160J611239-13 — PLATE,STRUCTURAL,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

160J611239-13: PLATE,STRUCTURAL,AIRCRAFT.

The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 3.000 INCHES NOMINAL IN, overall_length: 21.000 INCHES NOMINAL IN, special_features: DIMENSIONS ARE STOCKSIZE; MANF. SUGGESTED NAME (STRL PL-FILLER); STRENGTH T6; NHA -2; EFF.

TYPE A FROM 7 THRUON, aircraft_location: LWR REAR SPAR-CTR WG PANEL, material_thickness: 0.180 INCHES NOMINAL IN. This part is cataloged in the U.S. Government catalog under NSN 1560-01-488-7409, 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

160J611239-13

NSN: 1560-01-488-7409
FSC: 1560 — Airframe Structural Components
CAGE: 79RG9 — NORTHROP GRUMMAN SYSTEMS CORPORATION (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 7075
overall_width	3.000 INCHES NOMINAL IN
overall_length	21.000 INCHES NOMINAL IN
special_features	DIMENSIONS ARE STOCKSIZE; MANF. SUGGESTED NAME (STRL PL-FILLER); STRENGTH T6; NHA -2; EFF. TYPE A FROM 7 THRUON
aircraft_location	LWR REAR SPAR-CTR WG PANEL
material_thickness	0.180 INCHES NOMINAL IN
aircraft_station_number	WGS44.5 TO WGS66.0
aircraft_mission_design_series	A-10A A
material_document_and_classification	QQ-A-250/13 FED SPEC SINGLE MATERIAL RESPONSE
NSN	1560-01-488-7409

COMPONENT DIAGRAM

KEY FEATURES

•

AIRCRAFT STATION NUMBER: WGS44.5 TO WGS66.0

•

MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/13 FED SPEC SINGLE MATERIAL RESPONSE

•

MATERIAL THICKNESS: 0.180 INCHES NOMINAL IN

•

AIRCRAFT LOCATION: LWR REAR SPAR-CTR WG PANEL

•

MATERIAL: ALUMINUM ALLOY 7075

TECHNICAL CHARACTERISTICS

AIRCRAFT STATION NUMBER	WGS44.5 TO WGS66.0
MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-250/13 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH	21.000 INCHES NOMINAL IN
OVERALL WIDTH	3.000 INCHES NOMINAL IN
MATERIAL THICKNESS	0.180 INCHES NOMINAL IN
SPECIAL FEATURES	DIMENSIONS ARE STOCKSIZE; MANF. SUGGESTED NAME (STRL PL-FILLER); STRENGTH T6; NHA -2; EFF. TYPE A FROM 7 THRUON
AIRCRAFT LOCATION	LWR REAR SPAR-CTR WG PANEL
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.

1560-00-003-1977 1560-00-003-3257 1560-00-004-4244 1560-00-005-7280 1560-00-006-0576 1560-00-006-6538 1560-00-007-9578 1560-00-009-4192

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)

Ready to buy 160J611239-13?

Compare prices from verified sellers on eBay

Buy on eBay →

As an eBay Partner, PartsTable may earn a commission. Your price is not affected.

FREQUENTLY ASKED QUESTIONS

What is 160J611239-13?

160J611239-13 is a PLATE,STRUCTURAL,AIRCRAFT.

What is the NSN for 160J611239-13?

160J611239-13 is cataloged in the U.S. Government catalog under NSN 1560-01-488-7409. This indicates validated use in U.S. government and defense supply chains.

Community Feedback

160J611239-13 — PLATE,STRUCTURAL,AIRCRAFT

Request a Quote — 160J611239-13