| Alternative NSN: 1560-01-642-2020 |
| Item Name: Panel Structural Ai |
| CAGE Code : 1PT53 , 12255 |
| NIIN: 016422020 |
| FSC Name: 1560 Airframe Structural Components |
| NCB Code: USA (01) |
| Manufacturers: e d n aviation inc , united states department of the army |
|
Part No Part No
|
Manufacturer |
Item Name Item Name
|
QTY QTY
|
RFQ RFQ
|
|---|---|---|---|---|
| 3392AS1817-2 | e d n aviation inc | panel structural ai | Avl | |
| 3392AS1817-2 | united states department of the army | panel structural ai | Avl |
| MRC | Criteria | Characteristic |
|---|---|---|
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | PANEL,STRUCTURAL COMPONENT,AIRCRAFT |
| ABMK | OVERALL WIDTH | 3.75 INCHES NOMINAL |
| FEAT | SPECIAL FEATURES | SYSTEM USED ON MH-60S FFFW;NEXT HIGHER ASSEMBLY 3392AS1818;EDGE LIGHT PANEL ASSEMBLY;PANEL SHALL BE ACCORDANCE WITH MIL-DTL-7788, CLASS-NVIS GREEN A, IN ACCORDANCE WITH MIL-L-85762, TYPE V, 5V AC. THE FRONT PANEL CURRENT SHALL NOT EXCEED 0.75 AMPS. PANEL SHALL BE BLACK COLOR NO. 37038;PANEL TEMPERATURE REQUIREMENTS SHALL BE IN ACCORDANCE WITH MIL-E-5400, PARAGRAPH 3.2.24.1 FOR CLASS 1A EQUIPMENT;TOUCH TEMPERATURE SHALL CONFORM TO MIL-HDBK-454, GUIDANCE 1, PARAGRAPH 4.4;PANEL SHALL WITH STAND EXPOSURE TO FUNGUS GROWTH IN ACCORDANCE WITH MIL-STD-810F, METHOD 508.5 IN OPERATING CONDITIONS |
| ABHP | OVERALL LENGTH | 5.75 INCHES NOMINAL |
| MATT | MATERIAL | ALUMINUM ALLOY 6061 |
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