MMM-A-132 Revision B:1994
Current
Current
The latest, up-to-date edition.
Adhesives, Heat Resistant, Airframe Structural, Metal to Metal
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PDF
Published date
01-04-1994
Publisher
€16.67
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PACKAGING
6. NOTES
Describes the requirements for heat resistant adhesives for use in bonding primary and secondary structural and external metallic airframe parts which will be exposed to temperatures within the range of -67 Degrees to 500 Degrees F (-55 Degrees to 260 Degrees C).
| DevelopmentNote |
B NOTICE 1 - Notice of Inactivation for new design. B NOTICE 2 - Notice of Reactivation. (02/2005)
|
| DocumentType |
Standard
|
| Pages |
33
|
| ProductNote |
NEW CHILD NOT 3 2019 IS NOW ADDED
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| Supersedes |
This specification covers the requirements for heat resistant adhesives for use in bonding primary and secondary structural and external metallic airframe parts which will be exposed to temperatures within the range of -67 degrees to 500 degrees F (-55 degrees to 260 degrees C).
| Standards | Relationship |
| SAE AMS3693D | Similar to |
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| MIL-P-5431 Revision A:1967 | Plastic, Phenolic, Graphited Sheets, Rods, Tubes and Shapes |
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| MIL M 83521 : A | MAINTENANCE KIT, ELECTRICAL CONNECTORS, GENERAL SPECIFICATION FOR |
| MIL-DTL-27443 Revision F:2003 | Pallets, Cargo, Aircraft, Type HCU-6/E |
| MS16051 Revision G:2014 | Coupling, Ground Cooling, Combat Type Aircraft |
| MIL-P-47276 Revision B:1991 | PRIMER, BONDING (NO S/S DOCUMENT) |
| DEFSTAN 00-970(PT1)SEC4/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION |
| MIL-A-25463 Revision B:1982 | Adhesive, Film Form, Metallic Structural sandwich Construction (S/S by SAE-AMS-A-25463) |
| MIL-DTL-83507 Revision A:2017 | Tool Kits, Electrical Connectors, Contacts, and Connector and Cable Accessories: General Specification for |
| SAE AMS4258B | Laminated Sheet, Aluminum Alloy, Aramid Fiber Reinforced 5.7Zn - 2.2Mg - 1.6Cu - 0.22Cr (Alclad, One Side 7475-T761) 5 or 7 Ply |
| DIN 65090:1979-07 | AEROSPACE; TEXTILE GLASS, PREIMPREGNATED FILAMENT GLASS CLOTH FROM E-GLASS (PREPREG), TECHNICAL SPECIFICATIONS |
| MIL-A-47074 Revision A:1983 | Adhesive System, Epoxy, for Dissimilar Metal Bonding (S/S by A-A-56015) |
| MIL-P-9400 Revision C:1991 | Plastic Laminate and Sandwich Construction Parts and Assembly, Aircraft Structural, Process Specification Requirements |
| MIL-P-43772 Revision A:1987 | PANEL, TYPE II MODULAR PLATFORM, AIRDROP (NO S/S DOCUMENT) |
| SAE AMSS83474B | Shims, Molded, Filled Resin Compound and Sheet Prepeg |
| FED-STD-313 Revision D:1996 | Material Safety Data, Transportation Data, and Disposal Data for Hazardous Materials Furnished to Government Activities |
| PPP-C-96 Revision E:1992 | Cans, Metal, 28 Gage and Lighter |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| PPP-B-636 Revision J:1981 | Boxes, Shipping, Fiberboard (S/S by ASTM-D1974 and ASTM-D5118) |
| PPP-B-566 Revision E:1974 | Boxes, Folding, Paperboard |
| MIL T 5624 : R | TURBINE FUEL, AVIATION, GRADES JP 4 AND JP 5 |
| ASME B46.1 : 2009 | SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY) |
| MIL-T-9046 Revision J:1983 | TITANIUM AND TITANIUM ALLOY, SHEET, STRIP AND PLATE (S/S BY SAE-AMS-T-9046) |
| FED-STD-123 Revision H:2007 | Marking for Shipment (Civil Agencies) |
| PPP-B-676 Revision E:1992 | Boxes, Setup |
| MIL B 22191 : D | BARRIER MATERIAL, TRANSPARENT, FLEXIBLE, HEAT SEALABLE |
| MIL H 83282 : C | HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, AIRCRAFT, METRIC, NATO CODE NUMBER H 537 |
| PPP-B-601 Revision H:1989 | BOXES, WOOD, CLEATED-PLYWOOD (S/S BY ASTM-D6251) |
| MIL-STD-105 Revision E:1989 | Sampling Procedures and Tables for Inspection by Attributes (See Notice 3 for Replacement Information) |
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