This filler metal has been used typically for joining corrosion and heat resistant steels and alloys requiring corrosion and oxidation resistant joints with good strength at elevated temperatures, but usage is not limited to such applications. This filler metal may also be used as a corrosion and oxidation resistant hard coating.
This SAE Aerospace Standard (AS) defines minimum performance standards, qualification requirements, and minimum documentation requirements for passenger and crew seats in civil rotorcraft, transport aircraft, and general aviation aircraft. The goal is to achieve comfort, durability, and occupant protection under normal operational loads and to define test and evaluation criteria to demonstrate occupant protection when a seat/occupant/restraint system is subjected to statically applied ultimate loads and to dynamic impact test conditions set forth in the applicable Federal Regulations 14 CFR 23, 25, 27, or 29.
Guidance for test procedures, measurements, equipment, and interpretation of results is also presented to promote uniform techniques and to achieve acceptable data.
While this document addresses system performance, responsibility for the seating system is divided between the seat supplier and the installation applicant.
Classification: The properties of heat shrinkable molded components shall be as specified in the applicable specification sheet.
These products have been used typically as a flexible, electrical insulation tubing whose diameter can be reduced to a predetermined size by heating to 150 degrees C (302 degrees F) or higher, but usage is not limited to such applications. This tubing is stable for continuous exposure from -20 to +105 degrees C (-4 to 221 degrees F).