68A332197-2003 — STIFFENER,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

68A332197-2003: STIFFENER,AIRCRAFT.

The STIFFENER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 1.900 INCHES NOMINAL IN, overall_length: 11.200 INCHES NOMINAL IN, aircraft_location: STIFFENERS-LOWER EMPENAGE SUPPORTBEAM CLOSURE, material_thickness: 0.050 INCHES NOMINAL IN, aircraft_station_number: 822.640. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-467-4199, 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

68A332197-2003

NSN: 1560-01-467-4199
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 2024
overall_width	1.900 INCHES NOMINAL IN
overall_length	11.200 INCHES NOMINAL IN
special_features	NEXT HIGER ASSY,68A332201,U/O F-15A BLK 12 AND UP,F-15B BLK 12 AND UP,F-15C CUM 1 AND UP,F-15D CUM 1 AND UP,F-15E CUM 1-2,68A33200,U/O F-15E CUM 3-209,DIM.STOCK MATERIAL A
aircraft_location	STIFFENERS-LOWER EMPENAGE SUPPORTBEAM CLOSURE
material_thickness	0.050 INCHES NOMINAL IN
aircraft_station_number	822.640
side_for_which_designed	LEFT SIDE
aircraft_mission_design_series	F-15A,B,C,D,E A
material_document_and_classification	QQ-A-250/5,COND 0,T62 FED SPEC 1ST MATERIAL RESPONSE
NSN	1560-01-467-4199

COMPONENT DIAGRAM

KEY FEATURES

•

AIRCRAFT STATION NUMBER: 822.640

•

MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/5,COND 0,T62 FED SPEC 1ST MATERIAL RESPONSE

•

MATERIAL THICKNESS: 0.050 INCHES NOMINAL IN

•

AIRCRAFT LOCATION: STIFFENERS-LOWER EMPENAGE SUPPORTBEAM CLOSURE

•

MATERIAL: ALUMINUM ALLOY 2024

TECHNICAL CHARACTERISTICS

AIRCRAFT STATION NUMBER	822.640
MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-250/5,COND 0,T62 FED SPEC 1ST MATERIAL RESPONSE
OVERALL LENGTH	11.200 INCHES NOMINAL IN
OVERALL WIDTH	1.900 INCHES NOMINAL IN
MATERIAL THICKNESS	0.050 INCHES NOMINAL IN
SPECIAL FEATURES	NEXT HIGER ASSY,68A332201,U/O F-15A BLK 12 AND UP,F-15B BLK 12 AND UP,F-15C CUM 1 AND UP,F-15D CUM 1 AND UP,F-15E CUM 1-2,68A33200,U/O F-15E CUM 3-209,DIM.STOCK MATERIAL A
AIRCRAFT LOCATION	STIFFENERS-LOWER EMPENAGE SUPPORTBEAM CLOSURE
MATERIAL	ALUMINUM ALLOY 2024
SIDE FOR WHICH DESIGNED	LEFT SIDE
AIRCRAFT MISSION DESIGN SERIES	F-15A,B,C,D,E 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

Demilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 68A332197-2003?

68A332197-2003 is a STIFFENER,AIRCRAFT.

What is the NSN for 68A332197-2003?

68A332197-2003 is cataloged in the U.S. Government catalog under NSN 1560-01-467-4199. This indicates validated use in U.S. government and defense supply chains.

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68A332197-2003 — STIFFENER,AIRCRAFT

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