Thank you for taking an interest in our selection of 2840-01-022-0859 parts here on Boost AOG. You are currently on the RFQ form for part number 565720, a Turbo Power And Marine System Inc product listed with the Seal Metallic Aircraft Gas Turbi If part number 565720 catches your eye, be sure to use our online RFQ service to request quotes, with customized responses provided within 15 minutes of us receiving and reviewing a completed submission.
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To ensure the quality of our NSN components, we adhere to a strict NO CHINA SOURCING pledge, meaning every purchased item will be delivered alongside any pertinent qualifying certifications or manufacturing trace documentation for your benefit. Paired with numerous other commitments, we proudly operate with AS9120B, ISO 9001:2015, and FAA AC 00-56B accreditation. If you happen to be facing a time constraint and require NSN parts quickly, contact us at your earliest convenience, and we will discuss the expedited shipping options we have available for domestic and international customers alike. With our various dedications in mind, kick off procurement for Turbo Power And Marine System Inc part number 565720 and other Seal Metallic Aircraft Gas Turbi products today.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-022-0859 Item PartTypeName: SEAL,METALLIC,AIRCRAFT GAS TURBI | 2840 | 010220859 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
565720 | 6 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 1.215 INCHES MINIMUM AND 1.225 INCHES MAXIMUM |
ABMZ | DIAMETER | 6.873 INCHES MINIMUM AND 6.875 INCHES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | ACFT ENG TF33 |
APGF | DESIGN TYPE | AXIAL COMPRESSOR |
CRTL | CRITICALITY CODE JUSTIFICATION | MATT AND CZBJ AND ABHP AND ABMZ |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME CARBON SEAL,ENGINE |
CZBJ | ENGINE SECTION LOCATION | TURBINE |
FEAT | SPECIAL FEATURES | T.O. 2J-TF33-14,FIG 4,IND 41A; USED ON THE NO. 1 BEARING,SUPPORT COMPRESSOR INLET CONE; MATL IS GRAPHITE CARBON |
MATT | MATERIAL | GRAPHITE OVERALL |
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