Part Details | AIRCRAFT GAS TURBINE ENGINE COMPONENT MOUNTING PLATE
2840-01-078-5307 A metallic item of various shapes designed to reduce vibration and to secure a component part of an ENGINE, GAS TURBINE, AIRCRAFT to the engine case or housing as modified. For mounting accessories to the outside of the engine, see PLATE, MOUNTING.
Alternate Parts: 513099, 513099, 2840-01-078-5307, 01-078-5307, 2840010785307, 010785307
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUN 15, 1979 | 01-078-5307 | 50354 ( PLATE, COMPONENT MOUNTING, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-078-5307
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 513099 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 513099 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-078-5307
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | DIFFUSER |
| OVERALL LENGTH | 5.068 INCHES NOMINAL |
| OVERALL WIDTH | 1.218 INCHES NOMINAL |
| SPECIAL FEATURES | T.O. 2J-TF33-4, FIG 20, IND 86; 2ND END WIDTH 1.100; 1ST PLATE HOLE LENGTH 1.510; WIDTH 1.218; 2ND PLATE HOLEDIA. 0.807-0.817 |
| CRITICALITY CODE JUSTIFICATION | ACZBJ$$AABHP$$AABMK$$AFEAT |
| END ITEM IDENTIFICATION | TF33 ENGS |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME COVER,SERVICE FIX |