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Heat Application for Thermosetting Resin Curing
- Aerospace Standard
- ARP5144
- Reaffirmed
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This SAE Aerospace Recommended Practice (ARP) describes standard methods of heat application to cure thermosetting resins for commercial aircraft composite repairs.
The methods described in this document shall only be used when specified in an approved repair document or with the agreement of the Original Equipment Manufacturer (OEM) or regulatory authority.
Rationale
This document has been reaffirmed to comply with the SAE 5-year Review policy.
Recommended Content
| Aerospace Material Specification | Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 0 - Introduction |
| Aerospace Standard | Teaching Points for a Class on “Critical Issues in Composite Maintenance, Repair and Overhaul” |
| Aerospace Standard | Core Restoration of Thermosetting Composite Components |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Unnamed Dataset 3 | ||
| TABLE 1 | Thermal Conductivity Coefficients | |
| TABLE 2 | Standard Thermocouple Characteristics |
Issuing Committee
AMS CACRC Commercial Aircraft Composite Repair Committee
Scope: The charter of the ATA/IATA/SAE Commercial Aircraft Composite Repair Committee (CACRC) is to develop and improve maintenance, inspection and repair of commercial aircraft composite structure and components. The seven CACRC task groups are: Repair Materials, Repair Techniques, Analytical Repair Techniques, Design, Inspection, Training and Airline Inspection & Repair Conditions.
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