68R096018-2069 — BRACKET,STRUCTURAL COMPONENT,AIR

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

68R096018-2069: BRACKET,STRUCTURAL COMPONENT,AIR.

BRACKET,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 6.540 INCHES NOMINAL IN, overall_length: 7.700 INCHES NOMINAL IN, special_features: MATERIAL STOCK P/N 68A731053-1001, aircraft_location: CENTERLINE PYLON-REWORK, surface_treatment: ANODIZE. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-445-0671, 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

68R096018-2069

NSN: 1560-01-445-0671
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 2024
overall_width	6.540 INCHES NOMINAL IN
overall_length	7.700 INCHES NOMINAL IN
special_features	MATERIAL STOCK P/N 68A731053-1001
aircraft_location	CENTERLINE PYLON-REWORK
surface_treatment	ANODIZE
material_thickness	0.063 INCHES NOMINAL IN
aircraft_mission_design_series	F-15I
material_document_and_classification	QQ-A-250/4,T62 FED SPEC SINGLE MATERIAL RESPONSE
surface_treatment_document_and_classification	PS13201 TYPE II CLASS 1 MFR REF SINGLE TREATMENT RESPONSE
NSN	1560-01-445-0671

COMPONENT DIAGRAM

KEY FEATURES

•

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION: PS13201 TYPE II CLASS 1 MFR REF SINGLE TREATMENT RESPONSE

•

MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/4,T62 FED SPEC SINGLE MATERIAL RESPONSE

•

MATERIAL THICKNESS: 0.063 INCHES NOMINAL IN

•

SURFACE TREATMENT: ANODIZE

•

AIRCRAFT LOCATION: CENTERLINE PYLON-REWORK

TECHNICAL CHARACTERISTICS

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION	PS13201 TYPE II CLASS 1 MFR REF SINGLE TREATMENT RESPONSE
MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-250/4,T62 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH	7.700 INCHES NOMINAL IN
OVERALL WIDTH	6.540 INCHES NOMINAL IN
MATERIAL THICKNESS	0.063 INCHES NOMINAL IN
SPECIAL FEATURES	MATERIAL STOCK P/N 68A731053-1001
SURFACE TREATMENT	ANODIZE
AIRCRAFT LOCATION	CENTERLINE PYLON-REWORK
MATERIAL	ALUMINUM ALLOY 2024
AIRCRAFT MISSION DESIGN SERIES	F-15I

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 68R096018-2069?

68R096018-2069 is a BRACKET,STRUCTURAL COMPONENT,AIR.

What is the NSN for 68R096018-2069?

68R096018-2069 is cataloged in the U.S. Government catalog under NSN 1560-01-445-0671. This indicates validated use in U.S. government and defense supply chains.

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68R096018-2069 — BRACKET,STRUCTURAL COMPONENT,AIR

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