STRUCTURAL WELDBONDING OF ALUMINUM STRUCTURES

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

08-14-2014

Publisher

SAE International

1. SCOPE
2. APPLICABLE DOCUMENTS
3. DESCRIPTION OF THE PROCESS
4. TECHNICAL REQUIREMENTS
5. PROCEDURE
6. PROCESS CONTROL REQUIREMENTS
7. QUALITY ASSURANCE PROVISIONS
8. APPROVAL
9. SAFETY
10. NOTES

Defines the aluminum weldbonding process for fabrication of secondary aircraft structural assemblies possessing excellent strength, fatigue life, and environmental durability.

Committee	AMS-P17
DocumentType	Standard
Pages	36
PublisherName	SAE International
Status	Current
Supersedes	SAE ARP 1675 : 1990

SAE AMS 3708 : 1995	ADHESIVE, EPOXY PASTE, FOR STRUCTURAL WELDBOND For 80°C (180°F) Service
MIL P 17667 : D	PAPER, WRAPPING, CHEMICALLY NEUTRAL (NON CORROSIVE)
MIL-C-22751 Revision D:1971	COATING SYSTEM, EPOXY-POLYAMIDE, CHEMICAL AND SOLVENT RESISTANT, PROCESS FOR APPLICATION OF
SAE AMS 4035 : 2011	ALUMINUM ALLOY, SHEET AND PLATE, 4.4CU - 1.5MG - 0.60MN (2024-0) ANNEALED; OR WHEN SPECIFIED, 'AS FABRICATED' (2024-F)
SAE AMS 4037 : 2014	ALUMINUM ALLOY, SHEET AND PLATE, 4.4CU - 1.5MG - 0.60MN (2024; -T3 FLAT SHEET, -T351 PLATE) SOLUTION HEAT TREATED
SAE AMS 4045 : 2016	ALUMINUM ALLOY SHEET AND PLATE 5.6ZN - 2.5MG - 1.6CU - 0.23CR 7075: (-T6 SHEET, -T651 PLATE) SOLUTION AND PRECIPITATION HEAT TREATED
MIL P 23377 : G	PRIMER COATING, EPOXY, HIGH SOLIDS
MIL-STD-453 Revision C:1984	INSPECTION, RADIOGRAPHIC
SAE AMS 3107 : 1983(R2014)	PRIMER, ADHESIVE, CORROSION-INHIBITING, FOR HIGH DURABILITY STRUCTURAL ADHESIVE BONDING
MIL-H-6088 Revision G:1991	HEAT TREATMENT OF ALUMINIUM ALLOYS
MIL-W-6858 Revision D:1978	WELDING RESISTANCE, SPOT AND SEAM
SAE AMS 3755/2 : 2016	POWDER, FUMED SILICON DIOXIDE, THICKENING EFFICIENCY 95
MIL-T-81533 Revision A:1967	TRICHLOROETHANE, 1, 1, 1, (METHYL CHLOROFORM) INHIBITED, VAPOR DEGREASING