Part Details | AIRCRAFT GAS TURBINE ENGINE DIFFUSER
2840-01-428-7798 A frame with stationary struts, designed to diffuse and direct air from the COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It may have mounting facilities for external components. It may provide support and house a compressor rear bearing. May include a CASE (3), DIFFUSER, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 30916861, 3091686-1, 2840-01-428-7798, 01-428-7798, 2840014287798, 014287798
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 01, 1996 | 01-428-7798 | 50559 ( DIFFUSER, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-428-7798
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3091686-1 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-01-428-7798
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | CENTRIFUGAL |
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 4.102 INCHES MINIMUM AND 4.107 INCHES MAXIMUM |
| DIAMETER | 21.899 INCHES MINIMUM AND 21.901 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AAPGF$$ACZBJ$$AABMZ$$AABHP$$AAGAV |
| END ITEM IDENTIFICATION | PACER DAWN |