68A230001-2003 — PLATE,STRUCTURAL,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

68A230001-2003: PLATE,STRUCTURAL,AIRCRAFT.

The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 5052, overall_width: 0.750 INCHES NOMINAL IN, overall_length: 13.150 INCHES NOMINAL IN, special_features: NHA 68A230021; U/O F-15C CUM270&UP, F-15D CUM45&UP, F-15E CUM1-128, aircraft_location: VERTICAL STABILIZER, material_thickness: 0.048 INCHES NOMINAL IN. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-481-8353, 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

68A230001-2003

NSN: 1560-01-481-8353
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 5052
overall_width	0.750 INCHES NOMINAL IN
overall_length	13.150 INCHES NOMINAL IN
special_features	NHA 68A230021; U/O F-15C CUM270&UP, F-15D CUM45&UP, F-15E CUM1-128
aircraft_location	VERTICAL STABILIZER
material_thickness	0.048 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	SHIM
NSN	1560-01-481-8353

COMPONENT DIAGRAM

KEY FEATURES

•

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

•

MATERIAL THICKNESS: 0.048 INCHES NOMINAL IN

•

AIRCRAFT LOCATION: 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	13.150 INCHES NOMINAL IN
OVERALL WIDTH	0.750 INCHES NOMINAL IN
MATERIAL THICKNESS	0.048 INCHES NOMINAL IN
SPECIAL FEATURES	NHA 68A230021; U/O F-15C CUM270&UP, F-15D CUM45&UP, F-15E CUM1-128
AIRCRAFT LOCATION	VERTICAL STABILIZER
PART NAME ASSIGNED BY CONTROLLING AGENCY	SHIM
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 1

68A230001-2003WSame NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

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 68A230001-2003?

68A230001-2003 is a PLATE,STRUCTURAL,AIRCRAFT.

What parts can replace 68A230001-2003?

There is 1 known substitute for 68A230001-2003: 68A230001-2003W. Substitute compatibility should be verified for your specific system.

What is the NSN for 68A230001-2003?

68A230001-2003 is cataloged in the U.S. Government catalog under NSN 1560-01-481-8353. This indicates validated use in U.S. government and defense supply chains.

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