ASAP Aviation Procurement is pleased to announce that part number 99870 of NSN 2915-00-369-6270 is now available and in stock. We can get you one of the fastest and most competitive quotes on this part. Part number 99870 is a Sleeve Loading manufactured by Triumph Engine Control Systems Llc under CAGE Code 11599. Simply fill out the Request for Quote (RFQ) form provided here to get started on your quote. In order to make sure that we get you your quote in a timely manner, please take the time to make sure that all fields are completely filled out, particularly the asterisk-marked (*) fields like Parts Needed By and Quantity (ea).
We will be using your response to these fields to calculate your quote. Within 15 minutes of receiving your RFQ, a member of our sales team will contact you with your quote. ASAP Aviation Procurement, owned and operated by ASAP Semiconductor, is a leading distributor of new and obsolete NSN parts for the aerospace, civil aviation, and defense industries. With our inventory of more than 2 billion parts sourced from over 5000 manufacturers from around the world, we do our level best to become your go-to one-stop shop. And to help us offer you the best streamlined parts procurement experience, we have advanced shipping facilities across USA. 99870 Triumph Engine Control Systems Llc is in stock.
Are you interested in learning more about part number 99870? If so, feel free to contact us by phone at +1-714-705-4780, or by email at sales@asap-aviationprocurement.com.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2915-00-369-6270 Item PartTypeName: SLEEVE,LOADING | 2915 | 003696270 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
99870 | 6 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
AGAV | END ITEM IDENTIFICATION | FUEL PUMP ASSEMBLY P/N 50506 |
TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY AMS4120,ANODIZE FINISH AMS2470,1.621 IN. MIN,1.623 IN. MAX O/A DIA ON FIRST END,1.128 IN. MIN,1.130 IN,MAX ID,1.470 IN. MIN,1.480 IN. MAX O/A DIA ON SECOND END,0.274 IN. MIN,0.280 IN. MAX O/A W,20 HOLES 0.920 IN. MIN,0.970 IN |
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AS9120B and ISO 9001:2015 |
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Aviation Suppliers Association Member |
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FAA AC 0056B Accredited |
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AS 6081:2012 Certification |
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ESD S20.20-2014 Certification |
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