| Part Number: 16B1582-39 | Manufacturer: Elbit System Cyclone Ltd |
| NSN : 1560-01-106-7657 (1560011067657) | Item Name : door access aircraft |
| CAGE Code: 0600A | FSC : 1560 Airframe Structural Components |
| Alternate P/N : 16B158239 | INC Code: 51576 |
| NIIN : 01-106-7657 (011067657) | FSG : 15 Aircraft and Airframe Structural Components |
| Country: USA | NCB Code: 01 |
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1560-01-106-7657 Item Description: Door Access Aircraft | 1560 | 011067657 | 0 | P | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 16b1582-39 | 6 | 1 | C | 9 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AAGR | CROSS-SECTIONAL SHAPE STYLE | ARCHED |
| ABGL | WIDTH | 23.000 INCHES NOMINAL |
| ABMW | PERIPHERAL SHAPE STYLE | RECTANGLE, MULTI HOLES |
| ABRY | LENGTH | 26.000 INCHES NOMINAL |
| ADNV | HOLE QUANTITY ALONG LENGTH | 10 |
| ADNW | HOLE QUANTITY ALONG WIDTH | 11 |
| ADNY | DISTANCE BETWEEN HOLES ALONG LENGTH | 2.920 INCHES NOMINAL |
| ADNZ | DISTANCE BETWEEN HOLES ALONG WIDTH | 1.564 INCHES NOMINAL |
| ADPA | DISTANCE BETWEEN HOLE CENTERLINE AND FIRST HOLE ALONG LENGTH | 1.080 INCHES NOMINAL |
| ADPB | DISTANCE BETWEEN HOLE CENTERLINE AND FIRST HOLE ALONG WIDTH | 2.660 INCHES NOMINAL |
| ADPC | DISTANCE FROM FIRST HOLE CENTERLINE TO END ALONG LENGTH | 1.640 INCHES NOMINAL |
| ADPD | DISTANCE FROM FIRST HOLE CENTERLINE TO END ALONG WIDTH | 2.270 INCHES NOMINAL |
| ADPK | CORNER HOLE CENTERLINE RADIUS | 0.125 INCHES NOMINAL |
| ADPQ | INSIDE CORNER RADIUS | 3.137 INCHES NOMINAL |
| ADPR | BODY THICKNESS | 0.550 INCHES NOMINAL |
| ADQB | SECURING DEVICE TYPE | HINGE AND TURNLOCK FASTENER |
| AGAV | END ITEM IDENTIFICATION | F-16 |
| FEAT | SPECIAL FEATURES | RH LOWER STRAKE FS190 TO FS217 |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 AND ALUMINUM ALLOY 6061 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/4 FED SPEC 1ST MATERIAL RESPONSE AND QQ-A-250/11 FED SPEC 2ND MATERIAL RESPONSE |
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