68A332135-2001 — PLATE,STRUCTURAL,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

68A332135-2001: PLATE,STRUCTURAL,AIRCRAFT.

The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: TITANIUM ALLOY, overall_width: 2.250 INCHES NOMINAL IN, overall_length: 9.000 INCHES NOMINAL IN, special_features: DIM. STOCK MATERIAL; NEXT HIGHER ASSY 68A332013 U/O F-15A 1&UP A, aircraft_location: FORMER AFT CLOSURE BEAM, material_thickness: 1.500 INCHES NOMINAL IN.

This part is cataloged in the U.S. Government catalog under NSN 1560-01-467-2913, 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

68A332135-2001

NSN: 1560-01-467-2913
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)

SPECIFICATIONS

material	TITANIUM ALLOY
overall_width	2.250 INCHES NOMINAL IN
overall_length	9.000 INCHES NOMINAL IN
special_features	DIM. STOCK MATERIAL; NEXT HIGHER ASSY 68A332013 U/O F-15A 1&UP A
aircraft_location	FORMER AFT CLOSURE BEAM
material_thickness	1.500 INCHES NOMINAL IN
aircraft_station_number	FS837
side_for_which_designed	LEFT SIDE
aircraft_mission_design_series	F-15A A
material_document_and_classification	MIL-T-9047,TYPE 3,COMP A,ANL MIL SPEC SINGLE MATERIAL RESPONSE
part_name_assigned_by_controlling_agency	CAP
NSN	1560-01-467-2913

COMPONENT DIAGRAM

KEY FEATURES

•

AIRCRAFT STATION NUMBER: FS837

•

MATERIAL DOCUMENT AND CLASSIFICATION: MIL-T-9047,TYPE 3,COMP A,ANL MIL SPEC SINGLE MATERIAL RESPONSE

•

MATERIAL THICKNESS: 1.500 INCHES NOMINAL IN

•

AIRCRAFT LOCATION: FORMER AFT CLOSURE BEAM

TECHNICAL CHARACTERISTICS

AIRCRAFT STATION NUMBER	FS837
MATERIAL DOCUMENT AND CLASSIFICATION	MIL-T-9047,TYPE 3,COMP A,ANL MIL SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH	9.000 INCHES NOMINAL IN
OVERALL WIDTH	2.250 INCHES NOMINAL IN
MATERIAL THICKNESS	1.500 INCHES NOMINAL IN
SPECIAL FEATURES	DIM. STOCK MATERIAL; NEXT HIGHER ASSY 68A332013 U/O F-15A 1&UP A
AIRCRAFT LOCATION	FORMER AFT CLOSURE BEAM
PART NAME ASSIGNED BY CONTROLLING AGENCY	CAP
MATERIAL	TITANIUM ALLOY
SIDE FOR WHICH DESIGNED	LEFT SIDE

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 68A332135-2001?

68A332135-2001 is a PLATE,STRUCTURAL,AIRCRAFT.

What is the NSN for 68A332135-2001?

68A332135-2001 is cataloged in the U.S. Government catalog under NSN 1560-01-467-2913. This indicates validated use in U.S. government and defense supply chains.

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68A332135-2001 — PLATE,STRUCTURAL,AIRCRAFT

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