Howmet
Head Style |
N/A Protruding Shear |
Type |
N/A Shear |
Material |
N/A 6AI-4V Titanium alloy per AMS 4928 or 4967. |
Finish and Lubricant |
N/A Cetyl alcohol |
Nominal Diameter |
N/A 3/8 in |
Thread Size |
N/A 0.3750-24 UNJF-3A |
External Thread - Major Diameter |
N/A 0.3620-0.3680 in |
External Thread - Pitch Diameter |
N/A 0.344 in |
A |
N/A 0.565-0.600 in |
D |
N/A 0.3740-0.3745 in |
F |
N/A 0.040 in |
H |
N/A 0.078-0.088 in |
R |
N/A 0.020-0.030 in |
Chamfer |
N/A 3/64" x 45° |
W |
N/A 0.1582-0.1617 in |
T |
N/A 0.150-0.180 in |
Y |
N/A 0.207 in |
Minimum Double Shear, pounds |
N/A 21000.000 lb |
Tension Pounds Minimum |
N/A 8700.000 lb |
Notes |
N/A
1. Dimensions, unless otherwise noted: in inches; apply after finish. 2. Surface texture per ASME B46.1. 3. "A" diameter is concentric to "D" diameter within 0.010 TIR. 4. Flute location ("K" dimanesion) and geometry are inspected per HFS specification E106. 5. Threads must accept a AS8879 "GO" ring gage to assure free running nut capability. AS8879 limits do not apply to threads in the fluted portion of the thread, the minor and pitch diameters may be up to 0.00 below AS8879 minimum values and major diameter may be up to 0.002 below sheet 1 values for a distance equal to the flute length plus 1.5P Max. 6. Blended radius transition permits use in interference fit application. 7. See table I. 8. Pins shall be packaged in clear sealed plastic bags from the original manufacturer (no repackaging allowed). Each bag shall contain a maximum of 100 pins for 5 and 6 diameter. 50 pins per bag for 8 and 10 diameters, 25 pins per bag for 12 diameter. Each bag shall be marked with "EDDIE-BOLT® 2 PIN", purchaser´s and manufacturer´s complete part number, manufacturer´s lot number, manufacturer´s or distributor´s name and the "pack" date. 9. For dimensions not shown, see sheets 1 and 2. 10. For material, finish and lube information, see sheets 1 and 2. 11. For dimensions not shown, see sheets 1 and 2. 12. For material and finish and lube information, see sheets 1 and 2. 13. See table II |
