Aircraft Prime Moving Gas Turbines and Jet Engines and Components: 767511, 767666CL3, 767925
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 767511 | 2840-01-035-8206 | Case, fan Exit | III End Item Identification: TF30-P-412 engine | United Technologies Corporation (77445) | |
| 767512 | 2840-01-035-5579 | Spacer Assembly, Compressor Rotor | III End Item Identification: Aircraft engine model TF30-P-414 | United Technologies Corporation (52661,77445) | |
| 767515 | 2840-01-035-5581 | Plate, Positioning | General Characteristics Item Description: Cres AMS5616, 13.795 in. min, 13.805 in. max lg, 0.990 in. min, 1.010 in. max W | United Technologies Corporation (77445) | |
| 767528 | 2840-01-035-8218 | Plate, Positioning | III End Item Identification: TF-30 engine General Characteristics Item Description: Titanium AMS4911, 0.339 in. min, 0.349 in. max dia 22 holes, 24.924 in. min, 25.056 in. max O/a lg, 0.190-32 UNJF-3B thd 2 holes | United Technologies Corporation (77445) | |
| 767530 | 2840-01-035-8213 | Plate, Positioning | General Characteristics Item Description: Titanium alloy ams 4928, 23.900 in. min, 24.032 in. max lg, 0.129 in. min, 0.133 in. max thk | United Technologies Corporation (77445) | |
| 767554 | 2840-01-035-8210 | Ring, Air Sealing, Compressor | III End Item Identification: TF-30-P-414A (F-14A) aircraft engine General Characteristics Item Description: Cadmium AMS2416, 0.089 in. min, 0.099 in. max od 88 holes | Hansen Engineering and Machinery Co. (98839) United Technologies Corporation (77445) | |
| 767571 | 2840-01-035-8253 | Vane, Compressor Stator, Turbine E | III End Item Identification: Aircraft engine model TF30-P-414 | United Technologies Corporation (77445) | |
| 767572 | 2840-01-035-8252 | Vane, Compressor, Aircraft gas Tur | United Technologies Corporation (77445) | ||
| 767582 | 2840-01-043-9623 | Shroud, Turbine Stat | United Technologies Corporation (77445) | ||
| 767591 | 2840-01-085-0261 | Housing, Bleed Valve | III End Item Identification: Engine model J52 General Characteristics Item Description: 2.090 in. min, 2.092 in. max lg, 1.525 in. min, 1.545 in. max W | United Technologies Corporation (77445) | |
| 767666CL1 | 2840-01-049-5886 | Lock, Turbine Stator | III End Item Identification: Acft engine TF33 Criticality Code Justification: Matt and adav and abmk and agav Special Features: Matl ams 5736 | United Technologies Corporation (77445) | |
| 767666CL2 | 2840-01-049-5887 | Lock Ring, Turbine Nozzle, Aircraf | III End Item Identification: Acft engine TF33 Criticality Code Justification: AGAV Special Features: Matl ams 5736 | United Technologies Corporation (77445) | |
| 767666CL3 | 2840-01-049-5888 | Lock, Turbine Stator | III End Item Identification: Acft engine TF33 Criticality Code Justification: Matt and adav and abmk and agav Material: Steel corrosion resisting | United Technologies Corporation (77445) | |
| 767666CL4 | 2840-01-049-5889 | Lock, Turbine Stator | III End Item Identification: Acft engine TF33 Criticality Code Justification: Matt and adav and abmk and agav Material: Steel corrosion resisting | United Technologies Corporation (77445) | |
| 767666CL5 | 2840-01-049-5890 | Lock Ring, Turbine Nozzle, Aircraf | III End Item Identification: Acft engine TF33 Criticality Code Justification: AGAV Special Features: Matl ams 5736 | United Technologies Corporation (77445) | |
| 767779 | 2840-01-035-8205 | Strut Assembly, fan | III End Item Identification: TF30-P-412 engine | United Technologies Corporation (77445) | |
| 767783 | 2840-01-035-8208 | Cover, fan Exit Case | III End Item Identification: TF30-P-412 engine General Characteristics Item Description: Titanium; 4.010 in. max dia | United Technologies Corporation (77445) | |
| 767921 | 2840-01-036-4842 | Support, Turbine Component, Aircra | III End Item Identification: Acft eng TF33-P7/7A Criticality Code Justification: AGAV Overall Length: 6.330 inches minimum and 6.350 inches maximum | United Technologies Corporation (77445) | |
| 767922 | 2840-01-038-3217 | Shroud Segment, Turbine, Aircraft | III End Item Identification: Acft engine TF33-P3/5/9/11A Criticality Code Justification: Czbj and apgf and abhp and abmz Engine Section Location: Turbine | United Technologies Corporation (77445) | |
| 767925 | 2840-01-026-6540 | Kit, P and D Valve | III End Item Identification: Acft engine J57-13, 19, 21, 23, 29, 43, 55 and 59 | United Technologies Corporation (77445) |