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MIL-S-58095 Seat System: Crash Resistant, Non-Ejection, Aircrew, General Specification For

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MIL-S-58095A (AV)
TABLE I. Seat Design and Static test Requirements
12.3 Restraint System Strength and Elongation. Strength and dimensional
properties of the restraint webbing shall conform to Table II. The strength and
elongation properties of the lap belt, shoulder harness and lap belt. tiedown
strap assemblies shall conform to 4.7.7.
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