NSN 5305-01-269-6088

Part Details | PANEL SCREW ASSEMBLY

5305-01-269-6088 A headed, threaded fastening device over which may be assembled; (1) a stand-off; (2) a flanged bushing with washer(s) and/or a shouldered bushing without a flange, or it may have an internally threaded sleeve that is an integral part of the screw; a washer and an externally thread self-locking bushing that is driven by an inserted driver. Attached to panel by threaded bushing or by flaring end of stand-off, or bushing. Used in conjunction with a speed nut, nut plate, or driven into a threaded hole in the item that the panel is fastened to. May be spring loaded.

Alternate Parts: 139742011, 13974-201-1, 139742011, 13974-201-1, 5305-01-269-6088, 01-269-6088, 5305012696088, 012696088

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
53DEC 18, 198701-269-608833044 ( SCREW ASSEMBLY, PANEL )
REFERENCE DRAWINGS & PICTURES

HEXAGON COUNTERSUNK

CROSS RECESS TYPE 1

Cross Reference | NSN 5305-01-269-6088
Part Number Cage Code Manufacturer
13974-201-194756BOEING COMPANY, THEDBA BOEING
13974-201-118118TOLO INCDBA BF GOODRICH AEROSPACE TOLO
Technical Data | NSN 5305-01-269-6088
Characteristic Specifications
THREAD SERIES DESIGNATOR UNC
NOMINAL THREAD DIAMETER0.164 INCHES
THREAD QUANTITY PER INCH32
THREAD CLASS2A
THREAD DIRECTION RIGHT-HAND
THREAD LENGTH0.250 INCHES NOMINAL
FASTENER LENGTH0.625 INCHES NOMINAL
HEAD STYLE0 HEXAGON COUNTERSUNK
HEAD DIAMETER0.335 INCHES MAXIMUM
COUNTERSINK ANGLE99.0 DEGREES MINIMUM AND 101.0 DEGREES MAXIMUM
INTERNAL DRIVE STYLE CROSS RECESS TYPE 1
MATERIAL ACCOMMODATED THICKNESS0.100 INCHES MINIMUM AND 0.107 INCHES MAXIMUM