Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR
2840-01-160-3217 A single or multistage item designed to receive, compress, and deliver air to the combustion area at a required pressure and velocity. It consists of a CASE (3) AND VANE ASSEMBLY, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and a ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 765574, 2840-01-160-3217, 01-160-3217, 2840011603217, 011603217
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 19, 1983 | 01-160-3217 | 50555 ( COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-160-3217
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 765574 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-160-3217
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| DIAMETER | 27.720 INCHES MINIMUM AND 27.740 INCHES MAXIMUM |
| SPECIAL FEATURES | STAGE 14; TO BE USED ONLY ON P102/A/B/P103 ENGINE SERIES; SUPERSEDES P/N 389471, 446074, 534384, 612794, 555894, 703174, 744894 |
| CRITICALITY CODE JUSTIFICATION | AABMZ$$ACZBJ$$AFEAT |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-34, FIG 14, IND 23 |
| END ITEM IDENTIFICATION | TF33-P102/A/B/P103 AIRCRAFT GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME COMPRESSOR,AXIAL,TURBINE ENGINE |