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Thigh-Tangent-Angle-Rotorcraft-Max — Seating Geometry

Name: Mil1333B Cockpit Geometry — seating_geometry: dimension id thigh_tangent_angle_rotorcraft_max · description Thigh tangent angle maximum for rotorcraft · value in 10 inches or degrees (see unit column) · para ref Figure 2 Note 1 · figure ref Figure 2
Creator: Engineering Database

Category: Seating Geometry
Dimension Id: Thigh Tangent Angle Rotorcraft Max
Aircraft Applicability: Rotorcraft
Description: Thigh Tangent Angle Maximum for Rotorcraft
Figure Ref: Figure 2
Para Ref: Figure 2 Note 1
Qualifier: Max
Standard: MIL-Std-1333B
Unit: Degrees
Value in (inches or degrees (see unit column)): 10

Source: MIL-STD-1333B

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