Model: 1-190-036-01
Aircraf Component Mounting PlateSpecial Features:
Rockwell 30t scale 76 max hardness, 0.840 in. Nom lg, 0.420 in nom w, 0.240 in nom o/a h, 0.040 in nom shoulder located on one end, 0.040 in nom h shoulder, 0.220 in nom diameter hole located on shoulder end, 0.210 in nom distance to hole center from edge along lg, 0.020 in nom distance to hole center from edge along w, 0.047 in min, 0.062 in max diameter hole through corner on shoulder end, 25 degrees min, 35deg max angle of corner hole on ll edge, 0.093 in min, 0.125 in from corner, 0.093 in min, 0.125 in max distance to corner hole center from corner, 0.093 in min, 0.125 in max distance to hole center from bottom edge along h, 0.165 in on end oppsite shoulder, 0.176 in min, 0.196 in max radius of slot end, 69 degrees min, 79 degrees max angle chamfer of slot w/shoulder of slot radius on side w/shoulder, 85 degrees min, 95 degrees max angle chamfer of slot radius on side oppsite shoulder
Properties:
A metallic item of various shapes designed to reduce vibration and to secure a component part of an engine, gas turbine, aircraft to the engine case or housing as modified. for mounting accessories to the outside of the engine, see plate, mounting.
Part 1-190-036-01 NSN 2840-01-010-5941
Material Classification
Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicatorsPackaging & Shipping
Freight Classification
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Schedule B and Export
- Schedule B: 8411997050
- SITC: 71499
- End Use: Engines and turbines for military aircraft
- NAICS: 336412
- USDA: 1
Freight Class: Parts of gas turbine aircraft engines, other than for use in civil aircraft
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