68A332026-2115 — PLATE,STRUCTURAL,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

68A332026-2115: PLATE,STRUCTURAL,AIRCRAFT.

The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: TITANIUM ALLOY, overall_width: 22.000 INCHES NOMINAL IN, overall_length: 34.700 INCHES NOMINAL IN, special_features: WEB;MATERIAL:6AL-6V-2SN V, aircraft_location: INBOARD SHEAR BEAM-EMPENNAGE SUPPORT BEAM FS712.310 TO CFS791.650, material_thickness: 0.036 INCHES NOMINAL IN. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-421-1195, 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

68A332026-2115

NSN: 1560-01-421-1195
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)

SPECIFICATIONS

material	TITANIUM ALLOY
overall_width	22.000 INCHES NOMINAL IN
overall_length	34.700 INCHES NOMINAL IN
special_features	WEB;MATERIAL:6AL-6V-2SN V
aircraft_location	INBOARD SHEAR BEAM-EMPENNAGE SUPPORT BEAM FS712.310 TO CFS791.650
material_thickness	0.036 INCHES NOMINAL IN
aircraft_mission_design_series	F-15S
material_document_and_classification	MMS-1203 MFR REF SINGLE MATERIAL RESPONSE
NSN	1560-01-421-1195

COMPONENT DIAGRAM

KEY FEATURES

•

MATERIAL DOCUMENT AND CLASSIFICATION: MMS-1203 MFR REF SINGLE MATERIAL RESPONSE

•

MATERIAL THICKNESS: 0.036 INCHES NOMINAL IN

•

AIRCRAFT LOCATION: INBOARD SHEAR BEAM-EMPENNAGE SUPPORT BEAM FS712.310 TO CFS791.650

•

MATERIAL: TITANIUM ALLOY

•

AIRCRAFT MISSION DESIGN SERIES: F-15S

TECHNICAL CHARACTERISTICS

MATERIAL DOCUMENT AND CLASSIFICATION	MMS-1203 MFR REF SINGLE MATERIAL RESPONSE
OVERALL LENGTH	34.700 INCHES NOMINAL IN
OVERALL WIDTH	22.000 INCHES NOMINAL IN
MATERIAL THICKNESS	0.036 INCHES NOMINAL IN
SPECIAL FEATURES	WEB;MATERIAL:6AL-6V-2SN V
AIRCRAFT LOCATION	INBOARD SHEAR BEAM-EMPENNAGE SUPPORT BEAM FS712.310 TO CFS791.650
MATERIAL	TITANIUM ALLOY
AIRCRAFT MISSION DESIGN SERIES	F-15S

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 68A332026-2115?

68A332026-2115 is a PLATE,STRUCTURAL,AIRCRAFT.

What is the NSN for 68A332026-2115?

68A332026-2115 is cataloged in the U.S. Government catalog under NSN 1560-01-421-1195. This indicates validated use in U.S. government and defense supply chains.

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68A332026-2115 — PLATE,STRUCTURAL,AIRCRAFT

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