MIL I 6870 : E
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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INSPECTION PROGRAM REQUIREMENTS NONDESTRUCTIVE FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS
Available format(s)
PDF
Language(s)
English
Publisher
Superseded date
18-07-1996
Superseded by
£13.91
Excluding VAT
Describes non-destructive inspection program for procurement of all products and supplies in item specification contract.
| Committee |
AREA NDTI
|
| DocumentType |
Standard
|
| Pages |
14
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
| MIL-HDBK-337 Base Document:1982 | Adhesive Bonded Aerospace Structure Repair |
| MIL-B-007883 Revision C:1968 | Brazing of Steels, Copper, Copper Alloys, Nickel Alloys, Aluminum and Aluminum Alloys (Future Acquisitions should specify one AWS-C3.4, AWS-C3.5, AWS-C3.6 and AWS-C3.7) |
| MIL-A-83377 Revision B:1978 | Adhesive Bonding (Structural) for Aerospace and Other Systems, Requirements for (No S/S Document) |
| MIL-C-81769 Base Document:1972 | Chemical Milling of Metals, Specification for (S/S by SAE-AMS-C-81769) |
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-A-23121 Revision C:1970 | Aircrew Environmental, Escape and Survival Cockpit Capsule System General Specification for (No S/S Document) |
| MIL-HDBK-1587 Base Document:1996 | Materials and Process Requirements for Air Force Weapons Systems (S/S by MIL-STD-1587) |
| 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-A-81973 Base Document:1974 | Aircrew Automated Escape Systems, Test Vehicles for Ground Track Performance Testing, Rocket and/or Jet Engine Propelled, General Specification for (No S/S Document) |
| 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)/11(2013) : 2013 | 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)/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 |
| I.S. EN 14165:2004 | SPACE ENGINEERING STANDARDS - FRACTURE CONTROL |
| MIL-STD-1252 Base Document:1975 | Inertia Friction Welding Process, Procedure and Performance Qualification |
| MIL-HDBK-2097 Revision A:1997 | Acquisition of Support Equipment and Associated Integrated Logistics Support |
| MIL-STD-1547 Revision B:1992 | Electronic Parts, Materials, and Processes for Space and Launch Vehicles |
| MIL-B-9972 Revision B:1994 | Brazing, Nickel Alloy, General Specification for (S/S by AWS-C3.6) |
| MIL-HDBK-349 Base Document:1994 | Manufacture and Inspection of Adhesive Bonded, Aluminum Honeycomb Sandwich Assemblies for Aircraft |
| FF-N-836 Revision E:1994 | Nut: Square, Hexagon, Cap, Slotted, Castle, Knurled, Welding and Single Ball Seat |
| JSSG-2006 Base Document:1998 | Aircraft Structures |
| MIL-HDBK-83377 Base Document:1997 | Adhesive Bonding (Structural) for Aerospace and Other Systems, Requirements for |
| MIL-STD-645 Revision B:1981 | DIP BRAZING OF ALUMINUM ALLOYS |
| MIL-A-83376 Revision A:1978 | Adhesive Bonded Metal Faced, Sandwich Structures, Acceptance Criteria (No S/S Document) |
| ADS-13F-HDBK : 1997 | AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES |
| SAE AMSC81769A | Chemical Milling of Metals, Specification for |
| 03/311008 DC : DRAFT JUNE 2003 | EN 14165 - SPACE ENGINEERING STANDARDS - FRACTURE CONTROL |
| BS EN 14165:2004 | Space engineering standards. Fracture control |
| EN 14165:2004 | Space engineering standards - Fracture control |
| MIL-I-6868 Revision E:1976 | Inspection Process, Magnetic Particle (S/S by MIL-STD-1949) |
| DOD-STD-1866 Base Document:1968 | Soldering Process General (Non-Electrical) (No S/S Document) |
| MIL-I-83387 Revision A:1982 | Inspection Process, Magnetic Rubber (S/S by SAE-AMS-I-83387) |
| NASA MSFC STD 506 : 1988 | MATERIALS AND PROCESSES CONTROL |
| MIL-W-5013 Revision L:1991 | Wheel and Brake Assemblies, Aircraft General Specification For |
| DIN EN 14165:2005-02 | SPACE ENGINEERING STANDARDS - FRACTURE CONTROL |
| MIL-STD-1530 Revision D:2016 | Aircraft Structural Integrity Program (ASIP) |
| ASTM E 309 : 2016 : REDLINE | Standard Practice for Eddy Current Examination of Steel Tubular Products Using Magnetic Saturation |
| MIL I 8950 : B | INSPECTION, ULTRASONIC, WROUGHT METALS, PROCESS FOR |
| MIL-STD-410 Revision E:1991 | NONDESTRUCTIVE TESTING PERSONNEL QUALIFICATION AND CERTIFICATION (SEE NAS410 AS A POSSIBLE REPLACEMENT) |
| MIL I 6866 : B | INSPECTION, PENETRANT METHOD OF |
| MIL-STD-1537 Revision C:2002 | Electrical Conductivity Test for Verification of Heat Treatment of Aluminum Alloys, Eddy Current Method |
| MIL-STD-453 Revision C:1984 | Inspection, Radiographic (S/S By ASTM-E1742) |
| MIL-I-83387 Revision A:1982 | Inspection Process, Magnetic Rubber (S/S by SAE-AMS-I-83387) |
| 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-I-6868 Revision E:1976 | Inspection Process, Magnetic Particle (S/S by MIL-STD-1949) |
| MIL-STD-867 Revision C:2008 | Temper Etch Inspection |
| ASTM E 215 : 2016 : REDLINE | Standard Practice for Standardizing Equipment and Electromagnetic Examination of Seamless Aluminum-Alloy Tube |
| MIL A 83444 : 0 | AIRPLANE DAMAGE TOLERANCE REQUIREMENTS |
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