Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR CASE PLUG
2840-01-484-5562 A usually round item of various cross sections designed for temporary installation into a hole in a CASE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE for the purpose of preventing air from escaping during engine operation. When removed, the hole is for inserting inspection probes, borescopes and the like. It may be grooved or tapered for installation and removal. It may include spacers, springs, rivets and the like.
Alternate Parts: 4321064, 2840-01-484-5562, 01-484-5562, 2840014845562, 014845562
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 01, 2001 | 01-484-5562 | 52956 ( PLUG, COMPRESSOR CASE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-484-5562
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4321064 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-484-5562
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | AP 6 PROVIDES ACCESS BETWEEN 7TH AND 8TH STAGE INTEGRALLY BLADED MOTOR (IBR) |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F119-PW-100 ENGINE ON F-22 AIRCRAFT |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | PLUG ASSY OF--INSTRUMENTATION BOSS (AP 6) |