Mfg Part Number: 9531M51P01 | Manufacturer: Electro Methods Inc | NSN : 3040-01-200-9108 |
Item Name : Bell Crank | CAGE Code : 33617 | FSC : 3040 Miscellaneous Power Transmission Equipment |
On Stacked Aviation, we can help customers procure all the NSN components that they need with ease, including those such as NSN 3040-01-200-9108 by Electro Methods Inc. This Bell Crank part is listed alongside the part number 9531M51P01, and it is currently available for purchase from our website at any time. If you would like a quote on this item for your comparisons, we ask you to fill out and submit the RFQ form as provided below. As you complete our form, please provide us with as much detail as you can regarding your particular needs so that we may best personalize a solution that accommodates your individual requirements.
As an AS9120B, ISO 9001:2015, and FAA AC 00-56B certified and accredited enterprise, we go above and beyond to ensure that every part you purchase is of the highest quality. With this promise, we choose to only work with leading global manufacturers that we trust, including those such as Electro Methods Inc. Additionally, we list our items with all necessary details so that you can always be sure that you are purchasing exactly what you need. As such, many items are listed alongside their CAGE Code, such as how NSN 3040-01-200-9108 is listed as an item being produced under the CAGE Code 33617. Get started on the part procurement process and experience how we can serve as your strategic sourcing partner today.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
3040-01-200-9108 Item Description: Bell Crank | 3040 | 012009108 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
9531m51p01 | 6 | 9 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
ABXV | BORE DIAMETER | 0.6535 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | TF-33-P-7 (C-141 A/B) AIRCRAFT ENGINE. F110-GE-400 AIRCRAFT ENGINE. F110-GE-100/129 (F-16 C/D) AIRCRAFT ENGINE. F-108 (CFM-56, KC-135A) AIRCRAFT ENGINE. F-16 AIRCRAFT. |
CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
CZLM | CENTER TO CENTER DISTANCE BETWEEN FULCRUM AND ARM END HOLE/SLOT/BALL | 1.870 INCHES NOMINAL 1ST END |
CZLM | CENTER TO CENTER DISTANCE BETWEEN FULCRUM AND ARM END HOLE/SLOT/BALL | 2.112 INCHES NOMINAL 2ND END |
CZLN | END HOLE/BALL DIAMETER | 0.3125 INCHES NOMINAL 2ND END |
CZLN | END HOLE/BALL DIAMETER | 0.3745 INCHES NOMINAL 1ST END |
FEAT | SPECIAL FEATURES | WEAPON SYSTEM ESSENTIAL |
MATT | III MATERIAL | STEEL |
STYL | STYLE DESIGNATOR | FLAT, ONE OR MORE HOLES BOTH ARMS |
ZZZV | FSC APPLICATION DATA | ACFT ENG F-110 |
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