Mfg Part Number: BACP18C3 660
Alternate P/N: BACP18C3660
NSN : 5315-01-520-7274
NIIN : 015207274
CAGE Code : 81205
Manufacturer: The Boeing Company
Item Name : Pin Straight Headle
Here at Internet For Aviation, we have BACP18C3 660 Pin Straight Headle from The Boeing Company, as well as a variety of other parts from reliable manufacturers. As the only independent distributor with a No China Sourcing policy, we go to great lengths to ensure that we source responsibly when it comes to certified standard items. If you’re in need of a specific BACP18C3 660 to aid you in your aircraft repair capabilities, simply search by NSN part number, NSN or Cage Code on our parts directory. Submit an instant RFQ and a representative will get back to you in as little as 15 minutes.
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| MRC | Criteria | Characteristic |
|---|---|---|
| SFTT | SURFACE TREATMENT | CADMIUM OVERALL AND CHROMIUM OVERALL |
| ACHU | PIN OVERALL DIAMETER | 0.1860 INCHES MINIMUM AND 0.1900 INCHES MAXIMUM |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | ASTM A108 ASSN STD ALL MATERIAL RESPONSES OVERALL |
| ABRC | FIRST HOLE DIAMETER | 0.068 INCHES MINIMUM AND 0.078 INCHES MAXIMUM |
| CQBB | SECOND END RELATIONSHIP WITH FIRST END | IDENTICAL |
| ABRE | DISTANCE FROM CENTERLINE OF HOLE TO END OF PIN | 0.120 INCHES MINIMUM AND 0.130 INCHES MAXIMUM |
| ACHT | PIN OVERALL LENGTH | 6.600 INCHES MINIMUM AND 6.610 INCHES MAXIMUM |
| MATT | MATERIAL | STEEL COMP 1020 OR STEEL COMP 1025 OVERALL |
| AAGZ | FIRST END STYLE | CHAMFERED |
| CRMG | FIRST END TAPER ANGLE | 45.0 DEGREES NOMINAL |
| ABRD | SECOND HOLE DIAMETER | 0.068 INCHES MINIMUM AND 0.078 INCHES MAXIMUM |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | PIN, TWO HOLE |
| ABRF | CENTER TO CENTER DISTANCE BETWEEN HOLES | 6.360 INCHES NOMINAL |
| AMCS | FIRST END TAPER LENGTH | 0.045 INCHES NOMINAL |
| ABRB | HOLE ARRANGEMENT STYLE | BOTH END DRILLED |
| FEAT | SPECIAL FEATURES | WITH SCREWDRIVER SLOT ONE END ONLY |
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-P-416,TY 2,CL 2 FED SPEC SINGLE TREATMENT RESPONSE OVERALL |
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