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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Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

INSPECTION PROGRAM REQUIREMENTS NONDESTRUCTIVE FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS

Available format(s)

PDF

Superseded date

18-07-1996

Language(s)

English

€17.95
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Superseded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
MIL-A-83377 Revision B:1978 ADHESIVE BONDING (STRUCTURAL) FOR AEROSPACE AND OTHER SYSTEMS, REQUIREMENTS FOR
MIL-C-81769 Base Document:1972 CHEMICAL MILLING OF METALS, SPECIFICATION FOR
SAE AMS 3920 : 2014 ACCEPTANCE CRITERIA, ADHESIVE-BONDED METAL-FACED SANDWICH STRUCTURES
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
MIL-HDBK-1587 Base Document:1996 MATERIALS AND PROCESS REQUIREMENTS FOR AIR FORCE WEAPON SYSTEM
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
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 VEHICLES
MIL-B-9972 Revision B:1994 BRAZING, NICKEL, ALLOY, GENERAL SPECIFICATION FOR
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 JOINT SERVICE SPECIFICATION GUIDE - 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
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
DOD-STD-1866 Base Document:1968 SOLDERING PROCESS GENERAL (NON ELECTRICAL)
MIL-I-83387 Revision A:1982 INSPECTION PROCESS, MAGNETIC RUBBER
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 (EDDY CURRENT, LIQUID PENETRANT, MAGNETIC PARTICLE, RADIOGRAPHIC AND ULTRASONIC)
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
MIL-I-83387 Revision A:1982 INSPECTION PROCESS, MAGNETIC RUBBER
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
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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