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160D214005-121 — PLATE,STRUCTURAL,AIRCRAFT

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

160D214005-121: PLATE,STRUCTURAL,AIRCRAFT.

The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 43.400 INCHES NOMINAL IN, overall_length: 48.000 INCHES NOMINAL IN, aircraft_location: FLOOR INSTALLATION,AFT FUEL CELL, material_thickness: 0.125 INCHES NOMINAL IN, aircraft_station_number: STATION 481.00 TO STATION 524.30. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-174-7145, 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
160D214005-121
NSN: 1560-01-174-7145
FSC: 1560 — Airframe Structural Components
CAGE: 79RG9 — NORTHROP GRUMMAN SYSTEMS CORPORATION (USA)
SPECIFICATIONS
materialALUMINUM ALLOY 7075
overall_width43.400 INCHES NOMINAL IN
overall_length48.000 INCHES NOMINAL IN
aircraft_locationFLOOR INSTALLATION,AFT FUEL CELL
material_thickness0.125 INCHES NOMINAL IN
aircraft_station_numberSTATION 481.00 TO STATION 524.30
aircraft_mission_design_seriesA10
material_document_and_classificationQQ-A-250/12-0 FED SPEC SINGLE MATERIAL RESPONSE
NSN1560-01-174-7145
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available PLATE,STRUCTURAL,AIRCRAFT TITLE COMPONENT PN 160D214005-121 MFR PLATE,STRUCTURAL,AIRCR
KEY FEATURES
•
AIRCRAFT STATION NUMBER: STATION 481.00 TO STATION 524.30
•
MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/12-0 FED SPEC SINGLE MATERIAL RESPONSE
•
MATERIAL THICKNESS: 0.125 INCHES NOMINAL IN
•
AIRCRAFT LOCATION: FLOOR INSTALLATION,AFT FUEL CELL
•
MATERIAL: ALUMINUM ALLOY 7075
•
AIRCRAFT MISSION DESIGN SERIES: A10
TECHNICAL CHARACTERISTICS
AIRCRAFT STATION NUMBERSTATION 481.00 TO STATION 524.30
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-250/12-0 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH48.000 INCHES NOMINAL IN
OVERALL WIDTH43.400 INCHES NOMINAL IN
MATERIAL THICKNESS0.125 INCHES NOMINAL IN
AIRCRAFT LOCATIONFLOOR INSTALLATION,AFT FUEL CELL
MATERIALALUMINUM ALLOY 7075
AIRCRAFT MISSION DESIGN SERIESA10
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: Insurance item — stocked against contingency demandDemilitarization required — critical (Q)
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FREQUENTLY ASKED QUESTIONS
What is 160D214005-121?
160D214005-121 is a PLATE,STRUCTURAL,AIRCRAFT.
What is the NSN for 160D214005-121?
160D214005-121 is cataloged in the U.S. Government catalog under NSN 1560-01-174-7145. This indicates validated use in U.S. government and defense supply chains.
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✓ PartsTable — the parts reference. Every fact cited to its source.
PartsTable Design LLC · partstable.com
U.S. Government catalog: edition PUBLOGDVD v12.0.0 (OCT 2026), edition date 2026-10-01, retrieved 2026-10-18.
PartsTable commercial catalog: edition Unified commercial catalog snapshot through 2026-09-28, edition date not on file, retrieved 2026-09-28.