Part Details | AIRCRAFT GAS TURBINE ENGINE COMPONENT MOUNTING PLATE
2840-00-610-2726 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: 619E249G1, 619E249G1, 2840-00-610-2726, 00-610-2726, 2840006102726, 006102726
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1963 | 00-610-2726 | 50354 ( PLATE, COMPONENT MOUNTING, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-610-2726
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 619E249G1 | 24446 | GENERAL ELECTRIC COMPANY |
| 619E249G1 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-00-610-2726
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 6.880 INCHES MINIMUM AND 6.920 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | BLEED PAD CONNECTOR |