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CURRENT
2017-07-17
Standard
AMS2482E
This specification establishes the requirements for a hard aluminum oxide coating, impregnated or codeposited with polytetrafluoroethylene (PTFE) on aluminum alloys.
2017-07-13
WIP Standard
AIR4938C
This is a general curriculum that has been developed to identify the minimum knowledge and skill requirements of a composite and/or metal bond repair technician/specialist. This revision changes the document from an all-inclusive curriculum into a modular set of curricula. Teaching levels have been assigned to the curriculum to define the knowledge, skills and abilities graduates will need to make composite repairs. Minimum hours of instruction have been provided to ensure adequate coverage of all subject matter - lecture and laboratory. These minimums may be exceeded, and may include an increase in the total number of training hours and/or increases in the teaching levels.
CURRENT
2017-07-12
Standard
J2253_201707
This SAE Standard is intended to serve as a guide for the collection of physical, mechanical, and thermal properties of fiber-reinforced polymer composite materials for automotive structural applications. This document attempts to utilize test methods applicable to the widest range of structural materials and processes without compromising the integrity of the data being sought. A summary of the material characterization is shown in Section 15.
CURRENT
2017-06-20
Standard
AIR4844C
The following terminology has been generated by the ATA/IATA/SAE Commercial Aircraft Composite Repair Committee (CACRC) and provides terminology for design, fabrication, and repair of composite and bonded metal structures. The purpose of this AIR is to provide terminology that should be used when developing CACRC repair documents or repair documents produced by airlines or airframe and engine manufacturers. It is intended to develop this AIR into an AS.
CURRENT
2017-06-16
Standard
AMS4300D
This specification covers boron filaments and 6061-0 aluminum alloy foil laminated and bonded into a composite sheet.
CURRENT
2017-06-05
Standard
AIR4938B
This is a general curriculum that has been developed to identify the minimum knowledge and skill requirements of a composite and/or metal bond repair technician/specialist. This revision changes the document from an all-inclusive curriculum into a modular set of curricula. Teaching levels have been assigned to the curriculum to define the knowledge, skills and abilities graduates will need to make composite repairs. Minimum hours of instruction have been provided to ensure adequate coverage of all subject matter - lecture and laboratory. These minimums may be exceeded, and may include an increase in the total number of training hours and/or increases in the teaching levels.
2017-05-26
WIP Standard
ARP4977A
This SAE Aerospace Recommended Practice (ARP) describes standard methods for drying commercial aircraft composite structures prior to repair and gives general guidelines on use and applicability. It addresses the removal of liquids that have collected inside the structures through open damage, microcracks, or porosity and the removal of absorbed moisture from the composite material. 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. If this document is used for the drying of materials other than thermosetting composite materials, the fitness for this purpose must be determined by the user. The purpose of this document is to provide a set of standard drying methods that may be referenced in repair documents produced by airlines or airframe and engine manufacturers.
CURRENT
2017-04-03
Standard
ARP5144A
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.
CURRENT
2017-03-21
Standard
AMS03_1A
This SAE Standard specifies the processes and type of impregnant which can be used when impregnating castings for the following purposes: a. For the recovery of ferrous and non-ferrous castings containing micro porosity, where pressure tightness is mandatory. b. For sealing castings/sinter metal components to improve corrosion resistance and/or to render the surface suitable for subsequent surface treatment.
2017-03-15
WIP Standard
AMS3711F
This specification covers expanded honeycomb core made of fibrous aramid paper sheets and supplied in the form of blocks, slices, and ordered shapes. This honeycomb core has been used typically for bonded sandwich structures requiring high strength and corrosion resistance in the temperature range -65 to +180 °F (-54 to +82 °C), but usage is not limited to such applications.
CURRENT
2017-02-21
Standard
ARP5448/6A
This method outlines a standard procedure for performing conformity tests of bearings utilizing liners of bonded polytetrafluoroethylene (PTFE). The data from these tests shall be used to determine if the product meets the conformity requirements of the applicable specification.
2017-01-12
WIP Standard
AMS3713E
This specification covers honeycomb core made of polymide paper sheets in a non-hexagonal, flexible cell configuration and supplied in the form of blocks, slices, and ordered shapes. This honeycomb core has been used tyipcally in sandwich structures in single or compound curvature parts requiring high strength and corrosion resistance in the temperature range -55 to +82 degrees C (-67 to +180 degrees F) but usage is not limited to such applications.
CURRENT
2016-12-27
Standard
AMS3892/10B
This specification covers one type of carbon fiber in the form of tow.
CURRENT
2016-12-16
Standard
AMS3832D
This specification covers continuous, multiple-strand, roving of Type "S-2" glass impregnated with a heat-curable epoxy resin matrix and processed to a "B" stage condition.
CURRENT
2016-12-16
Standard
AMS3844C
This specification covers one type of glass cloth impregnated with a heat-reactive, thermosetting, hot-melt, addition-type, polyimide resin system, furnished in continuous rolls of full width material.
CURRENT
2016-12-16
Standard
AMS3892/1C
This specification covers one type of continuous multifilament carbon fibers in the form of a tow or yarn (when twisted). The weight per unit length of the tow or yarn is governed by the filament count which is identified by the supplier's grade or material designation.
CURRENT
2016-12-16
Standard
AMS3892/5C
This specification covers one type of continuous multifilament carbon fibers in the form of a tow or yarn (when twisted). The weight per unit length of the tow or yarn is governed by the filament count which is identified by the supplier's grade or material designation.
CURRENT
2016-12-16
Standard
AMS3892/6B
This specification covers one type of continuous multifilament carbon fibers in the form of a tow or yarn (when twisted). The weight per unit length of the tow or yarn is governed by the filament count which is identified by the supplier's grade or material designation.
CURRENT
2016-12-16
Standard
AMS3892/3C
This specification covers one type of continuous multifilament carbon fibers in the form of a tow or yarn (when twisted). The weight per unit length of the tow or yarn is governed by the filament count which is identified by the supplier's grade or material designation.
CURRENT
2016-12-15
Standard
AMS3895C
This specification covers epoxy-resin-impregnated carbon-fiber broadgoods and tape in the form of multi-plied unidirectional layers constructed from the same or uniform fibers and supplied as broadgood rolls, tape, or cut sheet. The individual ply orientation shall be as ordered.
CURRENT
2016-12-15
Standard
AMS3831B
This specification covers a glass cloth impregnated with a heat-curable epoxy resin system, the resin being processed to a “B” stage condition, and furnished in the form of continuous rolls.
CURRENT
2016-12-15
Standard
AMS3834B
This specification covers a style 7781 glass cloth impregnated with a heat-curable polyester resin system, the resin being processed to a “B” stage condition, and furnished in the form of continuous rolls.
CURRENT
2016-12-15
Standard
AMS3845C
This specification cover glass cloth impregnated with a heat-reactive, thermosetting, addition-cure polyimide resin system, the resin to be supplied in a "B" stage condition.
CURRENT
2016-12-15
Standard
AMS3847D
This specification covers one type of quartz cloth impregnated with a heat-reactive, thermosetting, polyimide resin system, the resin being processed to a "B" stage condition, and furnished in continuous rolls of full width material.
CURRENT
2016-12-15
Standard
AMS3849C
This specification covers one type of quartz cloth impregnated with a heat-reactive, thermosetting, hot-melt, addition-type, polyimide resin system, furnished in continuous rolls of full width material.
CURRENT
2016-12-15
Standard
AMS3890B
The product shall consist of 5-ply yarn having 720 continuous filaments per ply and a maximum of 4 turns per inch (25.4 mm).
CURRENT
2016-12-15
Standard
AMS3892C
This specification and its supplementary detail specifications cover carbon fibers in the form of continuous multifilament tow and yarn.
CURRENT
2016-12-15
Standard
AMS3837E
This specification covers "S" glass in one style of woven fabric with an HTS-904 finish.
CURRENT
2016-12-15
Standard
AMS3892/2C
This specification covers one type of continuous multifilament carbon fibers in the form of a tow or yarn (when twisted). The weight per unit length of the tow or yarn is governed by the filament count which is identified by the supplier's grade or material designation.
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