Thank you for your continued interest in sourcing the NSN 3040-01-200-9108 (Bell Crank) components you require from Integrated AOG. Below, you may locate all items with the NSN 3040-01-200-9108, including in-demand part numbers like 9531M51P01, and more! As an ASAP Semiconductor owned and operated purchasing platform, we proudly operate with AS9120B, ISO 9001:2015, and FAA AC 00-56B accreditation, in tandem with a strict No China Sourcing pledge. This allows us to ensure all products in our inventory of over 2 billion parts are vetted for fit and function before shipment to you, alongside their applicable trace documentation. To begin procuring any of the NSN 3040-01-200-9108 parts from Electro Methods Ltd, Tss Technologies Inc, Lpi Industries Corporation, General Electric Inc, Edac Technologies Corporation, simply fill out and submit a Request for Quote (RFQ) form outlining any pertinent details regarding your part needs, and we will provide you with a competitive quote within 15 minutes or less. Offering rapid lead times and competitive pricing, find out why loyal customers rely on us time and time again. To learn more, contact us at any time via phone or email.
Item Name | Bell Crank |
Federal Supply Class (FSC) | 3040 Miscellaneous Power Transmission Equipment |
NIIN | 01-200-9108 (012009108) |
NCB Code | USA (01) |
Part No | Manufacturer | Item Name | QTY | RFQ |
---|---|---|---|---|
9531M51P01 | electro methods ltd | bell crank | Avl | RFQ |
9531M51P01 | tss technologies inc | bell crank | Avl | RFQ |
9531M51P01 | lpi industries corporation | bell crank | Avl | RFQ |
9531M51P01 | general electric inc | bell crank | Avl | RFQ |
9531M51P01 | edac technologies corporation | bell crank | Avl | RFQ |
9531M51P01 | jet engine technology corporation | bell crank | Avl | RFQ |
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 |
3010-00-001-0013 (3010000010013) | 3010-00-001-0069 (3010000010069) | 3010-00-001-2168 (3010000012168) | 3010-00-001-2173 (3010000012173) |
3010-00-001-3588 (3010000013588) | 3010-00-001-5963 (3010000015963) | 3010-00-001-6187 (3010000016187) | 3010-00-001-6188 (3010000016188) |
3010-00-001-6189 (3010000016189) | 3010-00-001-6191 (3010000016191) | 3010-00-001-6230 (3010000016230) | 3010-00-001-6242 (3010000016242) |
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