68A332111-2011 — STIFFENER,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

68A332111-2011: STIFFENER,AIRCRAFT.

The STIFFENER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 2.600 INCHES NOMINAL IN, overall_length: 9.320 INCHES NOMINAL IN, special_features: DIM. STOCK MATERIAL; NEXT HIGHER ASSY 68A332001 U/O F-15AB CUM1-BLK11, aircraft_location: OUTBOARD AFT CLOSURE BEAM, material_thickness: 0.040 INCHES NOMINAL IN.

This part is cataloged in the U.S. Government catalog under NSN 1560-01-467-3145, 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

68A332111-2011

NSN: 1560-01-467-3145
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 2024
overall_width	2.600 INCHES NOMINAL IN
overall_length	9.320 INCHES NOMINAL IN
special_features	DIM. STOCK MATERIAL; NEXT HIGHER ASSY 68A332001 U/O F-15AB CUM1-BLK11
aircraft_location	OUTBOARD AFT CLOSURE BEAM
material_thickness	0.040 INCHES NOMINAL IN
aircraft_station_number	FS844.22
side_for_which_designed	LEFT SIDE
aircraft_mission_design_series	F-15
material_document_and_classification	QQ-A-250/5,T62 FED SPEC SINGLE MATERIAL RESPONSE
NSN	1560-01-467-3145

COMPONENT DIAGRAM

KEY FEATURES

•

AIRCRAFT STATION NUMBER: FS844.22

•

MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/5,T62 FED SPEC SINGLE MATERIAL RESPONSE

•

MATERIAL THICKNESS: 0.040 INCHES NOMINAL IN

•

AIRCRAFT LOCATION: OUTBOARD AFT CLOSURE BEAM

•

MATERIAL: ALUMINUM ALLOY 2024

TECHNICAL CHARACTERISTICS

AIRCRAFT STATION NUMBER	FS844.22
MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-250/5,T62 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH	9.320 INCHES NOMINAL IN
OVERALL WIDTH	2.600 INCHES NOMINAL IN
MATERIAL THICKNESS	0.040 INCHES NOMINAL IN
SPECIAL FEATURES	DIM. STOCK MATERIAL; NEXT HIGHER ASSY 68A332001 U/O F-15AB CUM1-BLK11
AIRCRAFT LOCATION	OUTBOARD AFT CLOSURE BEAM
MATERIAL	ALUMINUM ALLOY 2024
SIDE FOR WHICH DESIGNED	LEFT SIDE
AIRCRAFT MISSION DESIGN SERIES	F-15

OTHER ITEMS IN FSC 1560 — Airframe Structural Components

Items in the same Federal Supply class. No interchangeability or substitution relationship is implied.

1560-00-003-1977 1560-00-003-3257 1560-00-004-4244 1560-00-005-7280 1560-00-006-0576 1560-00-006-6538 1560-00-007-9578 1560-00-009-4192

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 68A332111-2011?

68A332111-2011 is a STIFFENER,AIRCRAFT.

What is the NSN for 68A332111-2011?

68A332111-2011 is cataloged in the U.S. Government catalog under NSN 1560-01-467-3145. This indicates validated use in U.S. government and defense supply chains.

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