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Seat Primary Load Path 16G Seat Testing Term

Seat Primary Load Path – The components within the seat that carry the load from the
point of load application to the structure that reacts the load from the seat system or sub-
system. The primary load path may be segmented into its discrete elements, depending
on the parameter being evaluated, as follows:
 Structural: from seat belt to fittings which attach the seat system to the airplane
structure.
 Lumbar: from bottom cushion to fittings which attach the seat system to the
airplane structure.
Row-to Row Head Injury Criterion (HIC): from point of ATD head contact to the
attachment of seat primary structure.
 Head Path (for example, front row or large pitch seats): same as structural. – AC 25.562-1B

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Posted in Aircraft Systems Terms, FAA Terms | Tagged 16G, Aircraft, Airline, Engineering, FAA, Seats

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    14 CFR 1.1 16G Abbreviation Acronym Aerodynamics Aircraft Airline Airlines Airport Airports Airworthiness AMT ATC Aviation Safety Aviation Weather Avionics Bird Strike Engineering ETOPS FAA FAA Pilot's Handbook Flight Flying Human Factors ICAO Icinig Inspection Instruments International Landing Maintenance Military Navigation NextGen Parts Pilot Technique Powerplant Regulatory Safety Seats Structures Systems Tires UK Weather

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