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75-11455-9 — FORMER,AIRCRAFT

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

75-11455-9: FORMER,AIRCRAFT.

The FORMER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7050, overall_width: 17.900 INCHES MINIMUM AND 18.100 INCHES MAXIMUM IN, overall_length: 22.960 INCHES MINIMUM AND 23.040 INCHES MAXIMUM IN, special_features: NHA FORMER-NACELLE, FUSELAGE STATION 305.50, aircraft_location: FUSELAGE STATION 305.50, material_thickness: 0.960 INCHES MINIMUM AND 1.040 INCHES MAXIMUM IN. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-497-7601, 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
75-11455-9
NSN: 1560-01-497-7601
FSC: 1560 — Airframe Structural Components
CAGE: 9U679 — CPI AEROSTRUCTURES INC (USA)
SPECIFICATIONS
materialALUMINUM ALLOY 7050
overall_width17.900 INCHES MINIMUM AND 18.100 INCHES MAXIMUM IN
overall_length22.960 INCHES MINIMUM AND 23.040 INCHES MAXIMUM IN
special_featuresNHA FORMER-NACELLE, FUSELAGE STATION 305.50
aircraft_locationFUSELAGE STATION 305.50
material_thickness0.960 INCHES MINIMUM AND 1.040 INCHES MAXIMUM IN
aircraft_mission_design_seriesT-38C
material_document_and_classificationAMS 4050 ASSN STD SINGLE MATERIAL RESPONSE
NSN1560-01-497-7601
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available FORMER,AIRCRAFT TITLE COMPONENT PN 75-11455-9 MFR FORMER,AIRCRAFT
KEY FEATURES
•
MATERIAL DOCUMENT AND CLASSIFICATION: AMS 4050 ASSN STD SINGLE MATERIAL RESPONSE
•
MATERIAL THICKNESS: 0.960 INCHES MINIMUM AND 1.040 INCHES MAXIMUM IN
•
AIRCRAFT LOCATION: FUSELAGE STATION 305.50
•
MATERIAL: ALUMINUM ALLOY 7050
•
AIRCRAFT MISSION DESIGN SERIES: T-38C
TECHNICAL CHARACTERISTICS
MATERIAL DOCUMENT AND CLASSIFICATIONAMS 4050 ASSN STD SINGLE MATERIAL RESPONSE
OVERALL LENGTH22.960 INCHES MINIMUM AND 23.040 INCHES MAXIMUM IN
OVERALL WIDTH17.900 INCHES MINIMUM AND 18.100 INCHES MAXIMUM IN
MATERIAL THICKNESS0.960 INCHES MINIMUM AND 1.040 INCHES MAXIMUM IN
SPECIAL FEATURESNHA FORMER-NACELLE, FUSELAGE STATION 305.50
AIRCRAFT LOCATIONFUSELAGE STATION 305.50
MATERIALALUMINUM ALLOY 7050
AIRCRAFT MISSION DESIGN SERIEST-38C
SUBSTITUTES & CROSS-REFERENCES 1
75-11455Reference document
Same NSN cross-reference
Reference document — Drawing number reference only
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 75-11455-9?
75-11455-9 is a FORMER,AIRCRAFT.
What parts can replace 75-11455-9?
There is 1 known substitute for 75-11455-9: 75-11455. Substitute compatibility should be verified for your specific system.
What is the NSN for 75-11455-9?
75-11455-9 is cataloged in the U.S. Government catalog under NSN 1560-01-497-7601. 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.