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68A111228-2003 — PLATE,STRUCTURAL,AIRCRAFT

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

68A111228-2003: PLATE,STRUCTURAL,AIRCRAFT.

The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_length: 36.000 INCHES NOMINAL IN, aircraft_location: SEAL STRIP-LEADING EDGE CLOSURE TO FUSELAGE MOLDLINE, material_thickness: 0.160 INCHES NOMINAL IN, aircraft_mission_design_series: F-15E, material_document_and_classification: QQ-A-250/4,T72 FED SPEC SINGLE MATERIAL RESPONSE. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-361-3441, 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
68A111228-2003
NSN: 1560-01-361-3441
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)
SPECIFICATIONS
materialALUMINUM ALLOY 2024
overall_length36.000 INCHES NOMINAL IN
aircraft_locationSEAL STRIP-LEADING EDGE CLOSURE TO FUSELAGE MOLDLINE
material_thickness0.160 INCHES NOMINAL IN
aircraft_mission_design_seriesF-15E
material_document_and_classificationQQ-A-250/4,T72 FED SPEC SINGLE MATERIAL RESPONSE
NSN1560-01-361-3441
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available PLATE,STRUCTURAL,AIRCRAFT TITLE COMPONENT PN 68A111228-2003 MFR PLATE,STRUCTURAL,AIRCR
KEY FEATURES
•
MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/4,T72 FED SPEC SINGLE MATERIAL RESPONSE
•
MATERIAL THICKNESS: 0.160 INCHES NOMINAL IN
•
AIRCRAFT LOCATION: SEAL STRIP-LEADING EDGE CLOSURE TO FUSELAGE MOLDLINE
•
MATERIAL: ALUMINUM ALLOY 2024
•
AIRCRAFT MISSION DESIGN SERIES: F-15E
TECHNICAL CHARACTERISTICS
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-250/4,T72 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH36.000 INCHES NOMINAL IN
MATERIAL THICKNESS0.160 INCHES NOMINAL IN
AIRCRAFT LOCATIONSEAL STRIP-LEADING EDGE CLOSURE TO FUSELAGE MOLDLINE
MATERIALALUMINUM ALLOY 2024
AIRCRAFT MISSION DESIGN SERIESF-15E
OTHER ITEMS IN FSC 1560 — Airframe Structural Components
Items in the same Federal Supply class. No interchangeability or substitution relationship is implied.
1560-00-003-1977 1560-00-003-3257 1560-00-004-4244 1560-00-005-7280 1560-00-006-0576 1560-00-006-6538 1560-00-007-9578 1560-00-009-4192
SUBSTITUTES & CROSS-REFERENCES

No substitute or cross-reference records for this part.

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 68A111228-2003?
68A111228-2003 is a PLATE,STRUCTURAL,AIRCRAFT.
What is the NSN for 68A111228-2003?
68A111228-2003 is cataloged in the U.S. Government catalog under NSN 1560-01-361-3441. This indicates validated use in U.S. government and defense supply chains.
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