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527-14791-1 — RIB,AIRFOIL

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

527-14791-1: RIB,AIRFOIL.

The RIB,AIRFOIL is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 6.500 INCHES NOMINAL IN, overall_length: 15.000 INCHES NOMINAL IN, aircraft_location: FORE FLAP, material_thickness: 0.050 INCHES NOMINAL IN, end_item_identification: KC-135 ACFT. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-571-1002, 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
527-14791-1
NSN: 1560-01-571-1002
FSC: 1560 — Airframe Structural Components
CAGE: 82918 — THE BOEING COMPANY DIV LEGACY WICHITA (USA)
SPECIFICATIONS
materialALUMINUM ALLOY 2024
overall_width6.500 INCHES NOMINAL IN
overall_length15.000 INCHES NOMINAL IN
special_featuresNHA 65-7360; DIM. ARE STOCKSIZE MATL; HEAT TREAT TO T42 PER BAC5602; AL2024 CLAD ALUM SH; FINISH F-2.16; 527-14791-2 OPPOSITE
aircraft_locationFORE FLAP
material_thickness0.050 INCHES NOMINAL IN
end_item_identificationKC-135 ACFT
aircraft_mission_design_seriesKC-135 ACFT
material_document_and_classificationQQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE
part_name_assigned_by_controlling_agencyRIB-FORE FLAP, KC-135
NSN1560-01-571-1002
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available RIB,AIRFOIL TITLE COMPONENT PN 527-14791-1 MFR RIB,AIRFOIL
KEY FEATURES
•
MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE
•
MATERIAL THICKNESS: 0.050 INCHES NOMINAL IN
•
AIRCRAFT LOCATION: FORE FLAP
TECHNICAL CHARACTERISTICS
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH15.000 INCHES NOMINAL IN
OVERALL WIDTH6.500 INCHES NOMINAL IN
MATERIAL THICKNESS0.050 INCHES NOMINAL IN
SPECIAL FEATURESNHA 65-7360; DIM. ARE STOCKSIZE MATL; HEAT TREAT TO T42 PER BAC5602; AL2024 CLAD ALUM SH; FINISH F-2.16; 527-14791-2 OPPOSITE
AIRCRAFT LOCATIONFORE FLAP
PART NAME ASSIGNED BY CONTROLLING AGENCYRIB-FORE FLAP, KC-135
END ITEM IDENTIFICATIONKC-135 ACFT
MATERIALALUMINUM ALLOY 2024
AIRCRAFT MISSION DESIGN SERIESKC-135 ACFT
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 — critical (Q)
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FREQUENTLY ASKED QUESTIONS
What is 527-14791-1?
527-14791-1 is a RIB,AIRFOIL.
What is the NSN for 527-14791-1?
527-14791-1 is cataloged in the U.S. Government catalog under NSN 1560-01-571-1002. 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.