DAA3234D089-001 — PLATE,STRUCTURAL,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

DAA3234D089-001: PLATE,STRUCTURAL,AIRCRAFT.

The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 1.130 INCHES NOMINAL IN, overall_length: 1.250 INCHES NOMINAL IN, aircraft_location: NSS VEHICLE WINDOW, surface_treatment: ANODIZE AND PAINT LUSTERLESS AND PRIMER, material_thickness: 0.250 INCHES NOMINAL IN. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-359-7352, 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

DAA3234D089-001

NSN: 1560-01-359-7352
FSC: 1560 — Airframe Structural Components
CAGE: 1W025 — NORTHROP GRUMMAN SYSTEMS CORP DBA NORTHROP GRUMMAN COMPUTING SYSTEMS (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 7075
overall_width	1.130 INCHES NOMINAL IN
overall_length	1.250 INCHES NOMINAL IN
aircraft_location	NSS VEHICLE WINDOW
surface_treatment	ANODIZE AND PAINT LUSTERLESS AND PRIMER
material_thickness	0.250 INCHES NOMINAL IN
aircraft_mission_design_series	B-2
material_document_and_classification	QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE
surface_treatment_document_and_classification	SF-105 MFR REF 1ST TREATMENT RESPONSE AND SF-303 MFR REF 2ND TREATMENT RESPONSE AND SF-202 MFR REF 3RD TREATMENT RESPONSE
NSN	1560-01-359-7352

COMPONENT DIAGRAM

KEY FEATURES

•

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION: SF-105 MFR REF 1ST TREATMENT RESPONSE AND SF-303 MFR REF 2ND TREATMENT RESPONSE AND SF-202 MFR REF 3RD TREATMENT RESPONSE

•

MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE

•

MATERIAL THICKNESS: 0.250 INCHES NOMINAL IN

•

SURFACE TREATMENT: ANODIZE AND PAINT LUSTERLESS AND PRIMER

•

AIRCRAFT LOCATION: NSS VEHICLE WINDOW

•

MATERIAL: ALUMINUM ALLOY 7075

TECHNICAL CHARACTERISTICS

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION	SF-105 MFR REF 1ST TREATMENT RESPONSE AND SF-303 MFR REF 2ND TREATMENT RESPONSE AND SF-202 MFR REF 3RD TREATMENT RESPONSE
MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH	1.250 INCHES NOMINAL IN
OVERALL WIDTH	1.130 INCHES NOMINAL IN
MATERIAL THICKNESS	0.250 INCHES NOMINAL IN
SURFACE TREATMENT	ANODIZE AND PAINT LUSTERLESS AND PRIMER
AIRCRAFT LOCATION	NSS VEHICLE WINDOW
MATERIAL	ALUMINUM ALLOY 7075
AIRCRAFT MISSION DESIGN SERIES	B-2

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 — mutilation

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FREQUENTLY ASKED QUESTIONS

What is DAA3234D089-001?

DAA3234D089-001 is a PLATE,STRUCTURAL,AIRCRAFT.

What is the NSN for DAA3234D089-001?

DAA3234D089-001 is cataloged in the U.S. Government catalog under NSN 1560-01-359-7352. This indicates validated use in U.S. government and defense supply chains.

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DAA3234D089-001 — PLATE,STRUCTURAL,AIRCRAFT

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