Thank you for taking an interest in the various military and defense parts, aerospace parts, and other items that we offer. You have reached the RFQ page for part number 1807M27G03, a General Electric Company item with the NSN 2840014446529 that is listed alongside the description “Damper Turbine Blade Aircraft Tu.” If you are interested in part number 1807M27G03 and wish to learn more about your purchasing options, be sure to submit the form below at your earliest convenience while supplying us with important information concerning your needs and restrictions alike. Once we have a chance to receive and review your completed form, a member of our staff will reach out to you in 15 minutes or less to present a tailored solution for your comparisons.
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To ensure that shopping with us is as simple as possible, we make it easy to identify and procure exact items by listing parts alongside all applicable designations and information. For example, part number 1807M27G03 is specifically listed with the NSN 2840-01-444-6529, and this code can be used to determine that it falls under FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Additionally, while tracing back to General Electric Company, this NSN part was specifically produced under CAGE Code 07482. With our services and dedication to simple procurement in mind, get started with us today!
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-444-6529 Item PartTypeName: DAMPER,TURBINE BLADE,AIRCRAFT TU | 2840 | 014446529 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
7 | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
1807M27 | 5 | 9 | D |
MRC | Criteria | Characteristic |
---|---|---|
APGF | Design Type | AXIAL COMPRESSOR |
FEAT | Special Features | ORIGNAL NAME DAMPER ASSEMBLY,HIGH PRESSURE TURBINE ROTOR-STAGE 1. G03 ADDED TO PART NUMBER PER CID 219639. THIS ITEM IS PART OF THE HT90 MOD FOR THE TF39 ENGING |
MRC | Decoded Requirement | Clear Text Reply |
AGAV | End Item Identification | ACFT ENG TF39 |
CZBJ | Engine Section Location | HIGH PRESSURE TURBINE |
CRTL | Criticality Code Justification | AGAV |
CZCJ | Stage Number | 1 |
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