Model: 1441M62P01
Aircraft Compressor Rotor SpacerSpecial Features:
1.3680-1.3620 in. Of length is tapered to an outside diameter of 6.4100-6.4120 in. And an inside diameter of 6.2450-6.2550 in.; tapered edge has 6 equally spaced prongs projecting internally w/bolt holes centrally located on each prong w/dia of 0.2620-0.2690 in., prongs are 0.5900-0.6100 in. Wide and 0.6435-0.6475 in. Long; at beginning of taper 6 equally spaced notches are located 0.2400-0.2600 in. Wide and 0.4450-0.4550 in. Long projecting internally; opposite of tapered end are 6 equally spaced prongs projecting internally w/bolt holes centrally located on each prong w/dia of 0.2620-0.2690 in. And chamfered 0.0250-0.0350 in., 45 deg; all bolt holes have 63.0 microinch finish
Properties:
A rigid item designed to maintain a predetermined space between two rotor, compressor, aircraft gas turbine engine. It may be a complete 360 degrees or a section thereof.
Part 1441M62P01 NSN 2840-01-320-0704
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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