Aircraft Gas Turbine Front Frame
6011T65G04
5.260 inches nominal overall length, acft eng. j-85. end item identification, frame, front part name assigned by controlling agency, steel material, navair 02b-105akb-4 reference data and literature
DAC | HCC | DMIL | RNCC |
---|---|---|---|
2 | - | - | 3 |
RNVC | SADC | MSDS | RNAAC |
---|---|---|---|
2 | - | - | SE |
A frame used for and part of the front section of an aircraft gas turbine engine. May include struts with or without variable guide vanes.
INC | FIIG | Concept | Condition |
---|---|---|---|
52345 | A522Q0 | 1 | 1 |
Details
The dimension measured along the longitudinal axis with terminated points at the extreme ends of the item.Details
The national stock number or the identification information of the end equipment for which the item is a part.Details
The name assigned to the item by the government agency or commercial organization controlling the design of the item.Details
The chemical compound or mechanical mixture properties of which the item is fabricated.Details
Literature and references available for information pertaining to the item.HMIC | PMIC | ESD/EMI | Criticality |
---|---|---|---|
N | A | - | - |
UFC | HMC | LTL | LCL |
---|---|---|---|
63220 | - | W | M |
RVC | WCC | TCC | SHC |
---|---|---|---|
1 | 671 | Z | 9 |
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