68A580618-1007 — SUPPORT,STRUCTURAL COMPONENT,AIR

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

68A580618-1007: SUPPORT,STRUCTURAL COMPONENT,AIR.

SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include height: 0.800 INCHES NOMINAL IN, material: ALUMINUM ALLOY 2024, overall_length: 7.400 INCHES NOMINAL IN, special_features: U/O F-15C 254 UP, F-15 42UP, F-1DJ 11UP;NEXT HIGHER ASSEMBLY 68A581570, aircraft_location: FUEL TRANSFER PUMP, surface_treatment: ANODIZE. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-458-4189, 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

68A580618-1007

NSN: 1560-01-458-4189
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)

SPECIFICATIONS

height	0.800 INCHES NOMINAL IN
material	ALUMINUM ALLOY 2024
hole_quantity	8
overall_length	7.400 INCHES NOMINAL IN
special_features	U/O F-15C 254 UP, F-15 42UP, F-1DJ 11UP;NEXT HIGHER ASSEMBLY 68A581570
aircraft_location	FUEL TRANSFER PUMP
surface_treatment	ANODIZE
aircraft_mission_design_series	F-15
material_document_and_classification	QQ-A-250/4,T851 FED SPEC SINGLE MATERIAL RESPONSE
surface_treatment_document_and_classification	PS13201,TYPE II,CLASS 1 MFR REF SINGLE TREATMENT RESPONSE
NSN	1560-01-458-4189

COMPONENT DIAGRAM

KEY FEATURES

•

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION: PS13201,TYPE II,CLASS 1 MFR REF SINGLE TREATMENT RESPONSE

•

MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/4,T851 FED SPEC SINGLE MATERIAL RESPONSE

•

HEIGHT: 0.800 INCHES NOMINAL IN

•

SURFACE TREATMENT: ANODIZE

•

AIRCRAFT LOCATION: FUEL TRANSFER PUMP

•

MATERIAL: ALUMINUM ALLOY 2024

TECHNICAL CHARACTERISTICS

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION	PS13201,TYPE II,CLASS 1 MFR REF SINGLE TREATMENT RESPONSE
MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-250/4,T851 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH	7.400 INCHES NOMINAL IN
HEIGHT	0.800 INCHES NOMINAL IN
SPECIAL FEATURES	U/O F-15C 254 UP, F-15 42UP, F-1DJ 11UP;NEXT HIGHER ASSEMBLY 68A581570
SURFACE TREATMENT	ANODIZE
AIRCRAFT LOCATION	FUEL TRANSFER PUMP
MATERIAL	ALUMINUM ALLOY 2024
HOLE QUANTITY	8
AIRCRAFT MISSION DESIGN SERIES	F-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

No substitute or cross-reference records for this part.

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 68A580618-1007?

68A580618-1007 is a SUPPORT,STRUCTURAL COMPONENT,AIR.

What is the NSN for 68A580618-1007?

68A580618-1007 is cataloged in the U.S. Government catalog under NSN 1560-01-458-4189. This indicates validated use in U.S. government and defense supply chains.

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68A580618-1007 — SUPPORT,STRUCTURAL COMPONENT,AIR

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