NSN 1560-01-388-2887 01-388-2887, 013882887
Product Details | AIRCRAFT FAIRING
1560-01-388-2887 A secondary structure whose function is to reduce drag by providing a streamlined surface or covering.
Part Alternates: 1560-01-388-2887, 01-388-2887, 1560013882887, 013882887
Aircraft and Airframe Structural Components | Airframe Structural Components
| Supply Group (FSG) | NSN Assign. | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 15 | 01-388-2887 | 41334 ( FAIRING, AIRCRAFT ) |
Cross Reference | NSN 1560-01-388-2887
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 68A250750-2005 | 76301 | BOEING COMPANY, THE DBA BOEING |
| 68A250750-2069 | 76301 | BOEING COMPANY, THE DBA BOEING |
| 68A250750-2075 | 58074 | HOWMET CORPORATION DBA HOWMET TICAST DIV TICAST |
| 68A250750-2075 | 76301 | BOEING COMPANY, THE DBA BOEING |
| 68A250796 | 76301 | BOEING COMPANY, THE DBA BOEING |
| 68A250796-2007 | 58074 | HOWMET CORPORATION DBA HOWMET TICAST DIV TICAST |
| 68A250796-2007 | 76301 | BOEING COMPANY, THE DBA BOEING |
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Related Products | NSN 1560-01-388-2887
Technical Data | NSN 1560-01-388-2887
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY |
| AIRCRAFT LOCATION | PYLON ASSY,AFT OUTBOARD,CONFORMALFUEL TANK |
| AIRCRAFT MISSION DESIGN SERIES | F-15 |
| MATERIAL THICKNESS | 4.500 INCHES NOMINAL |
| MANUFACTURERS CODE | 76301 |
| DESIGN CONTROL REFERENCE | 68A250750-2069 |
Restrictions/Controls & Freight Information | NSN 1560-01-388-2887
| Category | Code | Description |
|---|---|---|
| Hazardous Material Indicator Code | P | There is no information in the HMIS; however, the NSN is in an FSC in Table II of Federal Standard 313 and an MSDS may be required by the user. The requirement for an MSDS is dependent on a hazard determination of the supplier or the intended end use of the product |
| Category | Code | Description |
|---|---|---|
| No Freight Information | ||



