53-11041-44 — FORMER,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

53-11041-44: FORMER,AIRCRAFT.

The FORMER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: TITANIUM ALLOY, overall_width: 3.350 INCHES NOMINAL IN, overall_length: 14.650 INCHES NOMINAL IN, special_features: DO NOT USE CADMIUM PLATED TOOLS ON THIS ITEM, aircraft_location: WEB ASSEMBLY,SPEED BRAKE CLOSURE FORWARD, material_thickness: 0.080 INCHES NOMINAL IN. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-113-7017, 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

53-11041-44

NSN: 1560-01-113-7017
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)

SPECIFICATIONS

material	TITANIUM ALLOY
overall_width	3.350 INCHES NOMINAL IN
overall_length	14.650 INCHES NOMINAL IN
special_features	DO NOT USE CADMIUM PLATED TOOLS ON THIS ITEM
aircraft_location	WEB ASSEMBLY,SPEED BRAKE CLOSURE FORWARD
material_thickness	0.080 INCHES NOMINAL IN
side_for_which_designed	RIGHT SIDE
aircraft_mission_design_series	F-4E
criticality_code_justification	FEAT
material_document_and_classification	MIL-T-7046,TYPE 3,COND ANNEALED,COMP C MIL SPEC SINGLE MATERIAL RESPONSE
NSN	1560-01-113-7017

COMPONENT DIAGRAM

KEY FEATURES

•

CRITICALITY CODE JUSTIFICATION: FEAT

•

MATERIAL DOCUMENT AND CLASSIFICATION: MIL-T-7046,TYPE 3,COND ANNEALED,COMP C MIL SPEC SINGLE MATERIAL RESPONSE

•

MATERIAL THICKNESS: 0.080 INCHES NOMINAL IN

•

AIRCRAFT LOCATION: WEB ASSEMBLY,SPEED BRAKE CLOSURE FORWARD

•

MATERIAL: TITANIUM ALLOY

TECHNICAL CHARACTERISTICS

CRITICALITY CODE JUSTIFICATION	FEAT
MATERIAL DOCUMENT AND CLASSIFICATION	MIL-T-7046,TYPE 3,COND ANNEALED,COMP C MIL SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH	14.650 INCHES NOMINAL IN
OVERALL WIDTH	3.350 INCHES NOMINAL IN
MATERIAL THICKNESS	0.080 INCHES NOMINAL IN
SPECIAL FEATURES	DO NOT USE CADMIUM PLATED TOOLS ON THIS ITEM
AIRCRAFT LOCATION	WEB ASSEMBLY,SPEED BRAKE CLOSURE FORWARD
MATERIAL	TITANIUM ALLOY
SIDE FOR WHICH DESIGNED	RIGHT SIDE
AIRCRAFT MISSION DESIGN SERIES	F-4E

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: Normally procured from the manufacturer (OEM)Demilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 53-11041-44?

53-11041-44 is a FORMER,AIRCRAFT.

What is the NSN for 53-11041-44?

53-11041-44 is cataloged in the U.S. Government catalog under NSN 1560-01-113-7017. This indicates validated use in U.S. government and defense supply chains.

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