Part number 114s2868-3 is in stock in the following quantities and conditions.
Note: Availability of this item was last updated 02/13/2024 and may have changed since then. Request a quote for up to date pricing and availability.
Part Information
Chrome-molybdenum, mil-s-5626, comp 4140 cond f o/a, casehardened, rockwell c scale 35.0 min, 40.0 maximum hardness of body, 55.0 min, 60.0 maximum hardness of teeth, webbed, protruding shaft ends unequal lg, web offset from gear teeth centerline, 5.000 in. O/a lg, 2.383 in. Od gear, 2.300 in. Pitch dia, 0.897 min-0.899 maximum in. W of face, 2.370 in. Distance from 1st end shaft to face of gear, 1.731 min-1.733 maximum in. Distance from 2nd end shaft to face of gear, 1st end dim., 0.748 min-0.749 maximum in. Shaft dia, 1.122 min-1.124 maximum in. Lg from end of shaft to 1st groove, 0.701 min-0.707 maximum in. Dia, 0.046 min-0.049 maximum in. Of w of 1st groove, 0.7501 min-0.7504 maximum in. Dia, 0.667 min-0.672 maximum in. Lg of 1st step, 0.651 min-0.661 maximum in. Dia, 0.530 in. Lg of 2nd step, 2nd end dim: 0.748 min-0.749 maximum in. Shaft dia, 1.118 miin-1.122 maximum in. Lg from end of shaft to 1st groove, 0.701 min-0.707 maximum in. Dia, 0.046 min-0.049 maximum in. W of groove, 0.750
Part Number | RNVC | RNAAC | DAC | CAGE |
---|---|---|---|---|
114S2868-3 | 2 | XX | X | 81205 |
114S2868-3 | 2 | XX | X | 77272 |
114S2868-3 | 2 | XX | X | 81205 |
114S2868-3 | 2 | XX | X | 77272 |
Code | Definition |
---|---|
FN | Factory New. Parts manufactured by then OEM and includes manufacturer certification. |
NE | New. Parts manufactured by the OEM. May include manufacturer certification or company certification. |
NS | New Surplus. New material item purchased from excess inventory. |
OH | Overhauled. Product has been rebuilt and tested in accordance with the manufacturer's specifications by a repair shop (MRO). |
SV | Serviceable product. |
AR | As Removed. Product removed from aircraft or platform with no guarentee on the functionality of the part. |
RP | Repairable. Product can be repaired by a MRO and be given a FAA 8130 or EASA Form 1 certification. |