Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR DUCT
2840-01-451-9636 A cylindrical shaped item or a segment thereof designed to direct air into or around a COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. The air is further compressed or used for cooling purposes.
Alternate Parts: 408287101, 4082871-01, 4082871, 2840-01-451-9636, 01-451-9636, 2840014519636, 014519636
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 09, 1998 | 01-451-9636 | 52525 ( DUCT, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-451-9636
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4082871-01 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4082871 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-451-9636
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 12.130 INCHES NOMINAL |
| OVERALL WIDTH | 2.320 INCHES MINIMUM AND 2.326 INCHES MAXIMUM |
| DIAMETER | 27.647 INCHES MINIMUM AND 27.659 INCHES MAXIMUM |
| SPECIAL FEATURES | NO 3. BEARING REAL SEAL ASSY, REAR COMPRESSOR STATOR VARIABLE INLET VANES, EXIT FAN STATOR AND COMPRESSOR INTERMEDIATE CASE ASSY; STAGE 4; REPLACES P/N 4081682-01; CORROSION RESISTANT SEGMENTS |
| CRITICALITY CODE JUSTIFICATION | AABMK$$AABHP$$AABMZ$$AFEAT |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F100-54, FIG 84, IND 16 AND 17 |
| END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME DUCT SEGMENT,COMPRESSOR |