Part Details | AIRCRAFT GAS TURBINE ENGINE EXHAUST FRAME
2840-00-998-8623 A frame used for and part of the exhaust section of an aircraft gas turbine engine. May include struts.
Alternate Parts: 6006T75G02, 6006T75G01, 6006T75, 2840-00-998-8623, 00-998-8623, 2840009988623, 009988623
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 29, 1967 | 00-998-8623 | 52341 ( FRAME, EXHAUST, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-998-8623
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6006T75G02 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
| 6006T75G01 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
| 6006T75 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-00-998-8623
| Characteristic | Specifications |
|---|---|
| MATERIAL | NICKEL ALLOY |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5541 ASSN STD SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 8.480 INCHES MINIMUM AND 8.520 INCHES MAXIMUM |
| OUTSIDE DIAMETER | 19.880 INCHES MINIMUM AND 20.800 INCHES MAXIMUM |
| INSIDE DIAMETER | 18.400 INCHES NOMINAL |
| NUMBER OF VARIABLE GUIDE VANES | 7 |
| SPECIAL FEATURES | ITEM IS PART OF AN ASSEMBLY |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | TURBO PROP ENGINES (T64) |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | FRAME,POWER TURBINE EXHAUST |