160J611335-17 — PLATE,STRUCTURAL,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

160J611335-17: PLATE,STRUCTURAL,AIRCRAFT.

The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 6.000 INCHES NOMINAL IN, overall_length: 15.000 INCHES NOMINAL IN, aircraft_location: WING CTR. PANEL-FRT.

SPAR WEB, material_thickness: 0.100 INCHES NOMINAL IN, aircraft_station_number: WS44.5 TO WS54.0. This part is cataloged in the U.S. Government catalog under NSN 1560-01-488-9632, 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

160J611335-17

NSN: 1560-01-488-9632
FSC: 1560 — Airframe Structural Components
CAGE: 79RG9 — NORTHROP GRUMMAN SYSTEMS CORPORATION (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 7075
overall_width	6.000 INCHES NOMINAL IN
overall_length	15.000 INCHES NOMINAL IN
special_features	AND WS 79.0 LH;DIMENSIONS ARE STOCKSIZE; NHA -2; STRENGTH T6 BARE; MANUFACTURE SUGGESTED NAME(A/0A-10A WING CTR. PANEL REPAIR-FRT. SPAR WEB) A
aircraft_location	WING CTR. PANEL-FRT. SPAR WEB
material_thickness	0.100 INCHES NOMINAL IN
aircraft_station_number	WS44.5 TO WS54.0
side_for_which_designed	BOTH SIDES
aircraft_mission_design_series	A-10A A
material_document_and_classification	QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE
NSN	1560-01-488-9632

COMPONENT DIAGRAM

KEY FEATURES

•

AIRCRAFT STATION NUMBER: WS44.5 TO WS54.0

•

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

•

MATERIAL THICKNESS: 0.100 INCHES NOMINAL IN

•

AIRCRAFT LOCATION: WING CTR. PANEL-FRT. SPAR WEB

•

MATERIAL: ALUMINUM ALLOY 7075

TECHNICAL CHARACTERISTICS

AIRCRAFT STATION NUMBER	WS44.5 TO WS54.0
MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH	15.000 INCHES NOMINAL IN
OVERALL WIDTH	6.000 INCHES NOMINAL IN
MATERIAL THICKNESS	0.100 INCHES NOMINAL IN
SPECIAL FEATURES	AND WS 79.0 LH;DIMENSIONS ARE STOCKSIZE; NHA -2; STRENGTH T6 BARE; MANUFACTURE SUGGESTED NAME(A/0A-10A WING CTR. PANEL REPAIR-FRT. SPAR WEB) A
AIRCRAFT LOCATION	WING CTR. PANEL-FRT. SPAR WEB
MATERIAL	ALUMINUM ALLOY 7075
SIDE FOR WHICH DESIGNED	BOTH SIDES
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: Normally procured from the manufacturer (OEM)Demilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 160J611335-17?

160J611335-17 is a PLATE,STRUCTURAL,AIRCRAFT.

What is the NSN for 160J611335-17?

160J611335-17 is cataloged in the U.S. Government catalog under NSN 1560-01-488-9632. This indicates validated use in U.S. government and defense supply chains.

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160J611335-17 — PLATE,STRUCTURAL,AIRCRAFT

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