74A501237-2006 — BRACKET,STRUCTURAL COMPONENT,AIR

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

74A501237-2006: BRACKET,STRUCTURAL COMPONENT,AIR.

BRACKET,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 1.290 INCHES NOMINAL IN, overall_length: 6.200 INCHES NOMINAL IN, aircraft_location: ENGINE MOUNT, OUTBOARD, material_thickness: 0.050 INCHES NOMINAL IN, end_item_identification: EF-18, AIRCRAFT. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-528-9249, 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

74A501237-2006

NSN: 1560-01-528-9249
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 7075
overall_width	1.290 INCHES NOMINAL IN
overall_length	6.200 INCHES NOMINAL IN
aircraft_location	ENGINE MOUNT, OUTBOARD
material_thickness	0.050 INCHES NOMINAL IN
end_item_identification	EF-18, AIRCRAFT
aircraft_mission_design_series	EF-18
material_document_and_classification	QQ-A-250/13 COND T6 FED SPEC SINGLE MATERIAL RESPONSE
part_name_assigned_by_controlling_agency	BRACKET, ALIGNMENT, SUPPORT, FAIL SAFE ENGINE MOUNT, OUTBOARD
NSN	1560-01-528-9249

COMPONENT DIAGRAM

KEY FEATURES

•

MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/13 COND T6 FED SPEC SINGLE MATERIAL RESPONSE

•

MATERIAL THICKNESS: 0.050 INCHES NOMINAL IN

•

AIRCRAFT LOCATION: ENGINE MOUNT, OUTBOARD

•

MATERIAL: ALUMINUM ALLOY 7075

TECHNICAL CHARACTERISTICS

MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-250/13 COND T6 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH	6.200 INCHES NOMINAL IN
OVERALL WIDTH	1.290 INCHES NOMINAL IN
MATERIAL THICKNESS	0.050 INCHES NOMINAL IN
AIRCRAFT LOCATION	ENGINE MOUNT, OUTBOARD
PART NAME ASSIGNED BY CONTROLLING AGENCY	BRACKET, ALIGNMENT, SUPPORT, FAIL SAFE ENGINE MOUNT, OUTBOARD
END ITEM IDENTIFICATION	EF-18, AIRCRAFT
MATERIAL	ALUMINUM ALLOY 7075
AIRCRAFT MISSION DESIGN SERIES	EF-18

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

Demilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 74A501237-2006?

74A501237-2006 is a BRACKET,STRUCTURAL COMPONENT,AIR.

What is the NSN for 74A501237-2006?

74A501237-2006 is cataloged in the U.S. Government catalog under NSN 1560-01-528-9249. This indicates validated use in U.S. government and defense supply chains.

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74A501237-2006 — BRACKET,STRUCTURAL COMPONENT,AIR

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