Steel Tool & Engineering Co. NSN Parts
| CAGE | Address | Type | Status |
|---|---|---|---|
| 21023 | 28005 FORT ST, TRENTON, MI, 48183-4909, UNITED STATES | A | A |
FSC 2835 Gas Turbines and Jet Engines; NON-Aircraft Prime Mover, Aircraft NON-Prime Mover, and Components
| MFG SKU | NSN | Item Name | Details | CAGE Code | RFQ |
|---|---|---|---|---|---|
| 9663M23G10 | 2835-01-093-1864 | Shroud, Stage 1 | 21023 | ||
| 966M224G19 | 2835-01-093-1865 | Shroud, Stage 2 | 21023 | ||
| 9663M24G22 | 2835-01-093-1866 | Shroud, Stage 3 | 21023 | ||
| 9663M69G20 | 2835-01-093-1868 | Shroud, Stage 5 | Part Name Assigned BY Controlling Agency: Shroud, low pressure turbine stator stage 2 thru 5 | 21023 | |
| 9663M70G11 | 2835-01-093-1869 | Shroud, Stage 6 | 21023 |
FSC 2840 Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
| MFG SKU | NSN | Item Name | Details | CAGE Code | RFQ |
|---|---|---|---|---|---|
| 9978M69G41 | 2840-01-146-9395 | Housing, Seal, Aircraft gas Turbin | Criticality Code Justification: AGAV Engine Section Location: Compressor Material: Steel overall | 21023 | |
| 4007T13P05 | 2840-00-832-3305 | Seal Segment, Turbine | End Item Identification: J-85 aircraft engine General Characteristics Item Description: Zsteel AMS5759 material of body, steel ams 5536 material ofhoneycomb, 64 deg 18 min segment, 4.114 in. inside radius, 4.164 in.outside radius of flange, 0.355 in. max H O/a, three 0.1665 in.dia holes spaced 20 deg C to C on 4.355 in. radius | 21023 | |
| 4011T06G07 | 2840-00-118-9649 | Seal, Air, Aircraft gas Turbine En | III End Item Identification: J85 aircraft engine Criticality Code Justification: AGAV Engine Section Location: Compressor | 21023 | |
| 9978M69G42 | 2840-01-146-9396 | Seal, Air, Aircraft gas Turbine En | III End Item Identification: Acft eng F101 Criticality Code Justification: Apgf and czbj and czcj and abhp and abmz Engine Section Location: Compressor | 21023 | |
| 9978M69G43 | 2840-01-146-9397 | Seal, Air, Aircraft gas Turbine En | III End Item Identification: F101, F108, F110, F118 acft eng Criticality Code Justification: AGAV Material: Steel overall | 21023 | |
| 9978M69G44 | 2840-01-188-3653 | Seal, Air, Aircraft gas Turbine En | III End Item Identification: F108 aircraft engine Criticality Code Justification: Abhp and apgf and czbj and czcj and feat Engine Section Location: Compressor | 21023 | |
| 5060T50G07 | 2840-01-346-9516 | Seal, Metallic, Aircraft gas Turbi | 21023 | ||
| 9978M69G40 | 2840-01-146-9394 | Seal, Metallic, Aircraft gas Turbi | III End Item Identification: Acft eng F101 Criticality Code Justification: AGAV Engine Section Location: Compressor | 21023 | |
| 9978M69G45 | 2840-01-147-2646 | Seal, Metallic, Aircraft gas Turbi | III End Item Identification: Acft eng F101 Criticality Code Justification: AGAV Material: Steel overall | 21023 | |
| 6020T00G01 | 2840-00-042-0038 | Shroud Assembly, Tu | General Characteristics Item Description: 1.180 in. min, 1.230 in. max lg | 21023 | |
| 6020T01G01 | 2840-00-042-0045 | Shroud Assembly, Tu | General Characteristics Item Description: Cres, 1.180 in. min, 1.230 in.max lg | 21023 | |
| 6020T03G01 | 2840-00-042-0031 | Shroud Assembly, Tu | General Characteristics Item Description: Cres, 1.070 in. min, 1.100 in. max lg | 21023 | |
| 6020T02G01 | 2840-00-033-7518 | Shroud Sector, Turbi | 21023 | ||
| 6020T04G01 | 2840-00-033-7489 | Shroud Sector, Turbi | 21023 | ||
| 6020T05G01 | 2840-00-033-7500 | Shroud Sector, Turbi | 21023 |
