MPN: 9531M51P01
NSN : 3040-01-200-9108
CAGE Code : 33617
Manufacturer: Electro Methods Ltd
Item Name : Bell Crank
Limitless Purchasing is your sourcing solution for all of your NSN part needs like 9531M51P01, offering rapid lead-times and competitive pricing on everything that we carry. Manufactured by Electro Methods Ltd, this Bell Crank component is listed alongside the NSN part number 9531M51P01 for your ease of procurement. With current availability for this NSN part on our website, we invite you to begin the purchasing process by filling out the RFQ form as provided below. Once received by our team members, a dedicated account manager will review and respond in 15 minutes or less with a personalized quote that accommodates your individual needs and requirements.
NSN parts are those that follow the National Stock Number system as dictated by the United Nations, allowing for easier identification, supply, and procurement of standardized materials. As a leading distributor of NSN parts, we can help customers source the new, used, and obsolete components that they need from top global NSN parts manufacturers such as Electro Methods Ltd. If you are facing an Aircraft on Ground (AOG) situation, we also offer same-day and expedited shipping for a number of items that we carry. With over 2 billion items at your disposal, Limitless Purchasing can serve as your strategic sourcing partner for all of your operational needs. Get started on the purchasing process for NSN 3040012009108 and other parts such as 9531M51P01 that you have been searching for today and see what we can do for you!
| 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 | 2 | 3 |
| 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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