Aircraf Component Mounting Plate
707853
1.590 inches minimum and 1.610 inches maximum overall length, tf-30 aircraft gas turbine engine end item identification, czbj and abhp and agav criticality code justification, original name boss,combustion chamber,turbine engine part name assigned by controlling agency, combustion chamber engine section location, nickel alloy overall material
| DAC | HCC | DMIL | RNCC |
|---|---|---|---|
| 2 | - | - | 3 |
| RNVC | SADC | MSDS | RNAAC |
|---|---|---|---|
| 2 | - | - | SX |
A metallic item of various shapes designed to reduce vibration and to secure a component part of an engine, gas turbine, aircraft to the engine case or housing as modified. For mounting accessories to the outside of the engine, see plate, mounting.
| INC | FIIG | Concept | Condition |
|---|---|---|---|
| 50354 | A530F0 | - | 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 master requirement codes of those requirements which are technically critical by reason of tolerance,fit,performance,or other characteristics which affect identification of the item.Details
The name assigned to the item by the government agency or commercial organization controlling the design of the item.Details
Indicates the location of the item on the engine section.Details
The chemical compound or mechanical mixture properties of which the item is fabricated.Details
The specification, standard, or manufacturer's reference and the classification designation, such as class, condition, temper, and the like, that identifies the material.| HMIC | PMIC | ESD/EMI | Criticality |
|---|---|---|---|
| N | U | - | - |
| UFC | HMC | LTL | LCL |
|---|---|---|---|
| 04720 | - | W | - |
| RVC | WCC | TCC | SHC |
|---|---|---|---|
| - | 671 | Z | 9 |
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When the NSN 2840-00-003-9754 was assigned to the Federal Catalog?
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