUBBER |
| ASTM E 1417/E1417M : 2016 : REDLINE | Standard Practice for Liquid Penetrant Testing |
| MIL-STD-3024 Base Document:2008 | PROPULSION SYSTEM INTEGRITY PROGRAM (PSIP) |
| ASTM E 426 : 2016 : REDLINE | Standard Practice for Electromagnetic (Eddy Current) Examination of Seamless and Welded Tubular Products, Titanium, Austenitic Stainless Steel and Similar Alloys |
| MIL-STD-867 Revision C:2008 | TEMPER ETCH INSPECTION |
| MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
| MIL-DTL-87929 Revision E:2017 | MANUALS, TECHNICAL - OPERATION AND MAINTENANCE INSTRUCTIONS IN WORK PACKAGE FORMAT (FOR USAF EQUIPMENT) |
| MIL-STD-1798 Revision C:2013 | MECHANICAL EQUIPMENT AND SUBSYSTEMS INTEGRITY PROGRAM |
| JSSG-2006 Base Document:1998 | JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
| ASTM E 1004 : 2017 : REDLINE | Standard Test Method for Determining Electrical Conductivity Using the Electromagnetic (Eddy Current) Method |
| ASTM E 215 : 2016 : REDLINE | Standard Practice for Standardizing Equipment and Electromagnetic Examination of Seamless Aluminum-Alloy Tube |
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