Part Details | AIRCRAFT GAS TURBINE ENGINE INLET GUIDE VANE SYNCHRONIZING RING
2840-01-437-1124 A single or multipiece item of various cross sections used to insure the synchronization of movement of the inlet guide vanes. May include associated hardware.
Alternate Parts: 4079597, 2840-01-437-1124, 01-437-1124, 2840014371124, 014371124
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 05, 1996 | 01-437-1124 | 51914 ( SYNCHRONIZING RING, INLET GUIDE VANE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-437-1124
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4079597 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-437-1124
| Characteristic | Specifications |
|---|---|
| MATERIAL | TITANIUM ALLOY |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS4928 ASSN STD SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 0.960 INCHES MINIMUM AND 0.980 INCHES MAXIMUM |
| OUTSIDE DIAMETER | 37.264 INCHES MINIMUM AND 37.268 INCHES MAXIMUM |
| INSIDE DIAMETER | 36.000 INCHES MINIMUM AND 36.004 INCHES MAXIMUM |
| PORTION OF CIRCUMFERENCE | 360 DEGREES |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F100-24, FIG 116, IND 38 |
| SPECIAL FEATURES | FOUND IN THE NO. 1 BEARING HOUSING AND SEAL; COMPRESSOR STATOR INLET; WIDTH 0.520-0.524; 21 HOLES EQ SP 0.3120-0.3130 IN DIA. |
| CRITICALITY CODE JUSTIFICATION | AABKV$$AAARX$$AABHP$$AFEAT |
| END ITEM IDENTIFICATION | F100 AIRCRAFT GAS TURBINE ENGINE |