Aircraft Prime Moving Gas Turbines and Jet Engines and Components: 4081656, 4081662, 4081921-802
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 4081656 | 2840-01-390-6740 | Support, Augmentor Component, Airc | III End Item Identification: F100-PW-100/200 aircraft engines Criticality Code Justification: AGAV Material: Titanium alloy | United Technologies Corporation (77445) | |
| 4081662 | 2840-01-384-3647 | Parts kit, Turbine Engine | End Item Identification: Acft eng End Item Name: F100 | United Technologies Corporation (52661,77445) | |
| 4081665 | 2840-01-420-4764 | Seal, Air, Aircraft gas Turbine En | III End Item Identification: F100-PW-229 aircraft gas turbine engine Criticality Code Justification: Czbj and czcj and feat Engine Section Location: Compressor | United Technologies Corporation (77445) | |
| 4081672-01 408167201 | 2840-01-390-7450 | Duct, Compressor, Aircraft gas Tur | Criticality Code Justification: AGAV Engine Section Location: Compressor Material: Steel overall | United Technologies Corporation (77445) | |
| 4081672-02 408167202 | 2840-01-397-4401 | Duct, Compressor, Aircraft gas Tur | Criticality Code Justification: AGAV Engine Section Location: Compressor Material: Steel overall | United Technologies Corporation (77445) | |
| 4081704 | 2840-01-205-1298 | Vane, Compressor, Aircraft gas Tur | III End Item Identification: Acft eng F100-PW-220 Engine Section Location: Compressor Special Features: Original name vane, compressor stator, turbine engine | United Technologies Corporation (77445) | |
| 4081705 | 2840-01-205-1297 | Vane, Compressor, Aircraft gas Tur | III End Item Identification: Acft eng F100-PW-220 Engine Section Location: Compressor Special Features: Original name vane, compressor stator, turbine engine | United Technologies Corporation (77445) | |
| 4081726 | 2840-01-449-3295 | Case, Compressor, Aircraft gas Tur | III End Item Identification: F-16 aircraft | United Technologies Corporation (77445) | |
| 4081800 | 2840-01-539-2961 | Case and Nozzle Assembly, Turbine | III End Item Identification: F-16; F 100 engine | United Technologies Corporation (77445) | |
| 4081821 | 2840-01-341-0177 | Cold Section Module, Aircraft gas | III End Item Identification: F100-PW-220/220E aircraft eng Criticality Code Justification: AGAV General Characteristics Item Description: T.O. 2J-F100-24; house the three stage low pressure fan | United Technologies Corporation (77445) | |
| 4081821-800 4081821800 | 2840-01-341-0177 | Cold Section Module, Aircraft gas | III End Item Identification: F100-PW-220/220E aircraft eng Criticality Code Justification: AGAV General Characteristics Item Description: T.O. 2J-F100-24; house the three stage low pressure fan | United Technologies Corporation (77445) | |
| 4081821-802 4081821802 | 2840-01-341-0177 | Cold Section Module, Aircraft gas | III End Item Identification: F100-PW-220/220E aircraft eng Criticality Code Justification: AGAV General Characteristics Item Description: T.O. 2J-F100-24; house the three stage low pressure fan | United Technologies Corporation (77445) | |
| 4081821-804 4081821804 | 2840-01-341-0177 | Cold Section Module, Aircraft gas | III End Item Identification: F100-PW-220/220E aircraft eng Criticality Code Justification: AGAV General Characteristics Item Description: T.O. 2J-F100-24; house the three stage low pressure fan | United Technologies Corporation (77445) | |
| 4081821-805 4081821805 | 2840-01-341-0177 | Cold Section Module, Aircraft gas | III End Item Identification: F100-PW-220/220E aircraft eng Criticality Code Justification: AGAV General Characteristics Item Description: T.O. 2J-F100-24; house the three stage low pressure fan | United Technologies Corporation (77445) | |
| 4081851 | 2840-01-509-6670 | Vane Segment, Compressor, Aircraft | III End Item Identification: F100PW229 Criticality Code Justification: AGAV | United Technologies Corporation (77445) | |
| 4081874 | 2840-01-408-6920 | Blade set, Compressor, Aircraft Ga | Criticality Code Justification: AGAV Special Features: Used on 4TH stage, min 2 requiredboth must be same moment wt within .200 0Z-IN. End Item Identification: Acft eng F100 | United Technologies Corporation (77445) | |
| 4081904 | 2840-01-425-7589 | Blade, Turbine Rotor, Aircraft gas | III End Item Identification: F100PW229 aircraft gas turbine engine Criticality Code Justification: Apgf and czbj and czcj and bglw and abhp Engine Section Location: Turbine | United Technologies Corporation (77445) | |
| 4081921 | 2840-01-341-0178 | Cold Section Module, Aircraft gas | III End Item Identification: F100-PW-220/220E aircraft eng Criticality Code Justification: AGAV General Characteristics Item Description: T.O. 2J-F100-24; house the three stage low pressure fan | United Technologies Corporation (77445) | |
| 4081921-800 4081921800 | 2840-01-341-0178 | Cold Section Module, Aircraft gas | III End Item Identification: F100-PW-220/220E aircraft eng Criticality Code Justification: AGAV General Characteristics Item Description: T.O. 2J-F100-24; house the three stage low pressure fan | United Technologies Corporation (77445) | |
| 4081921-802 4081921802 | 2840-01-455-7198 | Fan, Aircraft gas Turbine Engine | III End Item Identification: Acft eng F100 Criticality Code Justification: AGAV Engine Section Location: FAN | United Technologies Corporation (77445) |