SAE ARP 4916 : 1997
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
MASKING AND CLEANING OF EPOXY AND POLYESTER MATRIX THERMOSETTING COMPOSITE MATERIALS
Available format(s)
Hardcopy , PDF
Superseded date
03-01-2016
Superseded by
Language(s)
English
Published date
01-01-1997
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.| DocumentType |
Standard
|
| Pages |
46
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy |
| SAE ARP5256 | MIXING RESINS, ADHESIVES AND POTTING COMPOUNDS |
| SAE AMS 2980/1 : 2014 | CARBON FIBER FABRIC AND EPOXY RESIN WET LAY-UP REPAIR MATERIAL - PART 1 - GENERAL REQUIREMENTS |
| SAE AIR5367 | Machining of Composite Materials, Components and Structures |
| SAE ARP 5143 : 2018 | VACUUM BAGGING OF THERMOSETTING COMPOSITE AND METALBOND REPAIRS |
| SAE ARP 5144 : 2017 | HEAT APPLICATION FOR THERMOSETTING RESIN CURING |
| SAE ARP 5319 : 2011 | IMPREGNATION OF DRY FABRIC AND PLY LAY-UP |
| SAE AIR5431 | Repair Tooling |
| SAE ARP4991A | Core Restoration of Thermosetting Composite Components |
| SAE AMS3970/1A | Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 1 - General Requirements |
| SAE AIR6291 | Guidelines for Repair Process Evaluation of Aluminum Bonded Structure |
| FAA AC 43-214 : 2016 | REPAIRS AND ALTERATIONS TO COMPOSITE AND BONDED AIRCRAFT STRUCTURE |
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