Titanium, 100° Intermediate Crown Head for Shear/Tension Metallic/Composite Applications
| Items |
 XPL4BC-V05-( ) XPL4BC (05-16) |
XPL4BC-V05-( )ACB XPL4BC (05-16) |
XPL4BC-V05-( )AD XPL4BC (05-16) |
XPL4BC-V05-( )AS XPL4BC (05-16) |
XPL4BC-V05-( )B XPL4BC (05-16) |
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| Part Family | XPL | |||||||||
| Head Style | 100° Flush | |||||||||
| Type | Shear/Tension | |||||||||
| Application | Metallic/Composite | |||||||||
| Pintail Configuration | Standard Pintail | |||||||||
| Material | 6Al-4V Titanium Alloy per AMS4967, 95KSI Minimum Shear Strength | |||||||||
| Finish Description | Uncoated Pin plus cetyl alcohol lube per MIL-L-87132 | Aluminum Coat (Kalgard 2242 or Hi-Kote 1) per NAS4006 identified by blue color on pintail end, plus cetyl alcohol lube per MIL-L-87132. | Aluminum Coat (Kalgard 2245) per NAS4006 plus cetyl alcohol lube per MIL-L-87132. Optional to color pintail end white. | Sulphuric Acid Anodize (Blue) per ISO 8080, plus cetyl alcohol lube per MIL-L-87132 | Uncoated Pin and no lubrication | |||||
| Sealant Escape Groove | No | |||||||||
| Nominal Size | 0.1640 | |||||||||
|
A Shank Dia +.0005 -.0000 |
0.1630 | 0.1630 | 0.1630 | |||||||
|
A Shank Dia Coated ±.0005 |
0.1630 | 0.1630 | ||||||||
| (B) Theoretical Dia Nom | 0.2765 | |||||||||
| (C) Head Height Nom | 0.0476 | |||||||||
|
F Flat Dia ±.005 |
0.125 | |||||||||
|
G Gage Dia ±.0001 |
0.2027 | |||||||||
| H Gage Height Max | 0.0350 | |||||||||
| H Gage Height Min | 0.0318 | |||||||||
| J Max | 0.010 | |||||||||
| (L) Ref | 0.124 | |||||||||
| M Max | 0.156 | |||||||||
| P Dia. Max | 0.156 | |||||||||
|
R Rad ±.005 |
0.020 | |||||||||
| S | 0.0045 | |||||||||
| (T) Ref | 0.207 | |||||||||
| Mating Collar Part Number | XBF-LV05 | |||||||||
| Minimum Double Shear Strength, pounds | 4010 | |||||||||
| Minimum Ultimate Tensile Strength, pounds | 1700 | |||||||||
| Typical Tensile Strength, pounds | 1785 | |||||||||
| Pin Position Swage Gauge | HG162-05 | |||||||||
| Minimum Grip Length Number | 3 | |||||||||
| Maximum Grip Length Number | 35 | |||||||||
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