160D612421-126 — SUPPORT,STRUCTURAL COMPONENT,AIR

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

160D612421-126: SUPPORT,STRUCTURAL COMPONENT,AIR.

SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 4.000 INCHES NOMINAL IN, overall_length: 7.000 INCHES NOMINAL IN, aircraft_location: RIB INSTL OUTBD WING PANEL, material_thickness: 0.063 INCHES NOMINAL IN, aircraft_station_number: WING STA 331.84. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-515-0601, 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

160D612421-126

NSN: 1560-01-515-0601
FSC: 1560 — Airframe Structural Components
CAGE: 79RG9 — NORTHROP GRUMMAN SYSTEMS CORPORATION (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 7075
overall_width	4.000 INCHES NOMINAL IN
overall_length	7.000 INCHES NOMINAL IN
special_features	NHA 160D612101; DIMS ARE STOCK MATERIAL; -126 OPP -125; HEAT TREAT PER MIL-H-6088, 7075-0 TO T-6 AND 2024-0 TO T-42 AFTER FORMING
aircraft_location	RIB INSTL OUTBD WING PANEL
material_thickness	0.063 INCHES NOMINAL IN
aircraft_station_number	WING STA 331.84
aircraft_mission_design_series	A-10
material_document_and_classification	QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE
part_name_assigned_by_controlling_agency	ANGLE
NSN	1560-01-515-0601

COMPONENT DIAGRAM

KEY FEATURES

•

AIRCRAFT STATION NUMBER: WING STA 331.84

•

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

•

MATERIAL THICKNESS: 0.063 INCHES NOMINAL IN

•

AIRCRAFT LOCATION: RIB INSTL OUTBD WING PANEL

TECHNICAL CHARACTERISTICS

AIRCRAFT STATION NUMBER	WING STA 331.84
MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH	7.000 INCHES NOMINAL IN
OVERALL WIDTH	4.000 INCHES NOMINAL IN
MATERIAL THICKNESS	0.063 INCHES NOMINAL IN
SPECIAL FEATURES	NHA 160D612101; DIMS ARE STOCK MATERIAL; -126 OPP -125; HEAT TREAT PER MIL-H-6088, 7075-0 TO T-6 AND 2024-0 TO T-42 AFTER FORMING
AIRCRAFT LOCATION	RIB INSTL OUTBD WING PANEL
PART NAME ASSIGNED BY CONTROLLING AGENCY	ANGLE
MATERIAL	ALUMINUM ALLOY 7075
AIRCRAFT MISSION DESIGN SERIES	A-10

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 160D612421-126?

160D612421-126 is a SUPPORT,STRUCTURAL COMPONENT,AIR.

What is the NSN for 160D612421-126?

160D612421-126 is cataloged in the U.S. Government catalog under NSN 1560-01-515-0601. This indicates validated use in U.S. government and defense supply chains.

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160D612421-126 — SUPPORT,STRUCTURAL COMPONENT,AIR

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