68A332013-2006 — RIB,STIFFENER,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

68A332013-2006: RIB,STIFFENER,AIRCRAFT.

The RIB,STIFFENER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: TITANIUM ALLOY, overall_width: 1.400 INCHES NOMINAL IN, overall_length: 5.400 INCHES NOMINAL IN, special_features: NEXT HIGHER ASSY,68A332001,U/O F-15A CUM1-BLK 11,F-15B CUM 1-BLK 11,DIM.STOCK MATERIAL A, aircraft_location: FORMER-FS837,AFT CLOSURE BEAM, material_thickness: 0.028 INCHES NOMINAL IN. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-467-4201, 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

68A332013-2006

NSN: 1560-01-467-4201
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)

SPECIFICATIONS

material	TITANIUM ALLOY
overall_width	1.400 INCHES NOMINAL IN
overall_length	5.400 INCHES NOMINAL IN
special_features	NEXT HIGHER ASSY,68A332001,U/O F-15A CUM1-BLK 11,F-15B CUM 1-BLK 11,DIM.STOCK MATERIAL A
aircraft_location	FORMER-FS837,AFT CLOSURE BEAM
material_thickness	0.028 INCHES NOMINAL IN
aircraft_station_number	837
side_for_which_designed	RIGHT SIDE
aircraft_mission_design_series	F-15A,B A
material_document_and_classification	MIL-T-9046,TYPE3,CMPSNC,ANL MIL SPEC 1ST MATERIAL RESPONSE
NSN	1560-01-467-4201

COMPONENT DIAGRAM

KEY FEATURES

•

AIRCRAFT STATION NUMBER: 837

•

MATERIAL DOCUMENT AND CLASSIFICATION: MIL-T-9046,TYPE3,CMPSNC,ANL MIL SPEC 1ST MATERIAL RESPONSE

•

MATERIAL THICKNESS: 0.028 INCHES NOMINAL IN

•

AIRCRAFT LOCATION: FORMER-FS837,AFT CLOSURE BEAM

•

MATERIAL: TITANIUM ALLOY

TECHNICAL CHARACTERISTICS

AIRCRAFT STATION NUMBER	837
MATERIAL DOCUMENT AND CLASSIFICATION	MIL-T-9046,TYPE3,CMPSNC,ANL MIL SPEC 1ST MATERIAL RESPONSE
OVERALL LENGTH	5.400 INCHES NOMINAL IN
OVERALL WIDTH	1.400 INCHES NOMINAL IN
MATERIAL THICKNESS	0.028 INCHES NOMINAL IN
SPECIAL FEATURES	NEXT HIGHER ASSY,68A332001,U/O F-15A CUM1-BLK 11,F-15B CUM 1-BLK 11,DIM.STOCK MATERIAL A
AIRCRAFT LOCATION	FORMER-FS837,AFT CLOSURE BEAM
MATERIAL	TITANIUM ALLOY
SIDE FOR WHICH DESIGNED	RIGHT SIDE
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.

1560-00-003-1977 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 68A332013-2006?

68A332013-2006 is a RIB,STIFFENER,AIRCRAFT.

What is the NSN for 68A332013-2006?

68A332013-2006 is cataloged in the U.S. Government catalog under NSN 1560-01-467-4201. This indicates validated use in U.S. government and defense supply chains.

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68A332013-2006 — RIB,STIFFENER,AIRCRAFT

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