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68A118114-2001 — PLATE,STRUCTURAL,AIRCRAFT

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

68A118114-2001: PLATE,STRUCTURAL,AIRCRAFT.

The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 3.240 INCHES NOMINAL IN, overall_length: 11.300 INCHES NOMINAL IN, aircraft_location: DOUBLER-OUTBOARD LEADING EDGE, material_thickness: 0.032 INCHES NOMINAL IN, aircraft_station_number: XFS208.7. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-356-3689, 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
68A118114-2001
NSN: 1560-01-356-3689
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)
SPECIFICATIONS
materialALUMINUM ALLOY 2024
overall_width3.240 INCHES NOMINAL IN
overall_length11.300 INCHES NOMINAL IN
aircraft_locationDOUBLER-OUTBOARD LEADING EDGE
material_thickness0.032 INCHES NOMINAL IN
aircraft_station_numberXFS208.7
aircraft_mission_design_seriesF-15C/D
material_document_and_classificationQQ-A-250/4,T81 FED SPEC SINGLE MATERIAL RESPONSE
NSN1560-01-356-3689
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available PLATE,STRUCTURAL,AIRCRAFT TITLE COMPONENT PN 68A118114-2001 MFR PLATE,STRUCTURAL,AIRCR
KEY FEATURES
•
AIRCRAFT STATION NUMBER: XFS208.7
•
MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/4,T81 FED SPEC SINGLE MATERIAL RESPONSE
•
MATERIAL THICKNESS: 0.032 INCHES NOMINAL IN
•
AIRCRAFT LOCATION: DOUBLER-OUTBOARD LEADING EDGE
•
MATERIAL: ALUMINUM ALLOY 2024
•
AIRCRAFT MISSION DESIGN SERIES: F-15C/D
TECHNICAL CHARACTERISTICS
AIRCRAFT STATION NUMBERXFS208.7
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-250/4,T81 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH11.300 INCHES NOMINAL IN
OVERALL WIDTH3.240 INCHES NOMINAL IN
MATERIAL THICKNESS0.032 INCHES NOMINAL IN
AIRCRAFT LOCATIONDOUBLER-OUTBOARD LEADING EDGE
MATERIALALUMINUM ALLOY 2024
AIRCRAFT MISSION DESIGN SERIESF-15C/D
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

No substitute or cross-reference records for this part.

LIFECYCLE
NSN statusActive· U.S. Government catalog
Acquisition advice: Insurance item — stocked against contingency demandDemilitarization required — critical (Q)
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FREQUENTLY ASKED QUESTIONS
What is 68A118114-2001?
68A118114-2001 is a PLATE,STRUCTURAL,AIRCRAFT.
What is the NSN for 68A118114-2001?
68A118114-2001 is cataloged in the U.S. Government catalog under NSN 1560-01-356-3689. This indicates validated use in U.S. government and defense supply chains.
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