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| Item Name | Cover Access Aircra |
| Federal Supply Group (FSG) | Aircraft and Airframe Structural Components |
| Federal Supply Class (FSC) | 1560 Airframe Structural Components |
| National Item Identification Number (NIIN) | 00-073-4702 (000734702) |
| NCB Code | USA (00) |
| Manufacturer | Northrop Grumman Systems Corporation, Northrop Grumman Technical Services Inc |
| MRC | Criteria | Characteristic |
|---|---|---|
| AAGR | CROSS-SECTIONAL SHAPE STYLE | FLAT |
| ABGL | WIDTH | 2.985 INCHES MINIMUM AND 3.000 INCHES MAXIMUM |
| ABMW | PERIPHERAL SHAPE STYLE | RECTANGLE,TWO HOLES |
| ABRY | LENGTH | 5.730 INCHES MINIMUM AND 5.750 INCHES MAXIMUM |
| ADPA | DISTANCE BETWEEN HOLE CENTERLINE AND FIRST HOLE ALONG LENGTH | 5.365 INCHES MINIMUM AND 5.370 INCHES MAXIMUM |
| ADPB | DISTANCE BETWEEN HOLE CENTERLINE AND FIRST HOLE ALONG WIDTH | 1.120 INCHES MINIMUM AND 1.130 INCHES MAXIMUM |
| ADPC | DISTANCE FROM FIRST HOLE CENTERLINE TO END ALONG LENGTH | 0.192 INCHES MINIMUM AND 2.002 INCHES MAXIMUM |
| ADPD | DISTANCE FROM FIRST HOLE CENTERLINE TO END ALONG WIDTH | 0.933 INCHES MINIMUM AND 0.943 INCHES MAXIMUM |
| ADPR | BODY THICKNESS | 0.063 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | F-5 AIRCRAFT |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5,T3 FED SPEC SINGLE MATERIAL RESPONSE |
| SFTT | SURFACE TREATMENT | ANODIZE |
| ZZZV | FSC APPLICATION DATA | WING,AIRFRAME |
| Relevant Components for NSN - 1560-00-073-4702, 1560000734702 | ||||
| 1560-01-554-4660 (1560015544660) | 1560-01-465-6016 (1560014656016) | 1560-00-873-3011 (1560008733011) | 1560-01-445-9850 (1560014459850) | |
| 1560-00-098-0168 (1560000980168) | 1560-00-251-5490 (1560002515490) | 1560-01-621-9290 (1560016219290) | 1560-01-544-3961 (1560015443961) | |
| 1560-00-531-6887 (1560005316887) | 1560-00-146-2205 (1560001462205) | 1560-00-870-4445 (1560008704445) | 1560-01-611-0493 (1560016110493) | |
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