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SAE ARP1524A

Current

Current

The latest, up-to-date edition.

Surface Preparation and Priming of Aluminum Alloy Parts for High Durability Structural Adhesive Bonding

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

19-07-2013

€93.68
Excluding VAT

1 SCOPE
2 DESCRIPTION OF THE PROCESS
3 HANDLING OF PARTS
4 STORAGE OF PARTS
5 EQUIPMENT AND ENVIRONMENT CONTROL
6 SURFACE PREPARATION SYSTEM FOR ALUMINUM ALLOY PARTS
7 QUALITY ASSURANCE PROVISIONS
8 APPROVAL
9 SAFETY
10 NOTES

Specifies the processing system and techniques for the surface preparation on priming of aluminum alloy parts for structural adhesive bonding to achieve optimum bondline durability, corrosion resistance, and manufacturing producibility.

DocumentType
Standard
Pages
10
PublisherName
SAE International
Status
Current
Supersedes

This Aerospace Recommended Practice (ARP) describes the processing system and techniques for the surface preparation and priming of aluminum alloy parts for structural adhesive bonding to achieve optimum bondline durability, corrosion resistance, and manufacturing producibility.

MIL-A-83377 Revision B:1978 ADHESIVE BONDING (STRUCTURAL) FOR AEROSPACE AND OTHER SYSTEMS, REQUIREMENTS FOR
AWS WHB.3.9 : 2007 WELDING PROCESSES - PART 2: WELDING HANDBOOK, 9TH EDITION, VOL. 3
DEFSTAN 00-970(PT1)SEC4/8(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4 - DESIGN AND CONSTRUCTION
DEFSTAN 00-970(PT1)SEC4/7(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
DEFSTAN 00-970(PT1)SEC4/9(2012) : 2012 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4 - DESIGN AND CONSTRUCTION
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(PT1)SEC4/5(2007) : 2007 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 4: DESIGN AND CONSTRUCTION
DEFSTAN 07-85(PT1)/3(2006) : 2006 DESIGN REQUIREMENTS FOR WEAPONS AND ASSOCIATED SYSTEMS - PART 1: MANDATORY DESIGN REQUIREMENTS
DEFSTAN 00-970(PT1)SEC4/11(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
DEFSTAN 00-970(PT1)SEC4/10(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
DEFSTAN 00-970(PT1)SEC4/4(2006) : 2006 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT A/C - SECTION 4: DESIGN AND CONSTRUCTION
DEFSTAN 00-970(PT1)SEC4/12(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
DEFSTAN 00-970(PT1)SEC4/6(2010) : 2010 DESIGN AND AIRWORTHINESS REQUIREMENTS FORD SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
DEFSTAN 00-970(PT1)SEC4/13(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
SAE AMS 3107 : 1983(R2014) PRIMER, ADHESIVE, CORROSION-INHIBITING, FOR HIGH DURABILITY STRUCTURAL ADHESIVE BONDING
SAE AMS 3695 : 2014 ADHESIVE FILM, EPOXY-BASE, FOR HIGH DURABILITY STRUCTURAL ADHESIVE BONDING
MIL-HDBK-349 Base Document:1994 MANUFACTURE AND INSPECTION OF ADHESIVE BONDED, ALUMINUM HONEYCOMB SANDWICH ASSEMBLIES FOR AIRCRAFT
DEFSTAN 00-970(PT1)SEC4/14(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
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)
MIL-HDBK-83377 Base Document:1997 Adhesive Bonding (Structural) for Aerospace and Other Systems, Requirements for

MIL-T-81533 Revision A:1967 TRICHLOROETHANE, 1, 1, 1, (METHYL CHLOROFORM) INHIBITED, VAPOR DEGREASING

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