Part Details | AIRCRAFT GAS TURBINE ENGINE OIL SUMP
2840-00-855-5799 A chamber surrounding the main bearings for a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. The chanber is used to collect lubricating fluid for recirculation.
Alternate Parts: 6003T87G01, 6003T87G01, 2840-00-855-5799, 00-855-5799, 2840008555799, 008555799
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 29, 1972 | 00-855-5799 | 52549 ( SUMP, OIL, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-855-5799
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6003T87G01 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
| 6003T87G01 | 93596 | KERNS MANUFACTURING CORP. |
Technical Data | NSN 2840-00-855-5799
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 2.868 INCHES MINIMUM AND 2.872 INCHES MAXIMUM |
| MATERIAL THICKNESS | 0.070 INCHES MINIMUM AND 0.090 INCHES MAXIMUM |
| DIAMETER | 6.300 INCHES NOMINAL |
| SPECIAL FEATURES | T.O. 2J-J85-94, FIG 7, IND 28; 2ND END DIA. 5.560 |
| CRITICALITY CODE JUSTIFICATION | AABHP$$AABPX$$AABMZ$$AFEAT |
| END ITEM IDENTIFICATION | J85-GE-21/21A/21B AIRCRAFT GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME SUMP,FRONT FRAME |