We appreciate your interest in General Electric Company part number 1441M31P06, which is currently ready for procurement here on Prompt Aerospace. For your reference, part number 1441M31P06 is listed with the NSN 2840-01-307-6361 and description “Lock Turbine Rotor Blade Aircraf.” If this is the item you are seeking and you would like to request a quote for your comparisons, simply complete the form below with information like your desired quantity, budget, and anticipated fulfillment timeframe. We regularly respond to requests within 15 minutes of receiving them, using the details we are offered to curate the most ideal purchasing options.
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If you want to explore other items produced by General Electric Company under the CAGE Code 07482 or that similarly fall under the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components, keep in mind that since we list everything with relevant information, you can easily locate related part numbers using our search engine or catalogs. We also excel at tracking down parts with long lead times or that are generally hard to find, meaning that we can serve you even if you do not see exactly what you need on our website. With all of this being said, we are ready to help you source any of the NSN 2840-01-307-6361 parts and Lock Turbine Rotor Blade Aircraf items your operations require, so request a quote today.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-307-6361 Item PartTypeName: LOCK,TURBINE ROTOR BLADE,AIRCRAF | 2840 | 013076361 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
KDS 2840-4003 | 2 | 1 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 0.666 INCHES MINIMUM AND 0.676 INCHES MAXIMUM |
ABMK | OVERALL WIDTH | 0.658 INCHES NOMINAL |
ABPX | MATERIAL THICKNESS | 0.074 INCHES MINIMUM AND 0.083 INCHES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | F110GE129 ACFT ENGINE |
FEAT | SPECIAL FEATURES | USED ON THE REAR HIGH PRESSURE TURBINE |
MATT | MATERIAL | TITANIUM |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | C50TF70,CL-A MFR REF SINGLE MATERIAL RESPONSE |
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