Aircraft Prime Moving Gas Turbines and Jet Engines and Components: 23052961, 23053320, 23053420
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 23052961 | 2840-01-497-3920 | Cushion, Aircraft, Ma | III End Item Identification: KC130J aircraft engine AE2100D3 Criticality Code Justification: AGAV | Rolls Royce Corp. (1E0F1) | |
| 23052969-03 2305296903 | 2840-01-393-2940 | SEAL | Rolls-Royce Corporation (63005) | ||
| 23052969-04 2305296904 | 2840-01-393-2941 | SEAL | Rolls-Royce Corporation (63005) | ||
| 23052969-05 2305296905 | 2840-01-393-4908 | SEAL | Overall Height: 0.123 inches minimum and 0.127 inches maximum Overall Diameter: 8.225 inches minimum and 8.235 inches maximum Special Features: Material ams 5596 per 718 inconel;i.D. 7.982 in. nom. | Rolls-Royce Corporation (63005) | |
| 23052980 | 2840-01-497-3924 | Bearing, Aircraft, Ma | III End Item Identification: KC130J aircraft engine AE2100D3 Criticality Code Justification: AGAV | Rolls Royce Corp. (1E0F1) | |
| 23053 | 2840-00-079-4085 | Control Assy, Feedba | Satair A/S (R1120) Triumph Controls LLC (78710) | ||
| 23053000 | 2840-01-497-3929 | Tube as, Aircraft, Ma | III End Item Identification: KC130J aircraft engine AE2100D3 Criticality Code Justification: AGAV | Rolls Royce Corp. (1E0F1) | |
| 23053001 | 2840-01-463-8679 | Gearbox, Assy, Acc D, | End Item Identification: Allison engine (AE1107C) Criticality Code Justification: AGAV | Rolls Royce Corp. (1E0F1) | |
| 23053014 | 2840-01-470-1497 | Cover Assembly, Airc | Rolls Royce Corp. (1E0F1) | ||
| 23053032 | 2840-01-470-1494 | Cover Assembly, Airc | Rolls Royce Corp. (1E0F1) | ||
| 23053112 | 2840-01-497-3931 | Bracket, Aircraft, Ma | III End Item Identification: KC130J aircraft engine AE2100D3 Criticality Code Justification: AGAV | Rolls Royce Corp. (1E0F1) | |
| 23053176 | 2840-01-191-7811 | Valve Assy, Bleed | III End Item Identification: T63-A-700 and T63-A-720 (turbine engine), rotary wing aircraft | Allison Transmission Inc. (73342) Rolls-Royce Corporation (63005) | |
| 23053293 | 2840-00-940-9467 | Reducer, Oil Pressur | III End Item Identification: T63-A-700 & T63-A-720 turbine engine | Allison Transmission Inc. (73342) Rolls-Royce Corporation (63005) | |
| 23053301 | 2840-01-514-2142 | Engine, gas Turbine, Aircraft | III Part Name Assigned By Controlling Agency: 250-C20R4 engine assembly | Allison Transmission Inc. (73342) | |
| 23053311 | 2840-01-334-1211 | Modification kit, Engine | End Item Identification: T63 series engine | Rolls-Royce Corporation (63005) | |
| 23053320 | 2840-01-038-1212 | Sump, Scavenge Oil | General Characteristics Item Description: Cres, 10 psig pressure test per E151880 | Rolls-Royce Corporation (63005) | |
| 23053355 | 2840-01-502-4479 | Lock Ring, Turbine Nozzle, Aircraf | III End Item Identification: Model A31107 and model T406-AD-400 and model AE2100A, C and AE2100D2, D3, J aircraft engine III Part Name Assigned By Controlling Agency: Ring, locking, power turbine | Rolls-Royce Corporation (63005) | |
| 23053372 | 2840-01-497-3935 | Bracket as, Aircraft | III End Item Identification: KC130J aircraft engine AE2100D3 Criticality Code Justification: AGAV | Rolls Royce Corp. (1E0F1) | |
| 23053375 | 2840-01-497-3937 | Insert, Aircraft, Mat | III End Item Identification: KC130J aircraft engine AE2100D3 Criticality Code Justification: AGAV | Rolls Royce Corp. (1E0F1) | |
| 23053420 | 2840-01-497-3951 | Insert, Aircraft, Mat | III End Item Identification: KC130J aircraft engine AE2100D3 Criticality Code Justification: AGAV | Rolls Royce Corp. (1E0F1) |