123CS11231 — BRACKET,STRUCTURAL COMPONENT,AIR

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

123CS11231: BRACKET,STRUCTURAL COMPONENT,AIR.

BRACKET,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 3.000 INCHES MINIMUM IN, overall_length: 3.000 INCHES NOMINAL IN, special_features: NEXT HIGHER ASSEMBLY 123CS11215, aircraft_location: RUDDER REAR BEAM, surface_treatment: ANODIZE AND PRIMER EPOXY-POLYAMIDE. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-530-9125, 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

123CS11231

NSN: 1560-01-530-9125
NIINs: 015309125, 017008730, 017008731, 017008849
FSC: 1560 — Airframe Structural Components
CAGE: 26512 — NORTHROP GRUMMAN SYSTEMS CORPORATION (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 7075
overall_width	3.000 INCHES MINIMUM IN
overall_length	3.000 INCHES NOMINAL IN
special_features	NEXT HIGHER ASSEMBLY 123CS11215
aircraft_location	RUDDER REAR BEAM
surface_treatment	ANODIZE AND PRIMER EPOXY-POLYAMIDE
material_thickness	0.020 INCHES NOMINAL IN
end_item_identification	E-2C; RUDDER REAR BEAM
aircraft_mission_design_series	E-2C
material_document_and_classification	QQ-A-250/13 ASSN STD SINGLE MATERIAL RESPONSE
part_name_assigned_by_controlling_agency	INAVY: BRACKET ASSEMBLY
surface_treatment_document_and_classification	MIL-A-8625TY2CL1 MIL SPEC 1ST TREATMENT RESPONSE AND MIL-P-23377TY1 MIL SPEC 2ND TREATMENT RESPONSE
NSN	1560-01-530-9125

COMPONENT DIAGRAM

KEY FEATURES

•

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION: MIL-A-8625TY2CL1 MIL SPEC 1ST TREATMENT RESPONSE AND MIL-P-23377TY1 MIL SPEC 2ND TREATMENT RESPONSE

•

MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/13 ASSN STD SINGLE MATERIAL RESPONSE

•

MATERIAL THICKNESS: 0.020 INCHES NOMINAL IN

•

SURFACE TREATMENT: ANODIZE AND PRIMER EPOXY-POLYAMIDE

•

AIRCRAFT LOCATION: RUDDER REAR BEAM

TECHNICAL CHARACTERISTICS

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION	MIL-A-8625TY2CL1 MIL SPEC 1ST TREATMENT RESPONSE AND MIL-P-23377TY1 MIL SPEC 2ND TREATMENT RESPONSE
MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-250/13 ASSN STD SINGLE MATERIAL RESPONSE
OVERALL LENGTH	3.000 INCHES NOMINAL IN
OVERALL WIDTH	3.000 INCHES MINIMUM IN
MATERIAL THICKNESS	0.020 INCHES NOMINAL IN
SPECIAL FEATURES	NEXT HIGHER ASSEMBLY 123CS11215
SURFACE TREATMENT	ANODIZE AND PRIMER EPOXY-POLYAMIDE
AIRCRAFT LOCATION	RUDDER REAR BEAM
PART NAME ASSIGNED BY CONTROLLING AGENCY	INAVY: BRACKET ASSEMBLY
END ITEM IDENTIFICATION	E-2C; RUDDER REAR BEAM

SUBSTITUTES & CROSS-REFERENCES 1

123CS11231-18Reference document

Same NSN cross-reference

Reference document — Secondary reference

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Insurance item — stocked against contingency demandDemilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 123CS11231?

123CS11231 is a BRACKET,STRUCTURAL COMPONENT,AIR.

What parts can replace 123CS11231?

There is 1 known substitute for 123CS11231: 123CS11231-18. Substitute compatibility should be verified for your specific system.

What is the NSN for 123CS11231?

123CS11231 is cataloged in the U.S. Government catalog under NSN 1560-01-530-9125. This indicates validated use in U.S. government and defense supply chains.

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