Mfg Part Number: BACP18C 3 310
Alternate P/N: BACP18C3310
NSN : 5315-01-464-1683
NIIN : 014641683
CAGE Code : 81205
Manufacturer: The Boeing Company
Item Name : Pin Straight Headle Pin Straight Headle
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NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
5315-01-464-1683 Item Description: Pin Straight Headle | 5315 | 014641683 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
BACP18C 3 310 | 5 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
AAGZ | FIRST END STYLE | CHAMFERED |
AAHP | SECOND END STYLE | CHAMFERED AND COUNTERBORED |
ABRB | HOLE ARRANGEMENT STYLE | BOTH END DRILLED |
ABRC | FIRST HOLE DIAMETER | 0.068 INCHES MINIMUM AND 0.078 INCHES MAXIMUM |
ABRD | SECOND HOLE DIAMETER | 0.068 INCHES MINIMUM AND 0.078 INCHES MAXIMUM |
ABRE | DISTANCE FROM CENTERLINE OF HOLE TO END OF PIN | 0.120 INCHES MINIMUM AND 0.130 INCHES MAXIMUM |
ABRF | CENTER TO CENTER DISTANCE BETWEEN HOLES | 2.770 INCHES MINIMUM AND 2.800 INCHES MAXIMUM |
ACHT | PIN OVERALL LENGTH | 3.100 INCHES NOMINAL |
ACHU | PIN OVERALL DIAMETER | 0.1860 INCHES MINIMUM AND 0.1900 INCHES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | C-135 |
AKTY | SECOND END COUNTERBORE DIAMETER | 0.037 INCHES MINIMUM AND 0.050 INCHES MAXIMUM |
AKVA | SECOND END COUNTERBORE DEPTH | 0.029 INCHES MINIMUM AND 0.045 INCHES MAXIMUM |
AMCS | FIRST END TAPER LENGTH | 0.030 INCHES NOMINAL |
AMFM | SECOND END TAPER LENGTH | 0.030 INCHES NOMINAL |
CQBB | SECOND END RELATIONSHIP WITH FIRST END | NOT IDENTICAL |
CRMG | FIRST END TAPER ANGLE | 45.0 DEGREES NOMINAL |
CTHC | SECOND END TAPER ANGLE | 45.0 DEGREES NOMINAL |
MATT | MATERIAL | STEEL COMP 1018 OVERALL OR STEEL COMP 1020 OVERALL OR STEEL COMP 1025 OVERALL |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | ASTM A 108 FED SPEC SINGLE MATERIAL RESPONSE OVERALL |
SFTT | SURFACE TREATMENT | CADMIUM OVERALL |
STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-P-416,TYPE II,CLASS 2 FED SPEC SINGLE TREATMENT RESPONSE OVERALL |
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