160D511132-12 — PLATE,STRUCTURAL,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

160D511132-12: PLATE,STRUCTURAL,AIRCRAFT.

The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 5.000 INCHES NOMINAL IN, overall_length: 5.000 INCHES NOMINAL IN, special_features: ALCD SH-0; DIM. ARE STOCKSIZE; NHA 160D511108 AND 09; -11 OPPOSITE, aircraft_location: AFT FAIRING, VENTRAL FIN, LASTE, material_thickness: 0.063 INCHES NOMINAL IN.

This part is cataloged in the U.S. Government catalog under NSN 1560-01-565-8737, 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

160D511132-12

NSN: 1560-01-565-8737
FSC: 1560 — Airframe Structural Components
CAGE: 79RG9 — NORTHROP GRUMMAN SYSTEMS CORPORATION (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 2024
overall_width	5.000 INCHES NOMINAL IN
overall_length	5.000 INCHES NOMINAL IN
special_features	ALCD SH-0; DIM. ARE STOCKSIZE; NHA 160D511108 AND 09; -11 OPPOSITE
aircraft_location	AFT FAIRING, VENTRAL FIN, LASTE
material_thickness	0.063 INCHES NOMINAL IN
end_item_identification	A-10 ACFT
aircraft_mission_design_series	A-10 ACFT
material_document_and_classification	QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE
part_name_assigned_by_controlling_agency	PLATE, STRUCTURAL
NSN	1560-01-565-8737

COMPONENT DIAGRAM

KEY FEATURES

•

MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE

•

MATERIAL THICKNESS: 0.063 INCHES NOMINAL IN

•

AIRCRAFT LOCATION: AFT FAIRING, VENTRAL FIN, LASTE

TECHNICAL CHARACTERISTICS

MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH	5.000 INCHES NOMINAL IN
OVERALL WIDTH	5.000 INCHES NOMINAL IN
MATERIAL THICKNESS	0.063 INCHES NOMINAL IN
SPECIAL FEATURES	ALCD SH-0; DIM. ARE STOCKSIZE; NHA 160D511108 AND 09; -11 OPPOSITE
AIRCRAFT LOCATION	AFT FAIRING, VENTRAL FIN, LASTE
PART NAME ASSIGNED BY CONTROLLING AGENCY	PLATE, STRUCTURAL
END ITEM IDENTIFICATION	A-10 ACFT
MATERIAL	ALUMINUM ALLOY 2024
AIRCRAFT MISSION DESIGN SERIES	A-10 ACFT

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 — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 160D511132-12?

160D511132-12 is a PLATE,STRUCTURAL,AIRCRAFT.

What is the NSN for 160D511132-12?

160D511132-12 is cataloged in the U.S. Government catalog under NSN 1560-01-565-8737. This indicates validated use in U.S. government and defense supply chains.

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160D511132-12 — PLATE,STRUCTURAL,AIRCRAFT

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