75A321139-2009 — SUPPORT,STRUCTURAL COMPONENT,AIR

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

75A321139-2009: SUPPORT,STRUCTURAL COMPONENT,AIR.

SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 3.000 INCHES NOMINAL IN, overall_length: 6.750 INCHES NOMINAL IN, aircraft_location: STRAKE ASSEMBLY, surface_treatment: ANODIZE, material_thickness: 1.500 INCHES NOMINAL IN. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-371-0359, 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

75A321139-2009

NSN: 1560-01-371-0359
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 7075
overall_width	3.000 INCHES NOMINAL IN
overall_length	6.750 INCHES NOMINAL IN
aircraft_location	STRAKE ASSEMBLY
surface_treatment	ANODIZE
material_thickness	1.500 INCHES NOMINAL IN
aircraft_station_number	FS285.500
end_item_identification	AIRCRAFT MODEL AV-8B
side_for_which_designed	LEFT SIDE
aircraft_mission_design_series	AV-8B
material_document_and_classification	MMS159 PLATE CONDITION T7351 MFR REF SINGLE MATERIAL RESPONSE
surface_treatment_document_and_classification	PS13201; TYPE 2,CLASS 1 MFR REF SINGLE TREATMENT RESPONSE
NSN	1560-01-371-0359

COMPONENT DIAGRAM

KEY FEATURES

•

AIRCRAFT STATION NUMBER: FS285.500

•

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION: PS13201; TYPE 2,CLASS 1 MFR REF SINGLE TREATMENT RESPONSE

•

MATERIAL DOCUMENT AND CLASSIFICATION: MMS159 PLATE CONDITION T7351 MFR REF SINGLE MATERIAL RESPONSE

•

MATERIAL THICKNESS: 1.500 INCHES NOMINAL IN

•

SURFACE TREATMENT: ANODIZE

•

AIRCRAFT LOCATION: STRAKE ASSEMBLY

TECHNICAL CHARACTERISTICS

AIRCRAFT STATION NUMBER	FS285.500
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION	PS13201; TYPE 2,CLASS 1 MFR REF SINGLE TREATMENT RESPONSE
MATERIAL DOCUMENT AND CLASSIFICATION	MMS159 PLATE CONDITION T7351 MFR REF SINGLE MATERIAL RESPONSE
OVERALL LENGTH	6.750 INCHES NOMINAL IN
OVERALL WIDTH	3.000 INCHES NOMINAL IN
MATERIAL THICKNESS	1.500 INCHES NOMINAL IN
SURFACE TREATMENT	ANODIZE
AIRCRAFT LOCATION	STRAKE ASSEMBLY
END ITEM IDENTIFICATION	AIRCRAFT MODEL AV-8B
MATERIAL	ALUMINUM ALLOY 7075

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

Demilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 75A321139-2009?

75A321139-2009 is a SUPPORT,STRUCTURAL COMPONENT,AIR.

What is the NSN for 75A321139-2009?

75A321139-2009 is cataloged in the U.S. Government catalog under NSN 1560-01-371-0359. This indicates validated use in U.S. government and defense supply chains.

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75A321139-2009 — SUPPORT,STRUCTURAL COMPONENT,AIR

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