Mfg Part Number: A138992
NSN : 3040-00-103-9186
NIIN : 001039186
CAGE Code : 53591
Manufacturer: Schwitzer Engine Components
Item Name : Shaft Turbine
Here at Internet For Aviation, we have A138992 Shaft Turbine from Schwitzer Engine Components, as well as a variety of other parts from reliable manufacturers. As the only independent distributor with a No China Sourcing policy, we go to great lengths to ensure that we source responsibly when it comes to certified standard items. If you’re in need of a specific A138992 to aid you in your aircraft repair capabilities, simply search by NSN part number, NSN or Cage Code on our parts directory. Submit an instant RFQ and a representative will get back to you in as little as 15 minutes.
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We pride ourselves in our abilities to deliver quality superior grade aviation parts in a timely schedule. Thanks to the various supply chain locations that we have across the United States. We can execute fast shipping times that outpace our competitors. Unlike other competitors, we can promise same day shipping and delivery right to the very place you need. We’re leaders in our industry thanks to our parts streamlining process which includes quick stock and acquisition of the certified product and fast shipping. For whatever needs you have, be they Shaft Turbine and A138992 parts, we can procure and deliver in a schedule that fits with you! Contact us today for an immediate quote!
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
3040-00-103-9186 Item Description: Shaft Turbine | 3040 | 001039186 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | U | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
A138992 | 5 | 9 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | STEEL SHAFT,CRES IMPELLER; 9.000 IN. O/A LG; ONE END THREADED; 1/2-20 UNF @RH 2A THD; 0.688 IN. LG OF THD; 0.500 IN. OD FIRSTSTEP OF SHAFT; 2.375 IN. LG OF FIRST STEP; 0.686 IN.OD SECOND STEP OF SHAFT; 3.062 IN. LG SECOND STEP OF SHAFT; 0.8 |
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