Part No. : HL6487W10 9 | Alternate P/N : HL6487W109 | Manufacturer : Lisi Aerospace Canada Corp |
CAGE Code : L4528 | Item Name : Pin Rivet | FSC : 5320 Rivets |
NSN : 5320-01-527-1345 |
You can send a request for quote for p/n HL6487W10 9 to ASAP Semiconductor using justpartsunlimited.com. This part is manufactured by Lisi Aerospace Canada Corp (CAGE Code L4528). The description of it is Pin Rivet. The national stock number associated with this part is NSN 5320015271345. This part belongs to FSC Rivets part family. An associate from ASAP Semiconductor will respond within 15 minutes to your query. It is our pleasure to help you with HL6487W10 9 part requirements.
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MRC | Criteria | Characteristic |
---|---|---|
AAZF | Shank Style | STUMP |
ABAJ | Lubrication | CETYL ALCOHOL, SPEC 305, HI-SHEAR CORP |
CWBJ | Collar Style | THREADED BREAK OFF TYPE |
CQJX | Nominal Thread Size | 0.328 INCHES |
SFTT | Surface Treatment | CADMIUM OVERALL |
ABAA | Collar Outside Diameter | 0.512 INCHES MINIMUM AND 0.518 INCHES MAXIMUM |
ABCJ | Collar Inside Diameter | 0.330 INCHES MINIMUM AND 0.336 INCHES MAXIMUM |
AAJD | Thread Class | 3A |
AGAV | End Item Identification | CH-53G-HELICOPTER |
ABAB | Collar Overall Height | 0.652 INCHES MINIMUM AND 0.672 INCHES MAXIMUM |
AASK | Head Style | COUNTERSUNK W/REVERSE CHAMFER |
AASU | Head Height | 0.098 INCHES MINIMUM AND 0.112 INCHES MAXIMUM |
AAZE | Shank Diameter | 0.2016 INCHES MINIMUM AND 0.2026 INCHES MAXIMUM |
THSD | Thread Series Designator | UNJF |
MATT | Material | STEEL BODY |
MDCL | Material Document And Classification | MIL-S-562 MIL SPEC SINGLE MATERIAL RESPONSE BODY OR MIL-S-6049 MIL SPEC SINGLE MATERIAL RESPONSE BODY |
AAZG | Head Major Diameter | 0.357 INCHES MINIMUM AND 0.377 INCHES MAXIMUM |
ANEE | Grip Length | 0.562 INCHES NOMINAL |
CMLP | Thread Quantity Per Inch | 24 |
STDC | Surface Treatment Document And Classification | QQ-P-416, TY II, CL2 FED SPEC ALL TREATMENT RESPONSES BODY |
CRSQ | Countersink Angle | 100.0 DEGREES NOMINAL |
MRC | Decoded Requirement | Clear Text Reply |
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