change location
321-802-5889
321-733-7477
Part Information
Steel black oxide; 20.0 min/25.0 maximum rockwell c harness rating; 5.980 in.Major complement dia; 3.281 in.Majorcomplement lg; 8.406 in.O/a lg; 5.750 in.X 0.250 in.W.Bearing seat 0.250 in.Fr first end; 5.928 in.Dia x 2.010 in. W.0.750 in.Fr first end; 5.750 in.Dia x 0.260 in.W.Bearing seat 2.900 in.Fr first end; 1.380 in.Dia x 3.938 in.Lg first step second end; 1.375-12acme-3c external thds 2.430 in.Lg first step second end; 1.260 in.Dia x 0.190 in.W. Thd relieve 2.430 in.Fr first step second end; 4.998 in.Dia x 1.187 in. Second step second end; 0.877 in.Dia through bore 8.406 in.Lg; 5.000 in.Dia x 2.530 in.Lg w/o.500 in.Radius cbore first end major complement body; 8/0.320 in.Dia x 0.310 in.Deep holes equally spaced on 2.750 in.Bolt hole circle 5.000 in.Dia cbore face; 2.000 in.Dia x 0.130 in.W. W/0.120 in.Raduiscbore 2.530 in.Fr first end; 1.104 in. Diameter x 0.304 in. W.Retainer seat 3.160 in.Fr first end on through bore dia
| Part Number | RNVC | RNAAC | DAC | CAGE |
|---|---|---|---|---|
| 12007751 | 2 | BF | 1 | 19204 |
| 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. |