74A401530-2003 — 74A401530-2003

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

74A401530-2003: 74A401530-2003.

The 74A401530-2003 is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 5052, construction: LAMINATED, hole_diameter: 0.209 INCHES MINIMUM AND 0.224 INCHES MAXIMUM IN, overall_width: 1.25 INCHES NOMINAL IN, overall_length: 2.50 INCHES NOMINAL IN, overall_thickness: 0.062 INCHES NOMINAL IN. This part is cataloged in the U.S.

Government catalog under NSN 5365-01-702-7654, 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

74A401530-2003

NSN: 5365-01-702-7654
FSC: 5365 — Bushings, Rings, Shims, and Spacers
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 5052
construction	LAMINATED
hole_diameter	0.209 INCHES MINIMUM AND 0.224 INCHES MAXIMUM IN
overall_width	1.25 INCHES NOMINAL IN
overall_length	2.50 INCHES NOMINAL IN
overall_thickness	0.062 INCHES NOMINAL IN
mounting_hole_type	PLAIN AND THRU HOLE ALL HOLES
outside_corner_radius	0.25 INCHES NOMINAL IN
mounting_hole_quantity	4
end_item_identification	F/A-18E & F AND EA-18G AIRCRAFT G
criticality_code_justification	AGAV
material_document_and_classification	MIL-S-22499, CL2, TY1, CM+1 MIL SPEC SINGLE MATERIAL RESPONSE
NSN	5365-01-702-7654

COMPONENT DIAGRAM

KEY FEATURES

•

MOUNTING HOLE QUANTITY: 4

•

OVERALL THICKNESS: 0.062 INCHES NOMINAL IN

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

MATERIAL DOCUMENT AND CLASSIFICATION: MIL-S-22499, CL2, TY1, CM+1 MIL SPEC SINGLE MATERIAL RESPONSE

TECHNICAL CHARACTERISTICS

MOUNTING HOLE QUANTITY	4
OVERALL THICKNESS	0.062 INCHES NOMINAL IN
CRITICALITY CODE JUSTIFICATION	AGAV
MATERIAL DOCUMENT AND CLASSIFICATION	MIL-S-22499, CL2, TY1, CM+1 MIL SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH	2.50 INCHES NOMINAL IN
OVERALL WIDTH	1.25 INCHES NOMINAL IN
PART NAME ASSIGNED BY CONTROLLING AGENCY	SHIM
END ITEM IDENTIFICATION	F/A-18E & F AND EA-18G AIRCRAFT G
OUTSIDE CORNER RADIUS	0.25 INCHES NOMINAL IN
MATERIAL	ALUMINUM ALLOY 5052

OTHER ITEMS IN FSC 5365 — Bushings, Rings, Shims, and Spacers

Items in the same Federal Supply class. No interchangeability or substitution relationship is implied.

5365-00-000-6078 5365-00-000-7436 5365-00-001-1292 5365-00-001-1365 5365-00-001-1841 5365-00-001-1915 5365-00-001-1916 5365-00-001-1940

SUBSTITUTES & CROSS-REFERENCES 1

74A401530Reference 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)No demilitarization required

Ready to buy 74A401530-2003?

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 74A401530-2003?

74A401530-2003 is a 74A401530-2003.

What parts can replace 74A401530-2003?

There is 1 known substitute for 74A401530-2003: 74A401530. Substitute compatibility should be verified for your specific system.

What is the NSN for 74A401530-2003?

74A401530-2003 is cataloged in the U.S. Government catalog under NSN 5365-01-702-7654. This indicates validated use in U.S. government and defense supply chains.

Community Feedback

74A401530-2003 — 74A401530-2003

Request a Quote — 74A401530-2003