68A350821-2009 — SUPPORT,STRUCTURAL COMPONENT,AIR

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

68A350821-2009: SUPPORT,STRUCTURAL COMPONENT,AIR.

SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include height: 4.000 INCHES NOMINAL IN, material: ALUMINUM ALLOY 7075, overall_width: 7.000 INCHES NOMINAL IN, overall_length: 7.000 INCHES NOMINAL IN, special_features: P/N 68A350821-2010 IS THE OPPOSITE CONFIGURATION;NEXT ASSEMBLY 68A350011, aircraft_location: FITTING-CANOPY FORWARD CORNER. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-445-1437, 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

68A350821-2009

NSN: 1560-01-445-1437
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)

SPECIFICATIONS

height	4.000 INCHES NOMINAL IN
material	ALUMINUM ALLOY 7075
overall_width	7.000 INCHES NOMINAL IN
overall_length	7.000 INCHES NOMINAL IN
special_features	P/N 68A350821-2010 IS THE OPPOSITE CONFIGURATION;NEXT ASSEMBLY 68A350011
aircraft_location	FITTING-CANOPY FORWARD CORNER
surface_treatment	ANODIZE
aircraft_mission_design_series	F-15I
material_document_and_classification	MMS-159,T7351 MFR REF SINGLE MATERIAL RESPONSE
surface_treatment_document_and_classification	PS13201 TYPE II CLASS 1 MFR REF SINGLE TREATMENT RESPONSE
NSN	1560-01-445-1437

COMPONENT DIAGRAM

KEY FEATURES

•

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

•

MATERIAL DOCUMENT AND CLASSIFICATION: MMS-159,T7351 MFR REF SINGLE MATERIAL RESPONSE

•

HEIGHT: 4.000 INCHES NOMINAL IN

•

SURFACE TREATMENT: ANODIZE

•

AIRCRAFT LOCATION: FITTING-CANOPY FORWARD CORNER

TECHNICAL CHARACTERISTICS

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION	PS13201 TYPE II CLASS 1 MFR REF SINGLE TREATMENT RESPONSE
MATERIAL DOCUMENT AND CLASSIFICATION	MMS-159,T7351 MFR REF SINGLE MATERIAL RESPONSE
OVERALL LENGTH	7.000 INCHES NOMINAL IN
OVERALL WIDTH	7.000 INCHES NOMINAL IN
HEIGHT	4.000 INCHES NOMINAL IN
SPECIAL FEATURES	P/N 68A350821-2010 IS THE OPPOSITE CONFIGURATION;NEXT ASSEMBLY 68A350011
SURFACE TREATMENT	ANODIZE
AIRCRAFT LOCATION	FITTING-CANOPY FORWARD CORNER
MATERIAL	ALUMINUM ALLOY 7075
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

Demilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 68A350821-2009?

68A350821-2009 is a SUPPORT,STRUCTURAL COMPONENT,AIR.

What is the NSN for 68A350821-2009?

68A350821-2009 is cataloged in the U.S. Government catalog under NSN 1560-01-445-1437. This indicates validated use in U.S. government and defense supply chains.

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68A350821-2009 — SUPPORT,STRUCTURAL COMPONENT,AIR

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