Part Details | AIRCRAFT GAS TURBINE ENGINE AUGMENTOR NOZZLE SECTION SEAL
2840-01-471-6752 A rigid item designed to complete the circumference when the NOZZLE,AUGMENTER EXHAUST,AIRCRAFT GAS TURBINE ENGINE is in the open position allowing the nozzle to maintain control of the hot exhaust gases. It is situated between the AUGMENTOR NOZZLE SECTION,OUTER,AIRCRAFT GAS TURBINE ENGINE and the AUGMENTOR NOZZLE SECTION,OUTER,AIRCRAFT GAS TURBINE ENGINE and the AUGMENTOR NOZZLE SECTION,CONVERGENT,AIRCRAFT GAS TURBINE ENGINE; AUGMENTOR NOZZLE SECTION,INNER,AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 4073477, 4073477, 2840-01-471-6752, 01-471-6752, 2840014716752, 014716752
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | FEB 10, 2000 | 01-471-6752 | 53243 ( SEAL, AUGMENTOR NOZZLE SECTION, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-471-6752
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4073477 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4073477 | 32543 | WHITCRAFT LLCDBA WHITCRAFT |
Technical Data | NSN 2840-01-471-6752
| Characteristic | Specifications |
|---|---|
| MATERIAL | TITANIUM ALLOY |
| MATERIAL THICKNESS | 0.045 INCHES MINIMUM AND 0.080 INCHES MAXIMUM |
| OVERALL LENGTH | 1.640 INCHES NOMINAL |
| OVERALL WIDTH | 2.280 INCHES NOMINAL |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F100-54 |
| END ITEM IDENTIFICATION | F100-220 ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | SEAL-AUGMENTOR COMBUSTION CHAMBER DUCT |