NSN 2840-01-499-7083 5102T02P05, 01-499-7083, 014997083
Product Details | AIRCRAFT GAS TURBINE ENGI COMPONENT MOUNTING PLATE
2840-01-499-7083 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.
Part Alternates: 5102T02P05, 2840-01-499-7083, 01-499-7083, 2840014997083, 014997083
Engines, Turbines, and Components | Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
| Supply Group (FSG) | NSN Assign. | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | 01-499-7083 | 50354 ( PLATE, COMPONENT MOUNTING, AIRCRAFT GAS TURBINE ENGINE ) |
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Technical Data | NSN 2840-01-499-7083
| Characteristic | Specifications |
|---|---|
| MATERIAL | TITANIUM ALLOY OVERALL |
| MATERIAL DOCUMENT AND CLASSIFICATION | SAE-AMS 4911 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| OVERALL LENGTH | 34.000 INCHES NOMINAL |
| MATERIAL THICKNESS | 0.115 INCHES MINIMUM AND 0.135 INCHES MAXIMUM |
| SPECIAL FEATURES | MATES WITH P/N: 5102T02P06: PLATE, REAR CLEVIS TO JOIN 2 SECTIONS OF P/N 5102T02: RING, ACTUATING - FRONT FRAME; ROUGHLY P-SHAPED (WITHOUT HOLE); HAS 4 MOUNTING HOLES, 0.2500-0.2505 INCH IN DIA. ALONG LENGTH AND ONE HOLE IN PROTRUDING PART, 0.3120-0.3125 INCH IN DIA. |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | GE F414-400 TURBINE GAS ENGINE; FRONT FRAME ASSY; RING, ACTUATING - FRONT FRAME |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | PLATE, FRONT CLEVIS |
Restrictions/Controls & Freight Information | NSN 2840-01-499-7083
| Category | Code | Description |
|---|---|---|
| Hazardous Material Indicator Code | N | There is no data in the HMIS and the NSN is in an FSC not generally suspected of containing hazardous materials |
| Category | Code | Description |
|---|---|---|
| No Freight Information | ||