MIL-A-25463 Revision B:1982
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
ADHESIVE, FILM FORM, METALLIC STRUCTURAL SANDWICH CONSTRUCTION
Available format(s)
PDF
Superseded date
30-09-1999
Publisher
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1 SCOPE
2 APPLICABLE DOCUMENTS
3 REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PACKAGING
6 NOTES
Outlines requirements for adhesives for bonding metal facings to metal cores and to metal components of sandwich panels intended for use in primary and secondary structural airframe parts exposed to temperatures up to 500 deg F (260 deg C).
| Committee |
FSC 8040
|
| DevelopmentNote |
B NOTICE 2 - Notice of Cancellation/Superseded by SAE AMS A 25463 (05/2004)
|
| DocumentType |
Standard
|
| Pages |
24
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| Standards | Relationship |
| SAE AMS3693D | Similar to |
| SAE AMS A 25463 : 2013 | Similar to |
| DOD-S-87956 Base Document:1979 | SHELTER, S-80A AND S-82A |
| MIL-HDBK-337 Base Document:1982 | ADHESIVE BONDED AEROSPACE STRUCTURE REPAIR |
| DEFSTAN 00-970(PT7)SEC4/2(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 4: DETAIL DESIGN AND STRENGTH OF MATERIALS |
| MIL-L-81293 Revision A:1992 | LIGHTWEIGHT SANDWICH CONSTRUCTED PANEL (ASROC) LAUNCHER MK 112 |
| MIL-A-23121 Revision C:1970 | AIRCREW ENVIRONMENTAL, ESCAPE AND SURVIVAL COCKPIT CAPSULE SYSTEM, GENERAL SPECIFICATION FOR |
| 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)/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)/14(2014) : 2014 | 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 |
| SAE AMS 3109 : 2014 | PRIMER, ADHESIVE, ELECTRODEPOSITED -55 TO +82 DEGREES C (-67 TO +180 DEGREES F) |
| DEFSTAN 00-970(PT7)SEC2/SUPP4/5(2015) : INTERIM | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 4: DESIGN AND CONSTRUCTION (SUBPART D) |
| DEFSTAN 00-970(PT7)SEC2/SUPP4/6(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 4: DESIGN AND CONSTRUCTION (SUBPART D) |
| SAE AMS 3688 : 2014 | ADHESIVE, FOAMING, HONEYCOMB CORE SPLICE, STRUCTURAL, -55 DEGREES C TO +82 DEGREES C (-65 DEGREES F TO +180 DEGREES F) |
| SAE AMS 3689 : 2014 | ADHESIVE, FOAMING, HONEYCOMB, CORE SPLICE, STRUCTURAL, -54 TO +177 DEGREES C (-65 TO +350 DEGREES F) |
| MIL-HDBK-772 Base Document:1981 | MILITARY PACKAGING ENGINEERING |
| DEFSTAN 00-970(PT7)SEC4/1(2006) : 2006 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 4: DETAIL DESIGN AND STRENGTH OF MATERIALS |
| MIL-P-9400 Revision C:1991 | PLASTIC LAMINATE AND SANDWICH CONSTRUCTION PARTS, AIRCRAFT STRUCTURAL PROCESS SPECIFICATION REQUIREMENTS |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| PPP-B-636 Revision J:1981 | BOX, SHIPPING, FIBERBOARD |
| MIL-A-83377 Revision B:1978 | ADHESIVE BONDING (STRUCTURAL) FOR AEROSPACE AND OTHER SYSTEMS, REQUIREMENTS FOR |
| MIL T 5624 : R | TURBINE FUEL, AVIATION, GRADES JP 4 AND JP 5 |
| ASTM C 393 : 2000 | Standard Test Method for Flexural Properties of Sandwich Constructions |
| MIL-C-7438 Revision G:1985 | CORE MATERIAL, ALUMINUM, FOR SANDWICH CONSTRUCTION |
| ASTM D 1781 : 1998 | Standard Test Method for Climbing Drum Peel for Adhesives |
| MIL B 22191 : D | BARRIER MATERIAL, TRANSPARENT, FLEXIBLE, HEAT SEALABLE |
| ASTM C 297 : 1994 : R1999 | Standard Test Method for Flatwise Tensile Strength of Sandwich Constructions |
| PPP-B-601 Revision H:1989 | BOXES, WOOD, CLEATED PLYWOOD |
| MMM-A-132 Revision B:1994 | ADHESIVES, HEAT RESISTANT, AIRFRAME STRUCTURAL, METAL TO METAL |
| MIL-STD-105 Revision E:1989 | SAMPLING PROCEDURES AND TABLES FOR INSPECTION BY ATTRIBUTES |
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