Thank you for considering Inspektorat Wsparcia Sil Zbrojnych part number 2840PL0784431, an item we carry that is listed with the NSN 2840-01-138-5658 and product description “Retainer Turbine Blade Aircraft.” This component is available for purchase through our website at this time, so complete the Request for Quote (RFQ) form provided below if you would like to receive pricing information for your comparisons. Simply offer our staff details like your desired quantity, budget, and delivery timeline to help us craft the best solution for your needs.
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We aim to make the process of locating and procuring exact items simple, which is why we feature key listing details with every offering. For example, part number 2840PL0784431 was specifically produced by Inspektorat Wsparcia Sil Zbrojnych under CAGE Code 9009H, and with the NSN 2840-01-138-5658, it belongs to FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Additionally, all stock comes delivered with any applicable qualifying certifications or manufacturer trace documentation for your further benefit. With all of this in mind, be sure to submit a request for part number 2840PL0784431 today, knowing we will be in touch shortly after reviewing your information.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-138-5658 Item PartTypeName: RETAINER,TURBINE BLADE,AIRCRAFT | 2840 | 011385658 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
2840PL0784431 | 3 | 9 | 6 |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 0.694 INCHES NOMINAL |
ABKV | OUTSIDE DIAMETER | 22.854 INCHES MINIMUM AND 22.885 INCHES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | ACFT ENG TF39 |
CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
CZCJ | STAGE NUMBER | 2 |
FEAT | SPECIAL FEATURES | HIGH PRESSURE TURBINE ROTOR ASSY;2ND STAGE; CBORE FOR 29 HOLES EQ SP,29 POCKETS |
MATT | MATERIAL | STEEL |
RDAL | REFERENCE DATA AND LITERATURE | 2J-TF39-4,FIG 59 IND 25 |
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