68A230108-2003 — SUPPORT,STRUCTURAL COMPONENT,AIR

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

68A230108-2003: SUPPORT,STRUCTURAL COMPONENT,AIR.

SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 2.031 INCHES NOMINAL IN, overall_length: 3.250 INCHES NOMINAL IN, special_features: NEXT HIGHER ASSEMBLY 68A230091 U/O F-15A CUM 223 AND UP;F-15B CUM 36 AND UP;F-15C CUM 1 AND UP;F-15D CUM 1 AND UP A, aircraft_location: VERTICAL STABILIZER, material_thickness: 0.250 INCHES NOMINAL IN. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-482-0002, 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

68A230108-2003

NSN: 1560-01-482-0002
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 2024
overall_width	2.031 INCHES NOMINAL IN
overall_length	3.250 INCHES NOMINAL IN
special_features	NEXT HIGHER ASSEMBLY 68A230091 U/O F-15A CUM 223 AND UP;F-15B CUM 36 AND UP;F-15C CUM 1 AND UP;F-15D CUM 1 AND UP A
aircraft_location	VERTICAL STABILIZER
material_thickness	0.250 INCHES NOMINAL IN
aircraft_mission_design_series	F-15A,B,C,D A
material_document_and_classification	WW-T-700/3 COND T3 FED SPEC 1ST MATERIAL RESPONSE
NSN	1560-01-482-0002

COMPONENT DIAGRAM

KEY FEATURES

•

MATERIAL DOCUMENT AND CLASSIFICATION: WW-T-700/3 COND T3 FED SPEC 1ST MATERIAL RESPONSE

•

MATERIAL THICKNESS: 0.250 INCHES NOMINAL IN

•

AIRCRAFT LOCATION: VERTICAL STABILIZER

•

MATERIAL: ALUMINUM ALLOY 2024

•

AIRCRAFT MISSION DESIGN SERIES: F-15A,B,C,D A

TECHNICAL CHARACTERISTICS

MATERIAL DOCUMENT AND CLASSIFICATION	WW-T-700/3 COND T3 FED SPEC 1ST MATERIAL RESPONSE
OVERALL LENGTH	3.250 INCHES NOMINAL IN
OVERALL WIDTH	2.031 INCHES NOMINAL IN
MATERIAL THICKNESS	0.250 INCHES NOMINAL IN
SPECIAL FEATURES	NEXT HIGHER ASSEMBLY 68A230091 U/O F-15A CUM 223 AND UP;F-15B CUM 36 AND UP;F-15C CUM 1 AND UP;F-15D CUM 1 AND UP A
AIRCRAFT LOCATION	VERTICAL STABILIZER
MATERIAL	ALUMINUM ALLOY 2024
AIRCRAFT MISSION DESIGN SERIES	F-15A,B,C,D A

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: Normally procured from the manufacturer (OEM)Demilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 68A230108-2003?

68A230108-2003 is a SUPPORT,STRUCTURAL COMPONENT,AIR.

What is the NSN for 68A230108-2003?

68A230108-2003 is cataloged in the U.S. Government catalog under NSN 1560-01-482-0002. This indicates validated use in U.S. government and defense supply chains.

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68A230108-2003 — SUPPORT,STRUCTURAL COMPONENT,AIR

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