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L1700154-049 — RIB,STIFFENER,AIRCRAFT

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

L1700154-049: RIB,STIFFENER,AIRCRAFT.

The RIB,STIFFENER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2219, overall_width: 5.850 INCHES NOMINAL IN, overall_length: 7.680 INCHES NOMINAL IN, aircraft_location: FWD AND AFT-SLAT NUMBER 2,WING PANEL, material_thickness: 0.063 INCHES NOMINAL IN, end_item_identification: B-1 AIRCRAFT. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-632-9502, 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
L1700154-049
NSN: 1560-01-632-9502
FSC: 1560 — Airframe Structural Components
CAGE: 43999 — THE BOEING COMPANY DIV LEGACY AM&M (USA)
SPECIFICATIONS
materialALUMINUM ALLOY 2219
overall_width5.850 INCHES NOMINAL IN
overall_length7.680 INCHES NOMINAL IN
aircraft_locationFWD AND AFT-SLAT NUMBER 2,WING PANEL
material_thickness0.063 INCHES NOMINAL IN
end_item_identificationB-1 AIRCRAFT
aircraft_mission_design_seriesB-1
material_document_and_classificationQQ-A-250/4 FED SPEC SINGLE MATERIAL RESPONSE
part_name_assigned_by_controlling_agencyRIB,AIR LOAD
NSN1560-01-632-9502
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available RIB,STIFFENER,AIRCRAFT TITLE COMPONENT PN L1700154-049 MFR RIB,STIFFENER,AIRCRAFT
KEY FEATURES
•
MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/4 FED SPEC SINGLE MATERIAL RESPONSE
•
MATERIAL THICKNESS: 0.063 INCHES NOMINAL IN
•
AIRCRAFT LOCATION: FWD AND AFT-SLAT NUMBER 2,WING PANEL
•
MATERIAL: ALUMINUM ALLOY 2219
TECHNICAL CHARACTERISTICS
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-250/4 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH7.680 INCHES NOMINAL IN
OVERALL WIDTH5.850 INCHES NOMINAL IN
MATERIAL THICKNESS0.063 INCHES NOMINAL IN
AIRCRAFT LOCATIONFWD AND AFT-SLAT NUMBER 2,WING PANEL
PART NAME ASSIGNED BY CONTROLLING AGENCYRIB,AIR LOAD
END ITEM IDENTIFICATIONB-1 AIRCRAFT
MATERIALALUMINUM ALLOY 2219
AIRCRAFT MISSION DESIGN SERIESB-1
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: Insurance item — stocked against contingency demandDemilitarization required — mutilation + specific procedure
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FREQUENTLY ASKED QUESTIONS
What is L1700154-049?
L1700154-049 is a RIB,STIFFENER,AIRCRAFT.
What is the NSN for L1700154-049?
L1700154-049 is cataloged in the U.S. Government catalog under NSN 1560-01-632-9502. This indicates validated use in U.S. government and defense supply chains.
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✓ PartsTable — the parts reference. Every fact cited to its source.
PartsTable Design LLC · partstable.com
U.S. Government catalog: edition PUBLOGDVD v12.0.0 (OCT 2026), edition date 2026-10-01, retrieved 2026-10-18.
PartsTable commercial catalog: edition Unified commercial catalog snapshot through 2026-09-28, edition date not on file, retrieved 2026-09-28.