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
15 01-388-2887

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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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 CodePThere 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