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68A112163-2019 — PLATE,STRUCTURAL,AIRCRAFT

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

68A112163-2019: PLATE,STRUCTURAL,AIRCRAFT.

The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 12.000 INCHES NOMINAL IN, overall_length: 81.000 INCHES NOMINAL IN, aircraft_location: SPLICE-PLATE,INNER WING-UPPER, material_thickness: 0.750 INCHES NOMINAL IN, aircraft_station_number: XW155.024. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-114-9155, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.

Verify compatibility with your specific system configuration before ordering.

WHERE IT FITS
68A112163-2019
NSN: 1560-01-114-9155
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)
SPECIFICATIONS
materialALUMINUM ALLOY 2024
overall_width12.000 INCHES NOMINAL IN
overall_length81.000 INCHES NOMINAL IN
aircraft_locationSPLICE-PLATE,INNER WING-UPPER
material_thickness0.750 INCHES NOMINAL IN
aircraft_station_numberXW155.024
aircraft_mission_design_seriesF-15
material_document_and_classificationQQ-A-250/4-T851 FED SPEC SINGLE MATERIAL RESPONSE
NSN1560-01-114-9155
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available PLATE,STRUCTURAL,AIRCRAFT TITLE COMPONENT PN 68A112163-2019 MFR PLATE,STRUCTURAL,AIRCR
KEY FEATURES
•
AIRCRAFT STATION NUMBER: XW155.024
•
MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/4-T851 FED SPEC SINGLE MATERIAL RESPONSE
•
MATERIAL THICKNESS: 0.750 INCHES NOMINAL IN
•
AIRCRAFT LOCATION: SPLICE-PLATE,INNER WING-UPPER
•
MATERIAL: ALUMINUM ALLOY 2024
•
AIRCRAFT MISSION DESIGN SERIES: F-15
TECHNICAL CHARACTERISTICS
AIRCRAFT STATION NUMBERXW155.024
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-250/4-T851 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH81.000 INCHES NOMINAL IN
OVERALL WIDTH12.000 INCHES NOMINAL IN
MATERIAL THICKNESS0.750 INCHES NOMINAL IN
AIRCRAFT LOCATIONSPLICE-PLATE,INNER WING-UPPER
MATERIALALUMINUM ALLOY 2024
AIRCRAFT MISSION DESIGN SERIESF-15
OTHER ITEMS IN FSC 1560 — Airframe Structural Components
Items in the same Federal Supply class. No interchangeability or substitution relationship is implied.
1560-00-000-0047 1560-00-001-1849 1560-00-001-1850 1560-00-001-1851 1560-00-001-2368 1560-00-001-2478 1560-00-001-2479 1560-00-001-2480
SUBSTITUTES & CROSS-REFERENCES 1
68A112163-2017Same NSN cross-reference
Same NSN cross-reference
Also cataloged under this NSN
LIFECYCLE
NSN statusActive· U.S. Government catalog
Acquisition advice: Normally procured from the manufacturer (OEM)Demilitarization required — critical (Q)
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FREQUENTLY ASKED QUESTIONS
What is 68A112163-2019?
68A112163-2019 is a PLATE,STRUCTURAL,AIRCRAFT.
What parts can replace 68A112163-2019?
There is 1 known substitute for 68A112163-2019: 68A112163-2017. Substitute compatibility should be verified for your specific system.
What is the NSN for 68A112163-2019?
68A112163-2019 is cataloged in the U.S. Government catalog under NSN 1560-01-114-9155. This indicates validated use in U.S. government and defense supply chains.
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