160J612461-11 — PLATE,STRUCTURAL,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

160J612461-11: PLATE,STRUCTURAL,AIRCRAFT.

The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 7.000 INCHES NOMINAL IN, overall_length: 29.500 INCHES NOMINAL IN, special_features: HEAT TREAT T6; NHA IS -2; DIMENSIONS ARE STOCKSIZE; MANF. SUGGESTED NAME(DOUBLER-MID SPAR WEB), aircraft_location: WING OUTER PANEL REPAIR, material_thickness: 0.071 INCHES NOMINAL IN.

This part is cataloged in the U.S. Government catalog under NSN 1560-01-490-4166, 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

160J612461-11

NSN: 1560-01-490-4166
FSC: 1560 — Airframe Structural Components
CAGE: 79RG9 — NORTHROP GRUMMAN SYSTEMS CORPORATION (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 7075
overall_width	7.000 INCHES NOMINAL IN
overall_length	29.500 INCHES NOMINAL IN
special_features	HEAT TREAT T6; NHA IS -2; DIMENSIONS ARE STOCKSIZE; MANF. SUGGESTED NAME(DOUBLER-MID SPAR WEB)
aircraft_location	WING OUTER PANEL REPAIR
material_thickness	0.071 INCHES NOMINAL IN
aircraft_station_number	WS 110 TO WS 143
aircraft_mission_design_series	A-10A A
material_document_and_classification	QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE
NSN	1560-01-490-4166

COMPONENT DIAGRAM

KEY FEATURES

•

AIRCRAFT STATION NUMBER: WS 110 TO WS 143

•

MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE

•

MATERIAL THICKNESS: 0.071 INCHES NOMINAL IN

•

AIRCRAFT LOCATION: WING OUTER PANEL REPAIR

•

MATERIAL: ALUMINUM ALLOY 7075

TECHNICAL CHARACTERISTICS

AIRCRAFT STATION NUMBER	WS 110 TO WS 143
MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH	29.500 INCHES NOMINAL IN
OVERALL WIDTH	7.000 INCHES NOMINAL IN
MATERIAL THICKNESS	0.071 INCHES NOMINAL IN
SPECIAL FEATURES	HEAT TREAT T6; NHA IS -2; DIMENSIONS ARE STOCKSIZE; MANF. SUGGESTED NAME(DOUBLER-MID SPAR WEB)
AIRCRAFT LOCATION	WING OUTER PANEL REPAIR
MATERIAL	ALUMINUM ALLOY 7075
AIRCRAFT MISSION DESIGN SERIES	A-10A A

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

160J612461Reference document

Same NSN cross-reference

Reference document — Drawing number reference only

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 160J612461-11?

160J612461-11 is a PLATE,STRUCTURAL,AIRCRAFT.

What parts can replace 160J612461-11?

There is 1 known substitute for 160J612461-11: 160J612461. Substitute compatibility should be verified for your specific system.

What is the NSN for 160J612461-11?

160J612461-11 is cataloged in the U.S. Government catalog under NSN 1560-01-490-4166. This indicates validated use in U.S. government and defense supply chains.

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160J612461-11 — PLATE,STRUCTURAL,AIRCRAFT

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