Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE FRAME
2840-01-434-7020 A frame used for and part of a TURBINE ASSEMBLY,AIRCRAFT GAS TURBINE ENGINE. May include struts.
Alternate Parts: 9184M63G05, 9138M62G10, 2840-01-434-7020, 01-434-7020, 2840014347020, 014347020
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 05, 1996 | 01-434-7020 | 52349 ( FRAME, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-434-7020
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9184M63G05 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9138M62G10 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-434-7020
| Characteristic | Specifications |
|---|---|
| MATERIAL | NICKEL ALLOY |
| OVERALL LENGTH | 13.165 INCHES MINIMUM AND 13.205 INCHES MAXIMUM |
| OUTSIDE DIAMETER | 16.160 INCHES MINIMUM AND 16.200 INCHES MAXIMUM |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF39-4, FIG 63 IND 1 |
| SPECIAL FEATURES | TURBINE MID FRAME ASSY; NEW FRAME TO REDUCE NUMBER OF LINER SADDLE AND BLIPPER CRACKS; G10 FRAME HAS NEW LINER, 1820M83G01, WHICH INCORPORATES A REDESIGNED BLIPPER, HIGHER IN STRENGTH/TEMPERATURE; INTERGAL WITH THE LINER FOWARD OUT RING INSTEAD OF BEING WELDED TO THE RING AS OF NOW; TURBINE MID FRAME NOT AFFECTED IN PHYSICAL INTERCHANGEABILITY; NEW LINER AND CURRENT LINER ARE PHYSICALLY INTERCHANGEABLE; FUNCTIONAL INTERCHANGEABILITY IS AFFECTED IN THAT THE NEW LINER HAS HIGHER STRENGTH/TEMPERATURE |
| CRITICALITY CODE JUSTIFICATION | AABHP$$AABKV$$AFEAT |
| END ITEM IDENTIFICATION | TF-39 AIRCRAFT GAS TURBINE ENGINE |