Part Details | AIRCRAFT GAS TURBINE ENGINE AUGMENTOR NOZZLE SECTION SEAL
2840-01-190-6884 A rigid item designed to complete the circumference when the NOZZLE,AUGMENTER EXHAUST,AIRCRAFT GAS TURBINE ENGINE is in the open position allowing the nozzle to maintain control of the hot exhaust gases. It is situated between the AUGMENTOR NOZZLE SECTION,OUTER,AIRCRAFT GAS TURBINE ENGINE and the AUGMENTOR NOZZLE SECTION,OUTER,AIRCRAFT GAS TURBINE ENGINE and the AUGMENTOR NOZZLE SECTION,CONVERGENT,AIRCRAFT GAS TURBINE ENGINE; AUGMENTOR NOZZLE SECTION,INNER,AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 9505M12G02, 9505M12G02, 9505M12G02, 9505M12G02, 9505M12G02, 2840-01-190-6884, 01-190-6884, 2840011906884, 011906884
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 29, 1984 | 01-190-6884 | 53243 ( SEAL, AUGMENTOR NOZZLE SECTION, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-190-6884
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9505M12G02 | 51226 | ASSOCIATED AEROSPACE ACTIVITIES INC |
| 9505M12G02 | 85291 | B. H. AIRCRAFT COMPANY, INC. |
| 9505M12G02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9505M12G02 | H1418 | THALES CRYOGENICS B.V. |
| 9505M12G02 | 16126 | UNISON ENGINE COMPONENTS INC.DBA UNISON ENGINE COMPONENTS |
Technical Data | NSN 2840-01-190-6884
| Characteristic | Specifications |
|---|---|
| OVERALL LENGTH | 13.350 INCHES MINIMUM AND 13.390 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG F110 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | SEAL, PRIMARY |