Sheet Spring Instrument Mounting Nut - Panel Thickness: 0.312", Thread: 6-32

Detail Characteristic
END ITEM IDENTIFICATIONHELICOPTER, SEAHAWK, H-60;AIRCRAFT, STRATOLIFTER C-135;HELICOPTER, LAMPS MARK III, SH-60B;AIRCRAFT, T-38;AIRCRAFT, HARRIER AV-8B
NUT HEIGHT0.678 INCHES MINIMUM AND 0.698 INCHES MAXIMUM
NUT STYLESHEET SPRING
NUT WIDTH0.271 INCHES MINIMUM AND 0.291 INCHES MAXIMUM
NUT LENGTH0.661 INCHES MINIMUM AND 0.681 INCHES MAXIMUM
PANEL THICKNESS0.302 INCHES MINIMUM AND 0.322 INCHES MAXIMUM
MATERIAL THICKNESS0.002 INCHES MINIMUM AND 0.022 INCHES MAXIMUM
MATERIALCOPPER ALLOY OVERALL
MATING MEMBER DIAMETER ACCOMMODATED0.138 INCHES NOMINAL
SURFACE TREATMENT DOCUMENT AND CLASSIFICATIONQQ-P-416,TYPE 1,CLASS 2 FED SPEC 1ST TREATMENT RESPONSE OVERALL OR QQ-Z-325 FED SPEC 2ND TREATMENT RESPONSE OVERALL OR QQ-Z-325 FED SPEC 3RD TREATMENT RESPONSE OVERALL OR QQ-Z-325 FED SPEC 4TH TREATMENT RESPONSE OVERALL OR QQ-Z-325 FED SPEC 5TH TREATMENT RESPONSE OVERALL
SURFACE TREATMENTCADMIUM OVERALL OR ZINC OVERALL AND CHROMATE OVERALL OR ZINC OVERALL AND PHOSPHATE OVERALL

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Unit of Measure

Discount Table - MS33737-14C

Unit
Discount Price / %
50 - 99
$2.81
100 - 499
$2.75
500 - 999
$2.59
1000   and up
$2.36

Inventory

N/A {1531}

Estimated Ship Date

N/A Ships in 1 Business Day

Inventory Note

N/A Need additional stock? Call (877) 920-1876 or email

Industry Standards/Certification

N/A MS33737

Panel Thickness

N/A 0.312 in

Weight

N/A .004 lb

Maximum Dimension A

N/A 0.688 in

Part Number for Reference Only

N/A NAS487-18

Alternate Part Number

N/A A8942-632-24J

NSN

N/A 5310-00-928-3878

NIIN

N/A 00-928-3878

Part # Unpunctuated

N/A MS3373714C

Minimum Order Note

N/A Minimum order is 10. Must order in increments of 1.

Note

N/A Our inventory is extensive. The majority of the items listed in our catalog are stocked and available for immediate shipment.

California Residents

N/A Prop 65 Warning: This product may contain chemicals known to the State of California to cause cancer, and birth defects or other reproductive harm.