| Part Number : 4082885 | Manufacturer : United Technologies Corporation | ||
| NSN : 2840-01-440-1697 (2840014401697) | |||
| Item Name : Damper Turbine Blade Aircraft Tu | CAGE Code : 77445 | ||
| NIIN : 01-440-1697 (014401697) | |||
| FSC Code : 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components | |||
| FSG Code : 28 Engines Turbines and Components | |||
| INC Code : 50557 | |||
| NCB Code : 01 | Country : USA | ||
Thank you for taking an interest in part number 4082885, that of which is listed with the description Damper Turbine Blade Aircraft Tu; Manufactured by United Technologies Corporation and listed alongside the NSN 2840014401697, part number 4082885 is available for immediate purchase on our website. As such, to learn more about this offering while receiving a competitive quote for your comparisons, be sure to fill out and submit the RFQ form presented on this page. Within 15 minutes of us receiving and reviewing a completed form, a member of our staff will contact you to present a tailored solution for your comparisons.
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| Part Number : 4082885 | Manufacturer : United Technologies Corporation | ||
| NSN Number : 2840-01-440-1697 (2840014401697) | |||
| Item Name : Damper Turbine Blade Aircraft Tu | CAGE Code : 77445 | ||
| NIIN : 014401697 | |||
| FSC CODE : 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components | |||
Thank you for taking an interest in part number 4082885, that of which is listed with the description Damper Turbine Blade Aircraft Tu; Manufactured by United Technologies Corporation and listed alongside the NSN 2840014401697, part number 4082885 is available for immediate purchase on our website. As such, to learn more about this offering while receiving a competitive quote for your comparisons, be sure to fill out and submit the RFQ form presented on this page. Within 15 minutes of us receiving and reviewing a completed form, a member of our staff will contact you to present a tailored solution for your comparisons.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-440-1697 Item PartTypeName: DAMPER,TURBINE BLADE,AIRCRAFT TU | 2840 | 014401697 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 2840PL0712503 | 2 | 9 | 6 |
| MRC | Criteria | Characteristic |
|---|---|---|
| CQFM | HARDNESS RATING | 34.0 ROCKWELL C MINIMUM AND 44.0 ROCKWELL C MAXIMUM OVERALL |
| AGAV | III END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS5544 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| ABMZ | DIAMETER | 16.788 INCHES NOMINAL |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT AND CZBJ |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| ABHP | OVERALL LENGTH | 0.565 INCHES MINIMUM AND 0.571 INCHES MAXIMUM |
| FEAT | SPECIAL FEATURES | T.O. 2J-F100-54, FIG 99, IND 21; REPL P/N 4074864 ONCE TCTO HAS BEEN ACCOMPLISHED; RETAINING PLATE DAMPER IS SYMMETRICAL IN SHAPE AND HAS 6 RETENTION TABS FORWARD AND AFT TO PRECLUDE POSSIBLE REVERSE INSTALLATION AND RESULTING CUT-OFF OF COOLING AIR TO THE 2ND STAGE BLADES |
| MATT | MATERIAL | NICKEL ALLOY OVERALL |
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