68A332195-2012 — STIFFENER,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

68A332195-2012: STIFFENER,AIRCRAFT.

The STIFFENER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 1.160 INCHES NOMINAL IN, overall_length: 5.150 INCHES NOMINAL IN, special_features: DIM. STOCK MATERIAL; NEXT HIGHER ASSY 68A332201 U/O F-15A,B BLK12&UP, F-15C CUM1-287, F-15D CUM1-46 A, aircraft_location: INBOARD,EMPENAGE SUPPORT BEAM CLOSURE, material_thickness: 0.050 INCHES NOMINAL IN.

This part is cataloged in the U.S. Government catalog under NSN 1560-01-467-3142, 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

68A332195-2012

NSN: 1560-01-467-3142
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 2024
overall_width	1.160 INCHES NOMINAL IN
overall_length	5.150 INCHES NOMINAL IN
special_features	DIM. STOCK MATERIAL; NEXT HIGHER ASSY 68A332201 U/O F-15A,B BLK12&UP, F-15C CUM1-287, F-15D CUM1-46 A
aircraft_location	INBOARD,EMPENAGE SUPPORT BEAM CLOSURE
material_thickness	0.050 INCHES NOMINAL IN
aircraft_station_number	FS844.22
side_for_which_designed	RIGHT SIDE
aircraft_mission_design_series	F-15A,B,C,D A
material_document_and_classification	QQ-A-250/5,T62 FED SPEC SINGLE MATERIAL RESPONSE
NSN	1560-01-467-3142

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: 0.050 INCHES NOMINAL IN

•

AIRCRAFT LOCATION: INBOARD,EMPENAGE SUPPORT BEAM CLOSURE

•

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	5.150 INCHES NOMINAL IN
OVERALL WIDTH	1.160 INCHES NOMINAL IN
MATERIAL THICKNESS	0.050 INCHES NOMINAL IN
SPECIAL FEATURES	DIM. STOCK MATERIAL; NEXT HIGHER ASSY 68A332201 U/O F-15A,B BLK12&UP, F-15C CUM1-287, F-15D CUM1-46 A
AIRCRAFT LOCATION	INBOARD,EMPENAGE SUPPORT BEAM CLOSURE
MATERIAL	ALUMINUM ALLOY 2024
SIDE FOR WHICH DESIGNED	RIGHT SIDE
AIRCRAFT MISSION DESIGN SERIES	F-15A,B,C,D A

OTHER ITEMS IN FSC 1560 — Airframe Structural Components

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

1560-00-003-1977 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 68A332195-2012?

68A332195-2012 is a STIFFENER,AIRCRAFT.

What is the NSN for 68A332195-2012?

68A332195-2012 is cataloged in the U.S. Government catalog under NSN 1560-01-467-3142. This indicates validated use in U.S. government and defense supply chains.

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