PL74A886604 — BRACKET,STRUCTURAL COMPONENT,AIR

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

PL74A886604: BRACKET,STRUCTURAL COMPONENT,AIR.

BRACKET,STRUCTURAL COMPONENT,AIR. Key specifications include height: 0.62 INCHES NOMINAL IN, material: ALUMINUM ALLOY 7075, overall_width: 1.672 INCHES NOMINAL IN, overall_length: 2.00 INCHES NOMINAL IN, aircraft_location: AFT/CTR FUSELAGE, material_thickness: 0.078 INCHES NOMINAL IN. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-710-5177, 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

PL74A886604

NSN: 1560-01-710-5177
NIINs: 017105177, 017105789, 017105840, 017105934, 017105939, 017106003, 017106005, 017106147, 017106289, 017106293, 017106429, 017106434, 017106642, 017107562, 017107571, 017107603
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)

SPECIFICATIONS

height	0.62 INCHES NOMINAL IN
material	ALUMINUM ALLOY 7075
overall_width	1.672 INCHES NOMINAL IN
overall_length	2.00 INCHES NOMINAL IN
aircraft_location	AFT/CTR FUSELAGE
material_thickness	0.078 INCHES NOMINAL IN
end_item_identification	EA-18G/F/A-18 E AND F AIRCRAFT G
aircraft_mission_design_series	EA-18G/F/A-18 E AND F AIRCRAFT G
material_document_and_classification	QQ-A-200/15 FED SPEC SINGLE MATERIAL RESPONSE
part_name_assigned_by_controlling_agency	BRACKET, EXTRUDED SUPPORT
surface_treatment_document_and_classification	74A901001 COMMERCIAL ITEM DESCRIPTION SINGLE TREATMENT RESPONSE
NSN	1560-01-710-5177

COMPONENT DIAGRAM

KEY FEATURES

•

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION: 74A901001 COMMERCIAL ITEM DESCRIPTION SINGLE TREATMENT RESPONSE

•

MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-200/15 FED SPEC SINGLE MATERIAL RESPONSE

•

MATERIAL THICKNESS: 0.078 INCHES NOMINAL IN

•

HEIGHT: 0.62 INCHES NOMINAL IN

•

AIRCRAFT LOCATION: AFT/CTR FUSELAGE

TECHNICAL CHARACTERISTICS

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION	74A901001 COMMERCIAL ITEM DESCRIPTION SINGLE TREATMENT RESPONSE
MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-200/15 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH	2.00 INCHES NOMINAL IN
OVERALL WIDTH	1.672 INCHES NOMINAL IN
MATERIAL THICKNESS	0.078 INCHES NOMINAL IN
HEIGHT	0.62 INCHES NOMINAL IN
AIRCRAFT LOCATION	AFT/CTR FUSELAGE
PART NAME ASSIGNED BY CONTROLLING AGENCY	BRACKET, EXTRUDED SUPPORT
END ITEM IDENTIFICATION	EA-18G/F/A-18 E AND F AIRCRAFT G
MATERIAL	ALUMINUM ALLOY 7075

SUBSTITUTES & CROSS-REFERENCES 1

74A886604Reference 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)Demilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is PL74A886604?

PL74A886604 is a BRACKET,STRUCTURAL COMPONENT,AIR.

What parts can replace PL74A886604?

There is 1 known substitute for PL74A886604: 74A886604. Substitute compatibility should be verified for your specific system.

What is the NSN for PL74A886604?

PL74A886604 is cataloged in the U.S. Government catalog under NSN 1560-01-710-5177. This indicates validated use in U.S. government and defense supply chains.

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PL74A886604 — BRACKET,STRUCTURAL COMPONENT,AIR

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