75A732760-2003 — FORMER,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

75A732760-2003: FORMER,AIRCRAFT.

The FORMER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 18.000 INCHES NOMINAL IN, overall_length: 19.000 INCHES NOMINAL IN, aircraft_location: 25MM GUN PAK MM, surface_treatment: ANODIZE, material_thickness: 1.750 INCHES NOMINAL IN. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-372-7937, 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

75A732760-2003

NSN: 1560-01-372-7937
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 7075
overall_width	18.000 INCHES NOMINAL IN
overall_length	19.000 INCHES NOMINAL IN
aircraft_location	25MM GUN PAK MM
surface_treatment	ANODIZE
material_thickness	1.750 INCHES NOMINAL IN
aircraft_station_number	FS327.44
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 TY 2 CLASS 1 MFR REF SINGLE TREATMENT RESPONSE
NSN	1560-01-372-7937

COMPONENT DIAGRAM

KEY FEATURES

•

AIRCRAFT STATION NUMBER: FS327.44

•

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION: PS13201 TY 2 CLASS 1 MFR REF SINGLE TREATMENT RESPONSE

•

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

•

MATERIAL THICKNESS: 1.750 INCHES NOMINAL IN

•

SURFACE TREATMENT: ANODIZE

•

AIRCRAFT LOCATION: 25MM GUN PAK MM

TECHNICAL CHARACTERISTICS

AIRCRAFT STATION NUMBER	FS327.44
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION	PS13201 TY 2 CLASS 1 MFR REF SINGLE TREATMENT RESPONSE
MATERIAL DOCUMENT AND CLASSIFICATION	MMS159 PLATE CONDITION T7351 MFR REF SINGLE MATERIAL RESPONSE
OVERALL LENGTH	19.000 INCHES NOMINAL IN
OVERALL WIDTH	18.000 INCHES NOMINAL IN
MATERIAL THICKNESS	1.750 INCHES NOMINAL IN
SURFACE TREATMENT	ANODIZE
AIRCRAFT LOCATION	25MM GUN PAK MM
MATERIAL	ALUMINUM ALLOY 7075
AIRCRAFT MISSION DESIGN SERIES	AV-8B

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 75A732760-2003?

75A732760-2003 is a FORMER,AIRCRAFT.

What is the NSN for 75A732760-2003?

75A732760-2003 is cataloged in the U.S. Government catalog under NSN 1560-01-372-7937. This indicates validated use in U.S. government and defense supply chains.

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