Product Details | AIRCRAFT SPAR

1560-01-138-2406 A principal spanwise member of the structural framework of a wing, stabilizer, other airfoil, and the like. It is designed to absorb bending loads applied to the airfoil.

Part Alternates: 1560-01-138-2406, 01-138-2406, 1560011382406, 011382406

Aircraft and Airframe Structural Components | Airframe Structural Components

Supply Group (FSG) NSN Assign. NIIN
15 01-138-2406

Cross Reference | NSN 1560-01-138-2406

Part Number Cage Code Manufacturer
68A112107-2030 76301 BOEING COMPANY, THE DBA BOEING
68A112107-2034 76301 BOEING COMPANY, THE DBA BOEING
68A112107-2040 76301 BOEING COMPANY, THE DBA BOEING
68A112107-2042 76301 BOEING COMPANY, THE DBA BOEING
68A112107-2050 76301 BOEING COMPANY, THE DBA BOEING
68A112107-2076 76301 BOEING COMPANY, THE DBA BOEING

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Technical Data | NSN 1560-01-138-2406

Characteristic Specifications
AIRCRAFT LOCATION REAR INBOARD TORQUE BOX
AIRCRAFT MISSION DESIGN SERIES F-15

Restrictions/Controls & Freight Information | NSN 1560-01-138-2406

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