68A112225-2006 — PANEL,STRUCTURAL,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

68A112225-2006: PANEL,STRUCTURAL,AIRCRAFT.

The PANEL,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, thickness: 0.125 INCHES NOMINAL IN, overall_width: 8.000 INCHES NOMINAL IN, overall_length: 16.100 INCHES NOMINAL IN, special_features: HEAT TREATED TO 2024-T72, aircraft_location: PANEL,AFT-WING,UPPER FAIRING. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-361-9902, 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

68A112225-2006

NSN: 1560-01-361-9902
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 2024
thickness	0.125 INCHES NOMINAL IN
overall_width	8.000 INCHES NOMINAL IN
overall_length	16.100 INCHES NOMINAL IN
special_features	HEAT TREATED TO 2024-T72
aircraft_location	PANEL,AFT-WING,UPPER FAIRING
end_item_identification	F-15E
side_for_which_designed	RIGHT SIDE
aircraft_mission_design_series	F-15E
criticality_code_justification	AGAV
material_document_and_classification	QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE
NSN	1560-01-361-9902

COMPONENT DIAGRAM

KEY FEATURES

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE

•

AIRCRAFT LOCATION: PANEL,AFT-WING,UPPER FAIRING

•

MATERIAL: ALUMINUM ALLOY 2024

TECHNICAL CHARACTERISTICS

CRITICALITY CODE JUSTIFICATION	AGAV
MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH	16.100 INCHES NOMINAL IN
OVERALL WIDTH	8.000 INCHES NOMINAL IN
SPECIAL FEATURES	HEAT TREATED TO 2024-T72
AIRCRAFT LOCATION	PANEL,AFT-WING,UPPER FAIRING
END ITEM IDENTIFICATION	F-15E
MATERIAL	ALUMINUM ALLOY 2024
SIDE FOR WHICH DESIGNED	RIGHT SIDE
AIRCRAFT MISSION DESIGN SERIES	F-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 68A112225-2006?

68A112225-2006 is a PANEL,STRUCTURAL,AIRCRAFT.

What is the NSN for 68A112225-2006?

68A112225-2006 is cataloged in the U.S. Government catalog under NSN 1560-01-361-9902. This indicates validated use in U.S. government and defense supply chains.

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68A112225-2006 — PANEL,STRUCTURAL,AIRCRAFT

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