FSC 2840 Aircraft Prime Moving Gas Turbines and Jet Engines and: 2840-00-005-6772, 2840-00-006-5308, 2840-00-007-8163
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 2840-00-005-6772 2840000056772 | 702815 | Disk, Compressor, Aircraft gas Tur | III End Item Identification: J57 aircraft engine Criticality Code Justification: AGAV Engine Section Location: Compressor | United Technologies Corporation (77445) | |
| 2840-00-005-6773 2840000056773 | 702305 | Disk, Compressor, Aircraft gas Tur | United Technologies Corporation (77445) | ||
| 2840-00-005-6775 2840000056775 | 701506 | Disk, Compressor, Aircraft gas Tur | United Technologies Corporation (77445) | ||
| 2840-00-005-6776 2840000056776 | 701607 | Disk, Compressor, Aircraft gas Tur | III End Item Identification: J57 aircraft engine Criticality Code Justification: AGAV Engine Section Location: Compressor | United Technologies Corporation (77445) | |
| 2840-00-005-6777 2840000056777 | 702609 740809 | Disk, Turbine, Aircraft gas Turbin | Engine Section Location: Compressor Special Features: Steel, ams 6415, rockwell C35-40 hardness, 1.354-1.365 in. thk, 20.017-20.027 in. od, 11.995-12.005 in. id, 103 blade slots equallyspaced around od, sixteen 0.437-0.440 in. holes equally spaced on 8.000IN. centerline radius, 32 scallops equally spaced on 7.260 in.centerline radius, thirty-two 0.108-0.113 in. holes equally spaced ON7.260 in. centerline radius Material: Steel overall | United Technologies Corporation (77445, 52661) | |
| 2840-00-006-2791 2840000062791 | 701608 | Disk, Turbine, Aircraft gas Turbin | Engine Section Location: Compressor Special Features: Rockwell C35-40 hardness; 1.482-1.493 inch thickness; 19.825-19.835 inch od; 101 blade slots equally spaced around od; 16 0.4205-0.4235 inch holes equally spaced on 8 inch centerline radius; 16 0.437-0.440 inch holes equally spaced on 8.0 inch centerline radius Material: Steel overall | United Technologies Corporation (77445, 52661) | |
| 2840-00-006-5098 2840000065098 | 2004T99P07 | Roller, Actuating | General Characteristics Item Description: Used on J85-GE-21 engine | General Electric Company (99207) | |
| 2840-00-006-5099 2840000065099 | 3902T00P07 5019T23P03 | Hanger, Afterburner Liner | General Characteristics Item Description: Used on J85 engine | General Electric Company (99207) | |
| 2840-00-006-5100 2840000065100 | 6008T09P02 3902T00P19 | Hanger, Afterburner Liner | General Characteristics Item Description: Used on J85 engine | General Electric Company (99207) | |
| 2840-00-006-5299 2840000065299 | 675797 | Poppet, Valve, Breath | General Characteristics Item Description: Stainless steel, ams 5616, 1.690-1.710 in. overall od, two 0.126-0.127IN. pin holes located on stem 1.275-1.285 in. hole center to holecenter, four 0.120-0.130 in. holes equally spaced around disk, 1.440-1.460IN. id of conical disk, rockwell C45-50 hardness III Fsc Application Data: Airdraft jet engine, TF30 | United Technologies Corporation (77445) | |
| 2840-00-006-5305 2840000065305 | 701708 | Disk, Compressor, Aircraft gas Tur | United Technologies Corporation (77445) | ||
| 2840-00-006-5308 2840000065308 | 754901 701701 | Disk, Turbine, Aircraft gas Turbin | Engine Section Location: Compressor Special Features: Steel, ams 6415, rockwell C35-40 hardness, 3.210-3.221 in. thk, 19.825-19.835 in. od, 6.995-7.005 in. id, 27 blade slots equally spacedaround od, sixteen 0.437-0.440 in. holes equally spaced on 8.000 in.centerline radius, thirty-two 0.101-0.113 in. holes equally spaced ON7.260 in. centerline radius, thirty-two scallops equally spaced on 7.260IN. centerline radius Material: Steel overall | United Technologies Corporation (77445) | |
| 2840-00-006-5309 2840000065309 | 701604 | Disk, Turbine, Aircraft gas Turbin | Engine Section Location: Compressor Special Features: Steel, ams 6415, rockwell C35-40 hardness, 2.028-2.039 in. thk, 19.825-19.835 in. od, 7.995-8.005 in. id, 51 blade slots equally spacedaround od, sixteen 0.4205-0.4235 in. holes equally spaced on 9.000 in.centerline radius, sixteen 0.437-0.440 in. holes equally spaced on 9.000IN.CENTERLINE radius Material: Steel overall | United Technologies Corporation (77445) | |
| 2840-00-006-5311 2840000065311 | 701513 701413 759313 | Disk, Compressor, Aircraft gas Tur | III End Item Identification: J57 aircraft engine Criticality Code Justification: AGAV Engine Section Location: Compressor | United Technologies Corporation (77445) | |
| 2840-00-007-1436 2840000071436 | 3019920 | Coupling Pressure, Pump | General Characteristics Item Description: Steel, 5.515 in. lg, 1.9900 in. dia, spur gear one end 17 teeth, 0.9020 in. ditch dia | Pratt and Whitney Canada Inc. (00198) | |
| 2840-00-007-5636 2840000075636 | 6870726 | Nozzle Segment, Turbine, Aircraft | III End Item Identification: Aircraft engine model T56 | Allison Transmission Inc. (73342) | |
| 2840-00-007-5637 2840000075637 | 6870727 | Vane, Turbine Nozzle, Turbine Engi | Allison Transmission Inc. (73342) | ||
| 2840-00-007-5638 2840000075638 | 6870728 | Vane, Turbine Nozzle, Turbine Engi | Allison Transmission Inc. (73342) | ||
| 2840-00-007-5639 2840000075639 | 6870729 | Nozzle Segment, Turbine, Aircraft | III End Item Identification: Model T56 engine | Allison Transmission Inc. (73342) | |
| 2840-00-007-8163 2840000078163 | 1-300-124-04 43338 | Coil-cable Assembly | General Characteristics Item Description: Four output connections, lgth excluding terminations, first lgth max 47.875 in. min 47.125 in., second lgth max 21.125 in. min 20.375 in., replaceable ceramic insulators, snap rings and end terminals Reference Number Differentiating Characteristics: As differentiated by replaceable parts | Honeywell International Inc. (91547) Unison Industries LLC (59501, 83311) |