You are currently exploring our in-stock options for part number 856A1154P01 with the NSN 4920011683561. This product is listed with the description “Master Set Up Compr” and is manufactured by Cfm International 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 856A1154P01 is listed alongside the NSN 4920-01-168-3561 and belongs to the FSC 4920 Aircraft Maintenance And Repair Shop Specialized Equipment. Additionally, it is also under the CAGE Code 58828, which is assigned to Cfm International 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 856A1154P01 seamless.
| MRC | Criteria | Characteristic |
|---|---|---|
| FTLD | Functional Description | USED TO ALIGN CHUCK/TABLE 856A1155 |
| MRC | Decoded Requirement | Clear Text Reply |
| FEAT | Special Features | HC/O HARDENED STEEL; OD 5.280 IN.; ID 3.900 IN.; TWO BANDS ONE FINISHED TO 4.714 IN. MIN,4.715 IN. MAX DIA AND THE OTHER TO 4.941 IN. MIN,4.945 IN. MAX DIA,ARE PROVIDED NEAR ONE END OF THE MASTER TO SIMULATE THE DIA OF THE ROTOR THAT ENGAGES THE FORWARD ROTOR IN THE ENGINE;AFT END OF THE MASTER HAS FINISHED DIA OF 4.820 IN. HELD VERY ACCURATELY CYLINDRICALLY; ONE 1.000 IN. DIA HOLE AFT END FOR HANDLING; GRAY ENAMEL FINISH ON 5.280 DIA; 28.000 IN. LG O/A |
| AGAV | End Item Identification | KC-135R CFM56 (F108-CF-100) ENGINE |
| CXCY | Part Name Assigned By Controlling Agency | COMPRESSOR ROTOR BUILD MASTER SET UP |
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