123CS10527-514 — PLATE,STRUCTURAL,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

123CS10527-514: PLATE,STRUCTURAL,AIRCRAFT.

The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, special_features: OMIT PILOT AND FASTENER HOLES;, aircraft_location: SKIN INSTALLATION CONTROL SURFACES-INBOARD FLAP-LOWER, material_thickness: 0.032 INCHES NOMINAL IN, end_item_identification: UUT ADAPTER, material_document_and_classification: QQ-A-250/3 FED SPEC SINGLE MATERIAL RESPONSE. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-702-4630, 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

123CS10527-514

NSN: 1560-01-702-4630
FSC: 1560 — Airframe Structural Components
CAGE: 70974 — NORTHROP GRUMMAN SYSTEMS CORPORATION DIV NORTHROP GRUMMAN AERONAUTICS SYSTEMS (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 7075
special_features	OMIT PILOT AND FASTENER HOLES;
aircraft_location	SKIN INSTALLATION CONTROL SURFACES-INBOARD FLAP-LOWER
material_thickness	0.032 INCHES NOMINAL IN
end_item_identification	UUT ADAPTER
material_document_and_classification	QQ-A-250/3 FED SPEC SINGLE MATERIAL RESPONSE
part_name_assigned_by_controlling_agency	DOUBLER
NSN	1560-01-702-4630

COMPONENT DIAGRAM

KEY FEATURES

•

MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/3 FED SPEC SINGLE MATERIAL RESPONSE

•

MATERIAL THICKNESS: 0.032 INCHES NOMINAL IN

•

AIRCRAFT LOCATION: SKIN INSTALLATION CONTROL SURFACES-INBOARD FLAP-LOWER

•

MATERIAL: ALUMINUM ALLOY 7075

TECHNICAL CHARACTERISTICS

MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-250/3 FED SPEC SINGLE MATERIAL RESPONSE
MATERIAL THICKNESS	0.032 INCHES NOMINAL IN
SPECIAL FEATURES	OMIT PILOT AND FASTENER HOLES;
AIRCRAFT LOCATION	SKIN INSTALLATION CONTROL SURFACES-INBOARD FLAP-LOWER
PART NAME ASSIGNED BY CONTROLLING AGENCY	DOUBLER
END ITEM IDENTIFICATION	UUT ADAPTER
MATERIAL	ALUMINUM ALLOY 7075

SUBSTITUTES & CROSS-REFERENCES 1

123CS10527Reference document

Same NSN cross-reference

Reference document — Drawing number reference only

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 123CS10527-514?

123CS10527-514 is a PLATE,STRUCTURAL,AIRCRAFT.

What parts can replace 123CS10527-514?

There is 1 known substitute for 123CS10527-514: 123CS10527. Substitute compatibility should be verified for your specific system.

What is the NSN for 123CS10527-514?

123CS10527-514 is cataloged in the U.S. Government catalog under NSN 1560-01-702-4630. This indicates validated use in U.S. government and defense supply chains.

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123CS10527-514 — PLATE,STRUCTURAL,AIRCRAFT

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