You are currently exploring our in-stock options for part number 1602M28P02 with the NSN 2840013574327. This product is listed with the description “Slider Divergent Flap Turbine En” and is manufactured by Silco Engineering And Manufacturing Inc. If you are looking to purchase this part, we encourage you to complete and submit the RFQ form below with as much information as you can provide, such as your desired quantity, budget, shipping time frame, and more. Within 15 minutes of receiving and reviewing your submission, one of our experts will reach out with a quote that is tailored to your needs.
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We supply all relevant information alongside the listings on our website, that way you know you are always getting the exact item you require. For example, part number 1602M28P02 is listed alongside the NSN 2840-01-357-4327 and belongs to the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Additionally, it is also under the CAGE Code 0EDL9, which is assigned to Silco Engineering And Manufacturing Inc. At Aerospace Procurement, you can trust that each product in our inventory is up to industry standards, as we are committed to various quality assurance practices. For example, we uphold a strict NO CHINA SOURCING pledge to ensure that each part is shipped out alongside its manufacturer trace documentation and qualifying certifications. These practices and more allow us to operate with AS9120B, ISO 9001:2015, and FAA AC 00-56B accreditation. Get in contact with us today to see how we can make the procurement process for part number 1602M28P02 seamless.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-357-4327 Item PartTypeName: SLIDER,DIVERGENT FLAP,TURBINE EN | 2840 | 013574327 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
1602M28P02 | 6 | 2 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 0.510 INCHES MINIMUM AND 0.514 INCHES MAXIMUM |
CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
ABMK | OVERALL WIDTH | 0.443 INCHES MINIMUM AND 0.447 INCHES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | F110-GE-100 AIRCRAFT ENGINE |
MATT | MATERIAL | NICKEL ALLOY |
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