We appreciate your interest in Boeing Company The part number 74A733095-2001, which is currently ready for procurement here on Prompt Aerospace. For your reference, part number 74A733095-2001 is listed with the NSN 1640-01-593-7582 and description “Clevis Rod End Aviation.” If this is the item you are seeking and you would like to request a quote for your comparisons, simply complete the form below with information like your desired quantity, budget, and anticipated fulfillment timeframe. We regularly respond to requests within 15 minutes of receiving them, using the details we are offered to curate the most ideal purchasing options.
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If you want to explore other items produced by Boeing Company The under the CAGE Code 76301 or that similarly fall under the FSC 1640 Aircraft Control Cable Products, keep in mind that since we list everything with relevant information, you can easily locate related part numbers using our search engine or catalogs. We also excel at tracking down parts with long lead times or that are generally hard to find, meaning that we can serve you even if you do not see exactly what you need on our website. With all of this being said, we are ready to help you source any of the NSN 1640-01-593-7582 parts and Clevis Rod End Aviation items your operations require, so request a quote today.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1640-01-593-7582 Item PartTypeName: CLEVIS,ROD END,AVIATION | 1640 | 015937582 | 0 | N | A | |
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | A | 0 | |||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
10399995 | 5 | 9 | 6 |
MRC | Criteria | Characteristic |
---|---|---|
FEAT | Special Features | ROD END-ADJUSTABLE; UMBILICAL ACTUATING; MATERIAL IS ALUMINUM BRONZE ALLOY IAW SAE AMS 4640. THIS CLEVIS ALSO HAS A HOLE THROUGH THE BODY OF THE CLEVIS 0.950 FROM THE CENTER OF THE SLOTED HOLE TO THE END OF THE ROD END OF THE CLEVIS. THE WHOLE, SLOTTED IS 0.312 INCHES IN DIAMETER. THIS CLEVIS HAS A POLYURETHANE COATING AND EPOXY PRIMER COATINGS. THE CLEVIS HAS TWO FLAT SIDES OPPOSITE OF EACH OTEHR AND RUN THE LENGTH OF THE CLEVIS. THIS CLEVIS IS A TYPE I, CLASS H. THREAD SIZE IS 0.250-28 UNJF - 3B. |
AGAV | End Item Identification | (NON-HSP) FIGHTER SUPPORT AIRCRAFT (F/A-18) |
BCLP | Hole Shape | ROUND |
CXCY | Part Name Assigned By Controlling Agency | CLEVIS,ROD END-ADJUSTABLE UMBILICAL ACTUATING |
AAUB | Hole Diameter | 0.312 INCHES NOMINAL |
THSD | Thread Series Designator | UNJF OVERALL |
AKYC | Rod Connection Bore Diameter | 0.250 INCHES NOMINAL |
AKYH | Distance From Center Of Securing Pin Hole To Rod End | 1.430 INCHES NOMINAL |
AKYE | Securing Pin Hole Diameter | 0.191 INCHES NOMINAL AND 0.197 INCHES MAXIMUM |
CQJX | Nominal Thread Size | 0.250 INCHES OVERALL |
MRC | Decoded Requirement | Clear Text Reply |
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