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16B5141-138 — WEB,STRUCTURAL COMPONENT,AIRCRAF

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

16B5141-138: WEB,STRUCTURAL COMPONENT,AIRCRAF.

WEB,STRUCTURAL COMPONENT,AIRCRAF. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 26.000 INCHES NOMINAL IN, overall_length: 63.000 INCHES NOMINAL IN, aircraft_location: FUEL SHELF CENTER FUSELAGE, material_thickness: 0.100 INCHES NOMINAL IN, aircraft_station_number: FS279 TO FS341. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-358-4797, 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
16B5141-138
NSN: 1560-01-358-4797
FSC: 1560 — Airframe Structural Components
CAGE: 81755 — LOCKHEED MARTIN CORPORATION DIV LOCKHEED MARTIN AERONAUTICS COMPANY (USA)
SPECIFICATIONS
materialALUMINUM ALLOY 2024
overall_width26.000 INCHES NOMINAL IN
overall_length63.000 INCHES NOMINAL IN
aircraft_locationFUEL SHELF CENTER FUSELAGE
material_thickness0.100 INCHES NOMINAL IN
aircraft_station_numberFS279 TO FS341
side_for_which_designedRIGHT SIDE
aircraft_mission_design_seriesF-16C
material_document_and_classificationQQ-A-250/4-T62 MIL SPEC SINGLE MATERIAL RESPONSE
NSN1560-01-358-4797
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available WEB,STRUCTURAL COMPONENT,AIRCRAF TITLE COMPONENT PN 16B5141-138 MFR WEB,STRUCTURAL COMPONE
KEY FEATURES
•
AIRCRAFT STATION NUMBER: FS279 TO FS341
•
MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/4-T62 MIL SPEC SINGLE MATERIAL RESPONSE
•
MATERIAL THICKNESS: 0.100 INCHES NOMINAL IN
•
AIRCRAFT LOCATION: FUEL SHELF CENTER FUSELAGE
•
MATERIAL: ALUMINUM ALLOY 2024
•
SIDE FOR WHICH DESIGNED: RIGHT SIDE
TECHNICAL CHARACTERISTICS
AIRCRAFT STATION NUMBERFS279 TO FS341
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-250/4-T62 MIL SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH63.000 INCHES NOMINAL IN
OVERALL WIDTH26.000 INCHES NOMINAL IN
MATERIAL THICKNESS0.100 INCHES NOMINAL IN
AIRCRAFT LOCATIONFUEL SHELF CENTER FUSELAGE
MATERIALALUMINUM ALLOY 2024
SIDE FOR WHICH DESIGNEDRIGHT SIDE
AIRCRAFT MISSION DESIGN SERIESF-16C
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 16B5141-138?
16B5141-138 is a WEB,STRUCTURAL COMPONENT,AIRCRAF.
What is the NSN for 16B5141-138?
16B5141-138 is cataloged in the U.S. Government catalog under NSN 1560-01-358-4797. This indicates validated use in U.S. government and defense supply chains.
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