Aerospace Engineering Solutions is proud to offer immediate purchasing options on United Technologies Corporation part number 555665, a Seal Air Aircraft Gas Turbine En product we carry that is listed with the NSN 2840-00-227-8889 for ease of identification. If you would like to learn more about this item, be sure to complete the Request for Quote (RFQ) form provided on this page. By including essential details like your target price, desired quantity, and expected fulfillment timeline, you are ensured a fully customized quote from our team.
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For your reference, this product is traceable to United Technologies Corporation through the CAGE Code 77445, as well as categorized under FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components based on the first four digits of the NSN 2840-00-227-8889. Using such information, you can easily narrow down exact items of need for an ease of procurement. With our quotation service in mind, be sure to submit a completed form when you are ready to begin. Should you wish to speak with one of our representatives to discuss services, you can also give us a call or email at your convenience. With all that we offer, choose Aerospace Engineering Solutions for part number 555665 and other NSN items of need.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-00-227-8889 Item PartTypeName: SEAL,AIR,AIRCRAFT GAS TURBINE EN | 2840 | 002278889 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
309770 | 2 | 9 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 1.134 INCHES MINIMUM AND 1.154 INCHES MAXIMUM |
ABMZ | DIAMETER | 24.900 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | J-75 AIRCRAFT ENGINE |
APGF | DESIGN TYPE | AXIAL COMPRESSOR |
CQFM | HARDNESS RATING | 30.0 ROCKWELL C NOMINAL OVERALL |
CRTL | CRITICALITY CODE JUSTIFICATION | CZBJ AND SFTT AND ABMZ AND ABHP AND FEAT |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME RING,COMPRESSOR ROTOR,AIRCRAFT GAS TURBINE ENGINE |
CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
CZCJ | STAGE NUMBER | 10 |
FEAT | SPECIAL FEATURES | T.O. 2J-J75-4,FIG 13,IND 12; CASE-REAR COMPRESSOR FRONT |
MATT | MATERIAL | STEEL OVERALL |
SFTT | SURFACE TREATMENT | NICKEL OVERALL AND CADMIUM OVERALL |
STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | AMS2416 ASSN STD SINGLE TREATMENT RESPONSE OVERALL |
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