Part Details | AIRCRAFT GAS TURBINE ENGINE EXHAUST DUCT
2840-01-190-9262 A cylindrical shaped item designed to direct the hot gases that are discharged from an ENGINE, GAS TURBINE, AIRCRAFT. It is the outer portion of a DUCT AND CONE, EXHAUST, AIRCRAFT GAS TURBINE ENGINE. It may be attached directly to the engine.
Alternate Parts: 1281M35G01, 1278M46G02, 1281M35G01, 1281M35G01, 2840-01-190-9262, 01-190-9262, 2840011909262, 011909262
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 04, 1984 | 01-190-9262 | 50343 ( DUCT, EXHAUST, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-190-9262
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1281M35G01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1278M46G02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1281M35G01 | 03350 | GENERAL ELECTRIC COMPANYDBA GE STRUCTURED SERVICES DIV |
| 1281M35G01 | 80512 | MAGELLAN AEROSPACE, MIDDLETOWN, INC. |
Technical Data | NSN 2840-01-190-9262
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| OVERALL LENGTH | 9.360 INCHES MINIMUM AND 9.420 INCHES MAXIMUM |
| OVERALL WIDTH | 8.180 INCHES MINIMUM AND 8.220 INCHES MAXIMUM |
| MATERIAL THICKNESS | 0.0125 INCHES MINIMUM AND 0.0155 INCHES MAXIMUM |
| SPECIAL FEATURES | 17 HOLES 0.243-0.251 IN. DIA.; 10 HOLES 0.098-0.102 IN. DIA. |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG F110 |
