Mfg Part Number: 4F11869-101A
Alternate P/N: 4F11869101A
NSN : 1680-00-110-2891
NIIN : 001102891
CAGE Code : 59213
Manufacturer: Aerocomponents Ltd
Item Name : Lever Remote Contro
In our inventory, we have more than two billion new and obsolete NSN part like 4F11869-101A. Aviation Sphere can offer an impressive selection of NSN parts. This includes parts like 4F11869-101A Lever Remote Contro from manufacturer Aerocomponents Ltd and many more, all of which are available with short lead times and competitive prices. For parts not in our inventory, our dedicated account managers can help you track them down through our international supply chain network that extends across the United States, Canada, and the United Kingdom. Furthermore, Aviation Sphere is an AS9120B, ISO 9001:2015, and FAA AC 0056B accredited business, as well as the only independent distributor with a strict No China Sourcing Pledge, allowing us to ensure that each part part like 4F11869-101A, you purchase from us is fully traceable or comes directly from its manufacturer.
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NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1680-00-110-2891 Item Description: Lever Remote Contro | 1680 | 001102891 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
4f11869-101a | 2 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
ASBP | BORE TYPE | SERRATED |
BFGW | CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES | 1.500 INCHES NOMINAL |
BFGX | SHAFT END THICKNESS | 0.590 INCHES NOMINAL |
BFGY | LINK END THICKNESS | 0.590 INCHES NOMINAL |
BFHA | LINK END HOLE DIAMETER | 0.251 INCHES MINIMUM AND 0.258 INCHES MAXIMUM |
BFHN | DISTANCE BETWEEN FORK INSIDE SPREAD | 0.344 INCHES MINIMUM AND 0.349 INCHES MAXIMUM |
CZLP | SHAFT SECURING METHOD | SERRATIONS |
MATT | III MATERIAL | ALUMINUM ALLOY |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-225/9, T651 FED SPEC SINGLE MATERIAL RESPONSE |
STYL | STYLE DESIGNATOR | CLEVIS LINK END, SECURING HOLE(S) SHAFT END |
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