68A250556-2001 — PLATE,STRUCTURAL,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

68A250556-2001: PLATE,STRUCTURAL,AIRCRAFT.

The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_length: 15.750 INCHES NOMINAL IN, aircraft_location: SIDEPLATE - INBOARD PYLON, OUTBOARD SIDE, FS468.150 - FS483.900, material_thickness: 0.250 INCHES NOMINAL IN, aircraft_station_number: FS468.150 TO FS483.900, end_item_identification: F-15 AIRCRAFT. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-445-6064, 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

68A250556-2001

NSN: 1560-01-445-6064
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 7075
overall_length	15.750 INCHES NOMINAL IN
aircraft_location	SIDEPLATE - INBOARD PYLON, OUTBOARD SIDE, FS468.150 - FS483.900
material_thickness	0.250 INCHES NOMINAL IN
aircraft_station_number	FS468.150 TO FS483.900
end_item_identification	F-15 AIRCRAFT
aircraft_mission_design_series	F-15
material_document_and_classification	MMS 159 PLATE COND-T7351 MFR REF SINGLE MATERIAL RESPONSE
NSN	1560-01-445-6064

COMPONENT DIAGRAM

KEY FEATURES

•

AIRCRAFT STATION NUMBER: FS468.150 TO FS483.900

•

MATERIAL DOCUMENT AND CLASSIFICATION: MMS 159 PLATE COND-T7351 MFR REF SINGLE MATERIAL RESPONSE

•

MATERIAL THICKNESS: 0.250 INCHES NOMINAL IN

•

AIRCRAFT LOCATION: SIDEPLATE - INBOARD PYLON, OUTBOARD SIDE, FS468.150 - FS483.900

•

MATERIAL: ALUMINUM ALLOY 7075

•

AIRCRAFT MISSION DESIGN SERIES: F-15

TECHNICAL CHARACTERISTICS

AIRCRAFT STATION NUMBER	FS468.150 TO FS483.900
MATERIAL DOCUMENT AND CLASSIFICATION	MMS 159 PLATE COND-T7351 MFR REF SINGLE MATERIAL RESPONSE
OVERALL LENGTH	15.750 INCHES NOMINAL IN
MATERIAL THICKNESS	0.250 INCHES NOMINAL IN
AIRCRAFT LOCATION	SIDEPLATE - INBOARD PYLON, OUTBOARD SIDE, FS468.150 - FS483.900
END ITEM IDENTIFICATION	F-15 AIRCRAFT
MATERIAL	ALUMINUM ALLOY 7075
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 68A250556-2001?

68A250556-2001 is a PLATE,STRUCTURAL,AIRCRAFT.

What is the NSN for 68A250556-2001?

68A250556-2001 is cataloged in the U.S. Government catalog under NSN 1560-01-445-6064. This indicates validated use in U.S. government and defense supply chains.

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68A250556-2001 — PLATE,STRUCTURAL,AIRCRAFT

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