68A230091-2007 — PLATE,STRUCTURAL,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

68A230091-2007: PLATE,STRUCTURAL,AIRCRAFT.

The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 5052, overall_width: 0.760 INCHES NOMINAL IN, overall_length: 2.700 INCHES NOMINAL IN, special_features: DIM. ARE STOCK MATERIAL; U/O F-15A CUM223&UP, F-15B CUM36&UP, F-15C CUM1&UP, F-15D CUM1&UP, F-15E CUM1-67 A, aircraft_location: UPPER AFT BOX,VERTICAL STABILIZER, material_thickness: 0.094 INCHES NOMINAL IN.

This part is cataloged in the U.S. Government catalog under NSN 1560-01-481-9280, 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

68A230091-2007

NSN: 1560-01-481-9280
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 5052
overall_width	0.760 INCHES NOMINAL IN
overall_length	2.700 INCHES NOMINAL IN
special_features	DIM. ARE STOCK MATERIAL; U/O F-15A CUM223&UP, F-15B CUM36&UP, F-15C CUM1&UP, F-15D CUM1&UP, F-15E CUM1-67 A
aircraft_location	UPPER AFT BOX,VERTICAL STABILIZER
material_thickness	0.094 INCHES NOMINAL IN
aircraft_mission_design_series	F-15
material_document_and_classification	MIL-S-22499 CLASS 2 TYPE 1 MIL SPEC SINGLE MATERIAL RESPONSE
part_name_assigned_by_controlling_agency	FILLER
NSN	1560-01-481-9280

COMPONENT DIAGRAM

KEY FEATURES

•

MATERIAL DOCUMENT AND CLASSIFICATION: MIL-S-22499 CLASS 2 TYPE 1 MIL SPEC SINGLE MATERIAL RESPONSE

•

MATERIAL THICKNESS: 0.094 INCHES NOMINAL IN

•

AIRCRAFT LOCATION: UPPER AFT BOX,VERTICAL STABILIZER

•

MATERIAL: ALUMINUM ALLOY 5052

TECHNICAL CHARACTERISTICS

MATERIAL DOCUMENT AND CLASSIFICATION	MIL-S-22499 CLASS 2 TYPE 1 MIL SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH	2.700 INCHES NOMINAL IN
OVERALL WIDTH	0.760 INCHES NOMINAL IN
MATERIAL THICKNESS	0.094 INCHES NOMINAL IN
SPECIAL FEATURES	DIM. ARE STOCK MATERIAL; U/O F-15A CUM223&UP, F-15B CUM36&UP, F-15C CUM1&UP, F-15D CUM1&UP, F-15E CUM1-67 A
AIRCRAFT LOCATION	UPPER AFT BOX,VERTICAL STABILIZER
PART NAME ASSIGNED BY CONTROLLING AGENCY	FILLER
MATERIAL	ALUMINUM ALLOY 5052
AIRCRAFT MISSION DESIGN SERIES	F-15

OTHER ITEMS IN FSC 1560 — Airframe Structural Components

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

1560-00-000-0047 1560-00-001-1849 1560-00-001-1850 1560-00-001-1851 1560-00-001-2368 1560-00-001-2478 1560-00-001-2479 1560-00-001-2480

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 68A230091-2007?

68A230091-2007 is a PLATE,STRUCTURAL,AIRCRAFT.

What is the NSN for 68A230091-2007?

68A230091-2007 is cataloged in the U.S. Government catalog under NSN 1560-01-481-9280. This indicates validated use in U.S. government and defense supply chains.

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68A230091-2007 — PLATE,STRUCTURAL,AIRCRAFT

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