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. Purpose The purpose of this document is to provide a number of standard heat application methods that may be referenced in repair documents produced by airlines or airframe and engine manufacturers. This document is one of several in support of other procedures required to perform composite repairs@ intended for use throughout the commercial aircraft industry. These include AIR4844@ AIR4938@ AIR5278@ ARP4916@ ARP4991 and others incorporated herein.
SAE ARP5144A-2017 history
1970SAE ARP5144A-2023 Heat Application for Thermosetting Resin Curing
2017SAE ARP5144A-2017 Heat Application for Thermosetting Resin Curing
2011SAE ARP5144-2011 Heat Application for Thermosetting Resin Curing
2000SAE ARP5144-2000 Heat Application for Thermosetting Resin Curing