Aerospace Engineering Solutions is proud to offer immediate purchasing options on Honeywell International Inc part number 441944-10, a Control Exhaust Nozzle Turbine E product we carry that is listed with the NSN 2995-01-433-6462 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 Honeywell International Inc through the CAGE Code 06848, as well as categorized under FSC 2995 Miscellaneous Engine Accessories Aircraft based on the first four digits of the NSN 2995-01-433-6462. 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 441944-10 and other NSN items of need.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2995-01-433-6462 Item PartTypeName: CONTROL,EXHAUST NOZZLE,TURBINE E | 2995 | 014336462 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
I | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
441944-10 | 3 | 3 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
AGAV | END ITEM IDENTIFICATION | F100-PW-129 ACFT ENGINE |
CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
FEAT | SPECIAL FEATURES | SORIGINAL ITEM NAME -- CONVERGENT EXHAUST NOZZLE CONTROL, THIS REDESIGNED NOZZLE CONTROL INCORPORATES ENHANCED TEMPERATURE CAPABILITY TO WITHSTAND HIGHER-THAN-EXPECTED-OPERATING TEMPERATURES THAT WILL EXTEND ITS FUNCTIONAL LIFE |
TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | CONTROLS/POSITIONS THE EXHAUST NOZZLE IN ORDER TO VARY ENGINE THRUST AND FAN STALL MARGIN; TRANSLATES SIGNALSRECEIVED FROM DEEC INTO MECHANICAL OUTPUT BY INCORPORATING ELECTRO/HYDRAULICSERVOVALVE AND RESOLVER, CONVERTING BLEED AIR PRESSURE |
ZZZY | REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATED BY SOURCE CONTROL DRAWING |
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