| Part Number: 114C3318-1 | Manufacturer: The Boeing Company |
| NSN : 1560-00-789-7783 (1560007897783) | Item Name : bell crank |
| CAGE Code: 81205 | FSC : 1560 Airframe Structural Components |
| Alternate P/N : 114C33181 | INC Code: 22321 |
| NIIN : 00-789-7783 (007897783) | FSG : 15 Aircraft and Airframe Structural Components |
| Country: USA | NCB Code: 00 |
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1560-00-789-7783 Item Description: Bell Crank | 1560 | 007897783 | 0 | N | A | |
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | A | 0 | |||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 114C3318-1 | 2 | 2 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AAWY | COUNTERBORE DIAMETER | 2.060 INCHES MINIMUM AND 2.061 INCHES MAXIMUM |
| AAWZ | COUNTERBORE DEPTH | 0.385 INCHES NOMINAL |
| ABXV | BORE DIAMETER | 1.880 INCHES NOMINAL |
| ADGE | BORE LENGTH | 2.560 INCHES NOMINAL |
| CZLM | CENTER TO CENTER DISTANCE BETWEEN FULCRUM AND ARM END HOLE/SLOT/BALL | 4.795 INCHES NOMINAL 1ST END |
| CZLM | CENTER TO CENTER DISTANCE BETWEEN FULCRUM AND ARM END HOLE/SLOT/BALL | 6.500 INCHES NOMINAL 2ND END |
| CZLN | END HOLE/BALL DIAMETER | 0.376 INCHES MINIMUM 2ND END AND 0.377 INCHES MAXIMUM 2ND END |
| CZLN | END HOLE/BALL DIAMETER | 0.501 INCHES MINIMUM 1ST END AND 0.502 INCHES MAXIMUM 1ST END |
| MATT | III MATERIAL | MAGNESIUM |
| STYL | STYLE DESIGNATOR | RAISED FACE PIVOT HOLE, CLEVIS BOTH ENDS |
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