MIL-P-9400 Revision C:1991
Current
Current
The latest, up-to-date edition.
Plastic Laminate and Sandwich Construction Parts and Assembly, Aircraft Structural, Process Specification Requirements
Available format(s)
PDF
Language(s)
English
Published date
14-11-1991
Publisher
€16.67
Excluding VAT
Details process specifications for processing and inspection of structural plastic laminate and sandwich construction parts for aircraft.
| DocumentType |
Standard
|
| Pages |
19
|
| ProductNote |
NEW CHILD NOT 1 2019 IS NOW ADDED.
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
This specification provides detailed instructions for the preparation of, and requirements to be included in, process specifications required for the processing, inspection, pre-fit, and assembly of structural plastic laminate and sandwich construction parts for aircraft.
| 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 for (No S/S Document) |
| 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 and Electronic Applications |
| MIL-R-38522 Revision B:1972 | RADOME CW-860/GPS( ) (NO S/S DOCUMENT) |
| 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, Flyer\'s HGU-55/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 (NO S/S DOCUMENT) |
| MIL-P-82540 Base Document:1968 | PLASTICS MATERIALS, POLYESTER RESIN, GLASS FIBER BASE, FILAMENT WOUND TUBE (NO S/S DOCUMENT) |
| JSSG-2006 Base Document:1998 | 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 (NO S/S DOCUMENT) |
| MIL-P-25515 Revision C:1968 | PLASTIC MATERIALS, PHENOLIC RESIN, GLASS-FIBER BASE, LAMINATED |
| MIL-C-9084 Revision C:1970 | Cloth, Glass, Finished, for Resin Laminates (S/S by SAE-AMS-C-9084) |
| MIL-S-9041 Revision B:1975 | Sandwich Construction; Plastic Resin, Glass Fabric Base, Laminated Facings and Honeycomb Core for Aircraft Structural and Electronic Applications |
| MIL-A-83377 Revision B:1978 | Adhesive Bonding (Structural) for Aerospace and Other Systems, Requirements for (No S/S Document) |
| 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 (See Notice 1 for Replacement Information) |
| MIL-A-25463 Revision B:1982 | Adhesive, Film Form, Metallic Structural sandwich Construction (S/S by SAE-AMS-A-25463) |
| MIL-C-81986 Base Document:1974 | Core Material, Plastic Honeycomb, Nylon, Paper Base, for Aircraft Structural Applications(S/S by SAE-AMS-C-81986) |
| MIL-STD-143 Revision B:1969 | STANDARDS & SPECIFICATIONS, ORDER OF PRECEDENCE FOR THE SELECTION OF (S/S BY MIL-STD-970) |
| MIL-A-83376 Revision A:1978 | Adhesive Bonded Metal Faced, Sandwich Structures, Acceptance Criteria (No S/S Document) |
| 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 (See Notice 3 for Replacement Information) |
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