Part Information
Requested name-shaft, motor; step 1 is 1.853 min. To 1.868 max. In. Longand 0.4990 min. To 0.4995 in dia. Ste p 2 is 0.2970 min. 0.3270 max. In. Long and 1.0613 min. To 1.0618 max. In. Iin dia. Step 3 is 0.1450 min. To 0.1600 max. In in dia. Step 4 is 0.1100 min. To 0.1400 max. In long and 1.4730 miin. To 1.4750 max. In. Dia. Step 5 is 0.6120 in. Long and 1.4330 min.To 1.4340 max. In. In dia. Step 6 is 0.3730 in long and 0.7810 in.In dia.Step 7 is 0.2850 min to 0.3150 in. Long and 0.6247 min. To 0.6250 max. In. In dia. Step 8 is 0.3770 in. Long and0.3120 in. In dia. Step 9 is 0.5470 min. To 0.5770 min. In. Long and 0.1875 min. To 0.1865 min. To0.1875 max. In. In dia. There is an .031 x 1.046 min. To .031 x 1.046 min undercut at the end of step 2, an .031 x 0.7660 min. To .031 x 0.7710 max. In. Undercut between step 5 and 6 and an .31 x 0.6200 min. To 0.6250 in. Maximum undercut at the end of step 8
Part Number | RNVC | RNAAC | DAC | CAGE |
---|---|---|---|---|
677159-3 | 2 | ZZ | 2 | 20418 |
677159-3 | 2 | ZZ | 5 | 98255 |
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. |