NSN 2840-01-499-7084 5102T02P06, 01-499-7084, 014997084
Product Details | AIRCRAFT GAS TURBINE ENGI COMPONENT MOUNTING PLATE
2840-01-499-7084 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: 5102T02P06, 2840-01-499-7084, 01-499-7084, 2840014997084, 014997084
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 | 01-499-7084 | 50354 ( PLATE, COMPONENT MOUNTING, AIRCRAFT GAS TURBINE ENGINE ) |
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Technical Data | NSN 2840-01-499-7084
Characteristic | Specifications |
---|---|
MATERIAL | TITANIUM ALLOY OVERALL |
OVERALL LENGTH | 34.000 INCHES NOMINAL |
MATERIAL THICKNESS | 0.115 INCHES MINIMUM AND 0.135 INCHES MAXIMUM |
SPECIAL FEATURES | MATES WITH P/N: 5102T02P05 (PLATE, FRONT CLEVIS) TO JOIN 2 SECTIONS OF P/N: 510T02 (RING, ACTUATING - FRONT FRAME); IS ROUGHLY P-SHAPED (WITHOUT HOLE); HAS 4 MOUNTING HOLES 0.250 DIA. ALONG LENGTH AND ONE HOLE 0.312 DIA. |
CRITICALITY CODE JUSTIFICATION | AGAV |
END ITEM IDENTIFICATION | GE F414-400 TURBINE GAS ENGINE; FRONT FRAME ASSY |
PART NAME ASSIGNED BY CONTROLLING AGENCY | PLATE, REAR CLEVIS |
Restrictions/Controls & Freight Information | NSN 2840-01-499-7084
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 |
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No Freight Information |