Aircraft Stiffener Rib
No.3 flap wing panel aircraft location, b-1b aircraft mission design series, c/o 1 seal,1 stud,3 bushing,1 rib,1 insert; nha l1804003 special features
DAC | HCC | DMIL | RNCC |
---|---|---|---|
2 | - | - | 3 |
RNVC | SADC | MSDS | RNAAC |
---|---|---|---|
2 | - | - | MF |
A vertical, relatively short, rib located in a fuselage, nacelle, pod, and the like. It follows the periphery and provides additional rigidity. It may join various components such as stringers, longerons, and the like. It is supplementary to the frames and blukheads. See also rib (1), airfoil.
INC | FIIG | Concept | Condition |
---|---|---|---|
41027 | A11400 | 1 | 1 |
Details
Indicates the location at which the item is used in the aircraft.Details
The series of letters and numbers which identify the basic aircraft mission and any additional modification or design changes.Details
Those unusual or unique characteristics or qualities of an item not covered in the other requirements and which are determined to be essential for identification on one or more other functions.HMIC | PMIC | ESD/EMI | Criticality |
---|---|---|---|
P | A | - | - |
UFC | HMC | LTL | LCL |
---|---|---|---|
63220 | - | W | M |
RVC | WCC | TCC | SHC |
---|---|---|---|
- | 671 | Z | Z |
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