FSC 2840 Aircraft Prime Moving Gas Turbines and Jet Engines and
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 2840-00-000-0048 2840000000048 | 2-001-020-14 T-55-L-11D | Engine, Aircraft, Turbo-Shaft | III End Item Identification: T-55 engines series | Honeywell International Inc. (99193) | |
| 2840-00-000-0049 2840000000049 | 2-200-070-67 | Modification kit, Engine | End Item Identification: T-55 series engines End Item Name: Engine, gas turbine End Item Source: Honeywell International Inc. (91547) | Honeywell International Inc. (99193) | |
| 2840-00-001-1741 2840000011741 | 6868835 | Case and Nozzle Assembly, Turbine | III End Item Identification: Acft eng TF-41 Criticality Code Justification: AGAV Engine Section Location: Turbine | Rolls-Royce Corporation (63005) Allison Transmission Inc. (73342) | |
| 2840-00-001-2114 2840000012114 | 9685M13P21 9685M13P27 K513P21 | Vane, Compressor, Aircraft gas Tur | III End Item Identification: Acft eng TF-39 Criticality Code Justification: AGAV Engine Section Location: Compressor | General Electric Company (07482) | |
| 2840-00-001-2117 2840000012117 | 9079M28G01 | Sleeve, Damper, Turbine Engine | General Electric Company (07482) | ||
| 2840-00-001-4903 2840000014903 | 8623102 | Seal, Air, Aircraft gas Turbine En | Allison Transmission Inc. (73342) General Motors LLC (7X677) Rolls-Royce Corporation (63005) | ||
| 2840-00-001-4908 2840000014908 | 8616052 | Seal, Air, Aircraft gas Turbine En | Allison Transmission Inc. (73342) Rolls-Royce Corporation (63005) | ||
| 2840-00-001-8342 2840000018342 | 3039M50P01 | Seal, Metallic, Aircraft gas Turbi | III End Item Identification: Acft eng TF-39 Criticality Code Justification: Apgf and czbj and feat Engine Section Location: High pressure turbine | General Electric Company (07482) | |
| 2840-00-001-8343 2840000018343 | 6009T46G03 | Nozzle, Turbine, Aircraft gas Turb | III End Item Identification: Engine assembly, turbo-jet, model no. J85-GE-21. Criticality Code Justification: AGAV | General Electric Company (99207) | |
| 2840-00-001-8347 2840000018347 | 9022M11G06 9022M11G07 9022M11G13 | Blade, Turbine Rotor, Aircraft gas | III End Item Identification: Acft eng TF-39 Criticality Code Justification: AGAV Engine Section Location: Turbine | General Electric Company (07482) | |
| 2840-00-001-8349 2840000018349 | 9084M26P01 | Plate, Turbine Rotor | General Characteristics Item Description: Steel, AMS5545, irregular shape, 0.880 in. approx lg, 0.800 in. min, 0.820 in. max, W, 0.029 in. min, 0.033 in. max thk, 2 0.110 in. min, 0.120 in.max, dia, holes spaced 0.340 in. apart, 4 embossments irregularly shaped | General Electric Company (07482) | |
| 2840-00-001-8351 2840000018351 | 9084M27P01 | Plate, High Pressure | General Characteristics Item Description: Steel, AMS5545, irregular shape, 0.740 in. min, 0.750 in. max, W, 0.029IN. min, 0.035 in. max, thk, 1.230 in. approx lg, 2 holes 0.150 in. min, 0.160 in. max dia, located 0.520 in. apart, 4 embossments irregularly shaped | General Electric Company (07482) | |
| 2840-00-001-9579 2840000019579 | 5026T38P01 | Vane, Compressor, Aircraft gas Tur | General Electric Company (99207) | ||
| 2840-00-001-9580 2840000019580 | 4027T26G02 | Bracket Assembly | General Electric Company (99207) | ||
| 2840-00-003-0750 2840000030750 | 6002T44P15 | Deflector Assembly, Power Takeoff | III End Item Identification: Eng J-85 General Characteristics Item Description: Steel AMS5512 and AMS5513, 5.150 in. approx, O/a W, 2.980 in. min, 3.020 in. max id | General Electric Company (99207, 03350) | |
| 2840-00-003-0833 2840000030833 | 3039M40P02 | Doubler, Flange, Fa | III End Item Identification: Acft eng TF-39 General Characteristics Item Description: Steel ams 5510, 6.380 in. O/a lg, 0.490 in. W, 0.300 in. O/a H, six 0.125 in. dia holes irregularly spaced | General Electric Company (07482) | |
| 2840-00-003-0834 2840000030834 | 3039M40P03 | Doubler, Flange, Fa | III End Item Identification: Acft eng TF-39 General Characteristics Item Description: Steel ams 5510, 6.050 in. O/a lg, 0.490 in. O/a W, 0.300 in. O/a H, six 0.125 in. dia holes irregularly spaced | General Electric Company (07482) | |
| 2840-00-003-0835 2840000030835 | 3039M40P04 | Doubler, Flange, Fa | General Characteristics Item Description: Steel ams 5510, 6.100 in. O/a lg, 0.490 in. O/a W, 0.300 in. O/ah, six 0.125 in. dia holes irregularly spaced | General Electric Company (07482) | |
| 2840-00-003-0836 2840000030836 | 3039M40P01 | Doubler, Flange, fan Stator Case | III End Item Identification: Acft eng TF-39 Criticality Code Justification: Matt and abhp and abmk and agav Special Features: Matl ams 5510 | General Electric Company (07482) | |
| 2840-00-003-0837 2840000030837 | 3020469 | Tube and Lead Assembly | III End Item Identification: Eng T400-CP400 General Characteristics Item Description: 13.804 in. min, 13.844 in. max O/a lg of tube, 16.750 in. approx.lg of lead, 9.094 in. approx. lg of heater element, resistance of heaterelement and lead wires 20 ohms porm 1.4 ohms at 68 deg F, fittings oneach end of tube per MS9381-04 | Canadian Commercial Corporation (98247) Pratt and Whitney Canada Inc. (00198) |