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75-11452 — FORMER,AIRCRAFT

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

75-11452: FORMER,AIRCRAFT.

The FORMER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7050, overall_width: 17.100 INCHES MINIMUM AND 17.300 INCHES MAXIMUM IN, overall_length: 24.800 INCHES MINIMUM AND 25.000 INCHES MAXIMUM IN, special_features: NHA FORMER, NACELLE-FUSELAGE STATION 284.00 T-38 IMPROVED INLET, aircraft_location: FUSELAGE STATION 284.00, material_thickness: 1.400 INCHES MINIMUM AND 1.600 INCHES MAXIMUM IN. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-497-7643, 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
75-11452
NSN: 1560-01-497-7643
NIINs: 014977643, 014977649
FSC: 1560 — Airframe Structural Components
CAGE: 76823 — NORTHROP GRUMMAN SYSTEMS CORPORATION DBA NORTHROP GRUMMAN IS DIV NORTHROP GRUMMAN AERONAUTICS SYSTEMS (USA)
SPECIFICATIONS
materialALUMINUM ALLOY 7050
overall_width17.100 INCHES MINIMUM AND 17.300 INCHES MAXIMUM IN
overall_length24.800 INCHES MINIMUM AND 25.000 INCHES MAXIMUM IN
special_featuresNHA FORMER, NACELLE-FUSELAGE STATION 284.00 T-38 IMPROVED INLET
aircraft_locationFUSELAGE STATION 284.00
material_thickness1.400 INCHES MINIMUM AND 1.600 INCHES MAXIMUM IN
aircraft_mission_design_seriesT-38C AND T-38N
NSN1560-01-497-7643
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available FORMER,AIRCRAFT TITLE COMPONENT PN 75-11452 MFR FORMER,AIRCRAFT
KEY FEATURES
•
MATERIAL THICKNESS: 1.400 INCHES MINIMUM AND 1.600 INCHES MAXIMUM IN
•
AIRCRAFT LOCATION: FUSELAGE STATION 284.00
•
MATERIAL: ALUMINUM ALLOY 7050
•
AIRCRAFT MISSION DESIGN SERIES: T-38C AND T-38N
TECHNICAL CHARACTERISTICS
OVERALL LENGTH24.800 INCHES MINIMUM AND 25.000 INCHES MAXIMUM IN
OVERALL WIDTH17.100 INCHES MINIMUM AND 17.300 INCHES MAXIMUM IN
MATERIAL THICKNESS1.400 INCHES MINIMUM AND 1.600 INCHES MAXIMUM IN
SPECIAL FEATURESNHA FORMER, NACELLE-FUSELAGE STATION 284.00 T-38 IMPROVED INLET
AIRCRAFT LOCATIONFUSELAGE STATION 284.00
MATERIALALUMINUM ALLOY 7050
AIRCRAFT MISSION DESIGN SERIEST-38C AND T-38N
SUBSTITUTES & CROSS-REFERENCES 1
75-11452-1Reference document
Same NSN cross-reference
Reference document — Advisory reference — outside the item-of-supply concept
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 75-11452?
75-11452 is a FORMER,AIRCRAFT.
What parts can replace 75-11452?
There is 1 known substitute for 75-11452: 75-11452-1. Substitute compatibility should be verified for your specific system.
What is the NSN for 75-11452?
75-11452 is cataloged in the U.S. Government catalog under NSN 1560-01-497-7643. 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.