Part Number: 11883-4-10/11883-4L10

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CONDITION:
NS
REID PRODUCTS INC.59563
BOEING COMPANY, THE76301
BOEING COMPANY, THE76301
VALLEY-TODECO, INC.6710
HEARTLAND PRECISION FASTENERS, INC.0ZC92
HOUSTON PRECISION FASTENERS I, LP1VSL7
BOEING COMPANY, THE76301
SPS TECHNOLOGIES, LLC56878
SPS TECHNOLOGIES, LLC6725
ARCONIC GLOBAL FASTENERS & RINGS, INC.6950
HUCK INTERNATIONAL, INC.17446
ARCONIC GLOBAL FASTENERS & RINGS, INC.1RC86
SPS TECHNOLOGIES, LLC27624
SPS TECHNOLOGIES, LLC56878
FASTENER INNOVATION TECHNOLOGY, INC.58998
HI-SHEAR CORPORATION73197
SPS TECHNOLOGIES, LLC80539
SPS TECHNOLOGIES LTD TJ BROOKS DIVISIONK5673
LISI AEROSPACE CANADA CORP DIV HI SHEAR HOLDINGS INCL4528
WEST COAST AEROSPACE INC60516
THREAD CLASS3A
THREAD DIRECTIONRIGHT-HAND
THREAD LENGTH0.444 INCHES MINIMUM AND 0.494 INCHES MAXIMUM
FASTENER LENGTH1.079 INCHES MINIMUM AND 1.109 INCHES MAXIMUM
HEAD STYLEOVAL COUNTERSUNK
HEAD DIAMETER0.3898 INCHES MINIMUM AND 0.3948 INCHES MAXIMUM
GRIP DIAMETER0.2485 INCHES MINIMUM AND 0.2495 INCHES MAXIMUM
INTERNAL DRIVE STYLEHIGH-TORQUE
END ITEM IDENTIFICATIONW/S: AIRCRAFT, PHANTOM F-4; AIRCRAFT, STRATOLIFTER C-135; AIRCRAFT, EAGLE F-15; AIRCRAFT, HARRIER AV-8B
NOMINAL THREAD DIAMETER0.250 INCHES
GRIP LENGTH0.615 INCHES MINIMUM AND 0.635 INCHES MAXIMUM
THREAD QUANTITY PER INCH28
COUNTERSINK ANGLE101.0 DEGREES NOMINAL
MATERIALSTEEL COMP XM-13 OVERALL
MATERIAL DOCUMENT AND CLASSIFICATIONAMS 5629 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
SURFACE TREATMENTALUMINUM OVERALL AND CHROMATE OVERALL
SURFACE TREATMENT DOCUMENT AND CLASSIFICATIONMIL-C-83488 TY 2 CL 3 MIL SPEC SINGLE TREATMENT RESPONSE OVERALL
THREAD SERIES DESIGNATORUNJF
A SCREW, MACHINE or SCREW, CAP, SOCKET HEAD whose unthreaded portion is of specified grip length, plated or unplated, and is machined to a tolerance of one thousandth ( . 1 IN.) ( . 25 mm) or less of a specific diameter for items (1. IN.) (25 mm) or less in diameter. Items over (1. IN.) (25 mm) in diameter shall have a tolerance of fifteen ten thousandths ( . 15 IN.) ( . 38 mm) or less. The nominal major diameter of the threads shall be at least one thousandth ( . 1 IN.) ( . 25 mm) below the minimum shank diameter, but not below the minimum major diameter for applicable class of fit, as shown in the Screw Thread Standards, FED STD H28 and/or other nationally recognized standards. The head is designed to be held or driven with an inserted driver. It is not designed for rotation by the thumb and fingers. A locking feature may be incorporated in the design of the head or threads.