68A332118-2004 — STIFFENER,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

68A332118-2004: STIFFENER,AIRCRAFT.

The STIFFENER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: TITANIUM ALLOY, overall_width: 2.380 INCHES NOMINAL IN, overall_length: 11.000 INCHES NOMINAL IN, special_features: DIM. ARE STOCK MATERIAL; U/O F-15A,B CUM1-BLK11; NEXT HIGHER ASSY 68A332001 A, aircraft_location: UPPER INBOARD SKIN,AFT CLOSURE BEAM, material_thickness: 0.045 INCHES NOMINAL IN.

This part is cataloged in the U.S. Government catalog under NSN 1560-01-474-0318, 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

68A332118-2004

NSN: 1560-01-474-0318
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)

SPECIFICATIONS

material	TITANIUM ALLOY
overall_width	2.380 INCHES NOMINAL IN
overall_length	11.000 INCHES NOMINAL IN
special_features	DIM. ARE STOCK MATERIAL; U/O F-15A,B CUM1-BLK11; NEXT HIGHER ASSY 68A332001 A
aircraft_location	UPPER INBOARD SKIN,AFT CLOSURE BEAM
material_thickness	0.045 INCHES NOMINAL IN
aircraft_mission_design_series	F-15A,B A
material_document_and_classification	MIL-T-9046,TYPE 3,COMP C,ANL MIL SPEC SINGLE MATERIAL RESPONSE
NSN	1560-01-474-0318

COMPONENT DIAGRAM

KEY FEATURES

•

MATERIAL DOCUMENT AND CLASSIFICATION: MIL-T-9046,TYPE 3,COMP C,ANL MIL SPEC SINGLE MATERIAL RESPONSE

•

MATERIAL THICKNESS: 0.045 INCHES NOMINAL IN

•

AIRCRAFT LOCATION: UPPER INBOARD SKIN,AFT CLOSURE BEAM

•

MATERIAL: TITANIUM ALLOY

•

AIRCRAFT MISSION DESIGN SERIES: F-15A,B A

TECHNICAL CHARACTERISTICS

MATERIAL DOCUMENT AND CLASSIFICATION	MIL-T-9046,TYPE 3,COMP C,ANL MIL SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH	11.000 INCHES NOMINAL IN
OVERALL WIDTH	2.380 INCHES NOMINAL IN
MATERIAL THICKNESS	0.045 INCHES NOMINAL IN
SPECIAL FEATURES	DIM. ARE STOCK MATERIAL; U/O F-15A,B CUM1-BLK11; NEXT HIGHER ASSY 68A332001 A
AIRCRAFT LOCATION	UPPER INBOARD SKIN,AFT CLOSURE BEAM
MATERIAL	TITANIUM ALLOY
AIRCRAFT MISSION DESIGN SERIES	F-15A,B A

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 68A332118-2004?

68A332118-2004 is a STIFFENER,AIRCRAFT.

What is the NSN for 68A332118-2004?

68A332118-2004 is cataloged in the U.S. Government catalog under NSN 1560-01-474-0318. This indicates validated use in U.S. government and defense supply chains.

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68A332118-2004 — STIFFENER,AIRCRAFT

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