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Technical Data Sheet
71091-13 ✓ Verified by PartsTable
· COMPONENT
WHAT YOU NEED TO KNOW
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Confirm exact part number — similar PNs may be different parts
PRODUCT OVERVIEW

The PANEL,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, thickness: 0.250 INCHES NOMINAL IN, overall_width: 6.000 INCHES NOMINAL IN, overall_length: 46.000 INCHES NOMINAL IN, special_features: SURFACE TREATMENT SPECIFICATION ALSO INCLUDES LPS-409., aircraft_location: WING CENTER SECTION TRAILING EDGE. This product is currently in active production with full OEM support.

This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 1560-01-528-1016, 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
71091-13
NSN: 1560-01-528-1016
FSC: 1560
CAGE: 91145 — FLEET READINESS CENTER SOUTHWEST (USA)
SPECIFICATIONS
materialALUMINUM ALLOY 2024
thickness0.250 INCHES NOMINAL IN
overall_width6.000 INCHES NOMINAL IN
overall_length46.000 INCHES NOMINAL IN
special_featuresSURFACE TREATMENT SPECIFICATION ALSO INCLUDES LPS-409.
aircraft_locationWING CENTER SECTION TRAILING EDGE
surface_treatmentPRIMER EPOXY
end_item_identificationC-2A AND E-2A A
side_for_which_designedBOTH SIDES
aircraft_mission_design_seriesC-2A A
relationship_to_similar_equipment71091-11 CAP STRIP REPAIR, FOR WING CENTER SECTION TRAILING EDGE
material_document_and_classificationQQ-A-250/5 ASSN STD SINGLE MATERIAL RESPONSE
NSN1560-01-528-1016
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available PANEL,STRUCTURAL,AIRCRAFT TITLE COMPONENT PN 71091-13 MFR PANEL,STRUCTURAL,AIRCR
KEY FEATURES
MATERIAL: ALUMINUM ALLOY 2024
MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/5 ASSN STD SINGLE MATERIAL RESPONSE
AIRCRAFT LOCATION: WING CENTER SECTION TRAILING EDGE
SURFACE TREATMENT: PRIMER EPOXY
SIDE FOR WHICH DESIGNED: BOTH SIDES
TECHNICAL CHARACTERISTICS (FLIS)
MATERIALALUMINUM ALLOY 2024
SPECIAL FEATURESSURFACE TREATMENT SPECIFICATION ALSO INCLUDES LPS-409.
OVERALL WIDTH6.000 INCHES NOMINAL IN
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-250/5 ASSN STD SINGLE MATERIAL RESPONSE
AIRCRAFT LOCATIONWING CENTER SECTION TRAILING EDGE
END ITEM IDENTIFICATIONC-2A AND E-2A A
SURFACE TREATMENTPRIMER EPOXY
SIDE FOR WHICH DESIGNEDBOTH SIDES
RELATIONSHIP TO SIMILAR EQUIPMENT71091-11 CAP STRIP REPAIR, FOR WING CENTER SECTION TRAILING EDGE
OVERALL LENGTH46.000 INCHES NOMINAL IN
VERIFIED SUBSTITUTES & CROSS-REFERENCES 10
74030Interchangeable
interchangeable cross-reference
interchangeable
71091Interchangeable
interchangeable cross-reference
interchangeable
TE11541Interchangeable
interchangeable cross-reference
interchangeable
7053Interchangeable
interchangeable cross-reference
interchangeable
722803-029Interchangeable
interchangeable cross-reference
interchangeable
04-0302-4609Interchangeable
interchangeable cross-reference
interchangeable
LIFECYCLE
StatusACTIVE
AvailabilityOEM and secondary market
RoHS CompliantEAR99Not HAZMAT
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FREQUENTLY ASKED QUESTIONS
What is 71091-13?
71091-13 is a PANEL,STRUCTURAL,AIRCRAFT.
What parts can replace 71091-13?
There are 10 known substitutes for 71091-13: 74030, 71091, TE11541 and 7 more. Substitute compatibility should be verified for your specific system.
What is the NSN for 71091-13?
71091-13 is cataloged in the Federal Logistics Information System (FLIS) under NSN 1560-01-528-1016. This indicates validated use in U.S. government and defense supply chains.
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