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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Superseded
Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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Superseded date

09-30-1999

Publisher

US Military Specs/Standards/Handbooks

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B NOTICE 2 - Notice of Cancellation/Superseded by SAE AMS A 25463 (05/2004)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Superseded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 AMS 3693 : 2016 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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