5305-12-185-9734

Machine Screw

5305121859734 121859734 DIN920-M2X4-2.0770 161017 DIN920M2X4-2-0770 M2X4DIN920-2-0770

An externally threaded fastener whose threaded portion is of one nominal diameter, No 0 (0.060 in./1.5 mm) or larger, designed to be held or driven with either a wrench or an inserted driver or both (excluding internal socket or internal multiple spline types), in sizes below No. 10 (0.190 in./5 mm). No. 10 and larger sizes must have a head designed for any type inserted driver (excluding internal socket or internal multiple spline types), but may also be designed for external wrenching. A locking feature may be incorporated in the design of the head or threads. Excludes BOLT, CLEVIS; BOLT, EXTERNALLY RELIEVED BODY; SCREW, EXTERNALLY RELIEVED BODY; and SCREW, ASSEMBLED WASHER. See also, SCREW, INSTRUMENT; BOLT, MACHINE; BOLT, INTERNAL WRENCHING; and SCREW, CAP SOCKET HEAD. View more Machine Screw

5305-12-185-9734 SCREW,MACHINE 5305121859734 121859734

Managed by Germany
NSN Created on 13 Nov 1980
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
5305-12-185-9734 SCREW,MACHINE 5305121859734 121859734 1/1
NSN 5305-12-185-9734 (Generic Image) 1/1

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1610-17-102-3014 1610171023014 171023014 is an item or items employed individually or conjunctively to modify aircraft components.
1610-17-112-0016 1610171120016 171120016 is a propeller designed to provide thrust for a fixed or tilt wing aircraft. it may be of solid or built-up construction; constant or controllable speed type; adjustable, fixed or variable pitch design with reversing and/or feathering capabilities during aircraft operation. variable pitch propellers have integral facilities for changing the pitch angle of the blades while aircraft is in flight. excludes hub-blade assembly, propeller, aircraft. see also test club.
1610-17-124-2389 1610171242389 171242389 is a propeller designed to provide thrust for a fixed or tilt wing aircraft. it may be of solid or built-up construction; constant or controllable speed type; adjustable, fixed or variable pitch design with reversing and/or feathering capabilities during aircraft operation. variable pitch propellers have integral facilities for changing the pitch angle of the blades while aircraft is in flight. excludes hub-blade assembly, propeller, aircraft. see also test club.
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