MIL-P-9400 Revision C:1991
Current
Current
The latest, up-to-date edition.
PLASTIC LAMINATE AND SANDWICH CONSTRUCTION PARTS, AIRCRAFT STRUCTURAL PROCESS SPECIFICATION REQUIREMENTS
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PDF
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English
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Important note : All end users must be registered with an Account prior to user licenses being assigned.Details process specifications for processing and inspection of structural plastic laminate and sandwich construction parts for aircraft.
| DocumentType |
Standard
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| Pages |
19
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| ProductNote |
NEW CHILD NOT 1 2019 IS NOW ADDED.
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Current
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| MIL-P-25518 Revision B:1981 | Plastic Materials, Silicone Resin, Glass Fiber Base, Low Pressure Laminated |
| MIL-M-8555 Revision C:1984 | MISSILE, GUIDED, DESIGN AND CONSTRUCTION, GENERAL SPECIFICATION |
| 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-S-9041 Revision B:1975 | SANDWICH CONSTRUCTION, PLASTIC RESIN, GLASS FABRIC BASE, LAMINATED FACINGS AND HONEYCOMB CORE FOR AIRCRAFT STRUCTURAL APPLICATIONS |
| MIL-R-38522 Revision B:1972 | RADOME CW-860/GPS |
| MIL-S-25392 Revision B:1968 | Sandwich Construction, Plastic Resin, Glass Fabric Base, Laminated Facings and Polyurethane Foamed-in-Place Core, For Aircraft Structural Applications |
| MIL-S-83427 Base Document:1974 | SURVIVAL KIT CONTAINERS, CNU-129(V)/P AND CNU-130/P |
| L-P-383 Base Document:1967 | PLASTIC MATERIAL, POLYESTER RESIN, GLASS FIBER BASE, LOW PRESSURE LAMINATED |
| MIL-DTL-87174 Revision A:1998 | HELMET, FLYERS HGU55/P |
| MIL A 87221 : 0 | AIRCRAFT STRUCTURES, GENERAL SPECIFICATION FOR REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
| MIL-R-7705 Revision B:1975 | RADOME, GENERAL SPECIFICATION FOR |
| MIL-P-82540 Base Document:1968 | PLASTIC MATERIAL, POLYESTER RESIN, GLASS FIBER BASE, FILAMENT WOUND TUBE |
| JSSG-2006 Base Document:1998 | JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
| MIL H 87174 : 0 | HELMET, FLYERS' HGU-55/P |
| MIL-DTL-25421 Revision C:2009 | Plastic Materials, Glass Fiber Base - Epoxy Resin, Low Pressure Laminated |
| ADS-13F-HDBK : 1997 | AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES |
| MIL-P-25770 Revision A:1961 | PLASTIC MATERIALS, ASBESTOS BASE, PHENOLIC RESIN, LOW OR HIGH PRESSURE LAMINATES |
| MIL-P-25515 Revision C:1968 | PLASTIC MATERIAL, PHENOLIC RESIN, GLASS FIBER BASE, LAMINATED |
| MIL-C-9084 Revision C:1970 | CLOTH, GLASS, FINISHED, FOR RESIN LAMINATES |
| MIL-S-9041 Revision B:1975 | SANDWICH CONSTRUCTION, PLASTIC RESIN, GLASS FABRIC BASE, LAMINATED FACINGS AND HONEYCOMB CORE FOR AIRCRAFT STRUCTURAL APPLICATIONS |
| MIL-A-83377 Revision B:1978 | ADHESIVE BONDING (STRUCTURAL) FOR AEROSPACE AND OTHER SYSTEMS, REQUIREMENTS FOR |
| L-P-383 Base Document:1967 | PLASTIC MATERIAL, POLYESTER RESIN, GLASS FIBER BASE, LOW PRESSURE LAMINATED |
| MIL C 8073 : D | CORE MATERIAL, PLASTIC HONEYCOMB, LAMINATED CLASS FABRIC BASE, FOR AIRCRAFT STRUCTURAL AND ELECTRONIC APPLICATIONS |
| MIL-C-7438 Revision G:1985 | CORE MATERIAL, ALUMINUM, FOR SANDWICH CONSTRUCTION |
| MIL-A-25463 Revision B:1982 | ADHESIVE, FILM FORM, METALLIC STRUCTURAL SANDWICH CONSTRUCTION |
| MIL-C-81986 Base Document:1974 | CORE MATERIAL, PLASTIC HONEYCOMB, NYLON PAPER BASE; FOR AIRCRAFT STRUCTURAL APPLICATIONS |
| MIL-STD-143 Revision B:1969 | STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF |
| MIL-A-83376 Revision A:1978 | ADHESIVE BONDED METAL FACED, SANDWICH STRUCTURES, ACCEPTANCE CRITERIA |
| MMM-A-132 Revision B:1994 | ADHESIVES, HEAT RESISTANT, AIRFRAME STRUCTURAL, METAL TO METAL |
| MIL-R-9300 Revision B:1968 | RESIN, EPOXY, LOW-PRESSURE LAMINATING |
| MIL-STD-105 Revision E:1989 | SAMPLING PROCEDURES AND TABLES FOR INSPECTION BY ATTRIBUTES |
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