2840-01-238-3622

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2840012383622 012383622,2185731,716241 Upgrade 2840-01-238-3622Aircraft Gas Turbine Engine Turbine
Rotor Blade2840012383622 012383622 2185731 716241 ROTOR,AIRCRAFT GAS TURBINE ENGINE 126 EA NS Request

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AssyUOMTechnical DocumentQuantative ExpressionDepartment of the Air Force (DF)LZDiscontinued-Use 2840-01-238-3622

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AssyUOMTechnical DocumentQuantative ExpressionDepartment of the Air Force (DF)LZDiscontinued-Use 2840-01-238-3622

5340-14-218-5731 5340142185731 142185731 is a forked part, having transverse hole(s) or slot(s) in each arm (prong) to accommodate a bolt, pin, or the like, and having a connection facility opposite the fork. it is designed to be attached to a shaft, rod, turnbuckle or the like by welding, threading, and/or pinning. may include provisions for locking. see also yoke, universal joint and connector, rod end. for items specifically designed for aviation, see clevis, rod end, aviation.

5998-01-218-5731 5998012185731 012185731 is a grouping of two or more physically connected or related electrical an/or electronic parts capable of dissassemblage. each component of the assemblage must be capable of functioning in accordance with its own item name. consists of a single printed circuit board or terminal board upon which are mounted separately manufactured electronic components such as capacitors, inductors, resistors, and the like. it may also include printed electronic components. the item is generally part of a subassembly and cannot be assigned a more definite item name. for items having a complete individual electrical/electronic function, use applicable item name such as amplifier (as modified); power supply; or the like. for items not having a complete individual electrical/electronic function, see applicable subassembly name, such as amplifier subassembly; power supply subassembly; or the like. for an assembly of electrical/electronic components mounted on other than a single printed wiring board, see electronic components assembly. excludes printed circuit boar