NSN 2840-00-188-2211
Part Details | AIRCRAFT GAS TURBINE ENGINE AIRFLOW BAFFLE
2840-00-188-2211 A generally metallic item of various shapes designed to provide an optimum diversion of cooling air around and through an air-cooled ENGINE, GAS TURBINE, AIRCRAFT. Excludes DEFLECTOR, AIR FLOW.
Alternate Parts: 106C3314G2, 2840-00-188-2211, 00-188-2211, 2840001882211, 001882211
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 01, 1972 | 00-188-2211 | 50529 ( BAFFLE, AIRFLOW, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-188-2211
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 106C3314G2 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-00-188-2211
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 2 |
| OVERALL LENGTH | 0.190 INCHES NOMINAL |
| MATERIAL THICKNESS | 0.040 INCHES MINIMUM AND 0.050 INCHES MAXIMUM |
| SPECIAL FEATURES | RADIUS 12.25 IN. MIN AND 12.29 IN. MAX; 5 MOUNTING HOLES, 1 AT 0.251-0.254 IN. DIA AND 4 AT 0.281 IN. DIA |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG |
