You are currently exploring our in-stock options for part number 60B89004-16 with the NSN 4320015734316. This product is listed with the description “Pump Subassembly Ce” and is manufactured by The Boeing Company. 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 60B89004-16 is listed alongside the NSN 4320-01-573-4316 and belongs to the FSC 4320 Power And Hand Pumps. Additionally, it is also under the CAGE Code 81205, which is assigned to The Boeing Company. 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 60B89004-16 seamless.
| MRC | Criteria | Characteristic |
|---|---|---|
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
| CXCY | III PART NAME ASSIGNED BY CONTROLLING AGENCY | MOTOR-IMPELLER SUBASSEMBLY |
| FEAT | SPECIAL FEATURES | THIS COMPONENT IS SUBJECT TO CRITICAL DESIGN CONFIGURATION CONTROL LIMITATIONS (CDCCLS) AS DEFINED AND CONTROLLED BY SPECIAL FEDERAL REGULATION (SFAR) 88; DO NOT ATTEMPT TO MAINTAIN, REPAIR, REBUILD, OVERHAUL OR REMANUFACTURE THIS UNIT EXCEPT IN STRICT ACCORDANCE WITH THE METHODS, TECHNIQUES AND PRACTICES SPECIFIED IN THE COMPONENT MAINTENANCE MANUAL; ANY USE OF PARTS, METHODS, TECHNIQUES OR PRACTICES NOT CONTAINED IN THE CMM MUST BE APPROVED BY THE FAA OFFICE RESPONSIBLE FOR THE AIRPLANE MODE TYPE CERTIFICATE, OR APPLICABLE REGULATORY AGENCY |
| ALCD | III USAGE DESIGN | AC MOTOR DRIVEN SELF-PRIMARY OVERRIDE PUMP |
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