|Part No. : LE111-0001-3014||Manufacturer : Boeing Co The||CAGE Code : 43999|
|NSN : 5305-01-187-5839||Item Name : Screw Close Tolerance|
|Alternate P/N : LE11100013014||FSC : 5305 Screws|
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|AASA||THREAD LENGTH||0.425 INCHES MINIMUM AND 0.465 INCHES MAXIMUM|
|AASB||FASTENER LENGTH||1.310 INCHES MINIMUM AND 1.330 INCHES MAXIMUM|
|AASK||HEAD STYLE||PAN NO. 2|
|AASL||HEAD DIAMETER||0.360 INCHES MINIMUM AND 0.374 INCHES MAXIMUM|
|AASU||HEAD HEIGHT||0.115 INCHES MINIMUM AND 0.125 INCHES MAXIMUM|
|AAUR||GRIP DIAMETER||0.1890 INCHES MINIMUM AND 0.1895 INCHES MAXIMUM|
|ABQZ||INTERNAL DRIVE STYLE||HEXAGON|
|AHYM||NOMINAL THREAD DIAMETER||0.190 INCHES|
|ANEE||GRIP LENGTH||0.865 INCHES MINIMUM AND 0.885 INCHES MAXIMUM|
|ASDB||WIDTH ACROSS FLATS||0.125 INCHES MINIMUM AND 0.127 INCHES MAXIMUM|
|CMLP||THREAD QUANTITY PER INCH||32|
|CQBC||MINIMUM TENSILE STRENGTH||180000 POUNDS PER SQUARE INCH|
|CSYM||SURFACE FINISH||32.0 MICROINCHES BEARING SURFACE OF HEAD|
|FEAT||SPECIAL FEATURES||3 KEYWAYS 1.280 IN. MIN. AND 1.300 IN. MAX. LONG AND 0.030 IN. MIN. AND 0.034 IN. MAX. WIDE MACHINED IN SHANK. BORE MACHINED IN THREAD END TO RECEIVE PLUG|
|MATT||MATERIAL||IRON ALLOY 660 OVERALL|
|MDCL||MATERIAL DOCUMENT AND CLASSIFICATION||AMS 5732 FED SPEC SINGLE MATERIAL RESPONSE OVERALL|
|SFTT||SURFACE TREATMENT||PASSIVATE OVERALL|
|STDC||SURFACE TREATMENT DOCUMENT AND CLASSIFICATION||QQ-P-35 FED SPEC SINGLE TREATMENT RESPONSE OVERALL|
|THSD||THREAD SERIES DESIGNATOR||UNJF|
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