Part Details | AIRCRAFT GAS TURBINE ENGINE AUGMENTOR NOZZLE SECTION SEAL
2840-01-470-0764 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: 4083510, 4083510, 2840-01-470-0764, 01-470-0764, 2840014700764, 014700764
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | DEC 07, 1999 | 01-470-0764 | 53243 ( SEAL, AUGMENTOR NOZZLE SECTION, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-470-0764
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4083510 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 4083510 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-470-0764
| Characteristic | Specifications |
|---|---|
| MATERIAL | TITANIUM ALLOY |
| MATERIAL THICKNESS | 0.175 INCHES MINIMUM AND 0.185 INCHES MAXIMUM |
| SPECIAL FEATURES | FOUR HOLES SIZE MIN.0.276,MAX.0.286 EVENLY SPACEDAROUND OUTSIDE DIA.;SIX HOLES EVENLY SPACED INSIDE DIA., TWO OF WHICH ARE SIZE MIN.0.807,MAX.0.817; ONENE IS MIN.0.620,MAX.0.630; THREE ARE MIN.0.276,MAX0.286 |
| END ITEM IDENTIFICATION | ENGINE AIRCRAFT, F-100-PW-229 |