75-11476 — SUPPORT,STRUCTURAL COMPONENT,AIR

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

75-11476: SUPPORT,STRUCTURAL COMPONENT,AIR.

SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 59.900 INCHES MINIMUM AND 60.100 INCHES MAXIMUM IN, overall_length: 2.400 INCHES MINIMUM AND 2.600 INCHES MAXIMUM IN, special_features: NHA SPLICE, INLET DUCT-UPPER, LEADING EDGE TO F.S. 325.00, aircraft_location: INLET DUCT, material_thickness: 0.040 INCHES MINIMUM AND 0.060 INCHES MAXIMUM IN.

This part is cataloged in the U.S. Government catalog under NSN 1560-01-497-7693, 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

75-11476

NSN: 1560-01-497-7693
NIINs: 014977693, 014977697
FSC: 1560 — Airframe Structural Components
CAGE: 76823 — NORTHROP GRUMMAN SYSTEMS CORPORATION DBA NORTHROP GRUMMAN IS DIV NORTHROP GRUMMAN AERONAUTICS SYSTEMS (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 7075
overall_width	59.900 INCHES MINIMUM AND 60.100 INCHES MAXIMUM IN
overall_length	2.400 INCHES MINIMUM AND 2.600 INCHES MAXIMUM IN
special_features	NHA SPLICE, INLET DUCT-UPPER, LEADING EDGE TO F.S. 325.00
aircraft_location	INLET DUCT
material_thickness	0.040 INCHES MINIMUM AND 0.060 INCHES MAXIMUM IN
aircraft_mission_design_series	T-38C
material_document_and_classification	QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE
NSN	1560-01-497-7693

COMPONENT DIAGRAM

KEY FEATURES

•

MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE

•

MATERIAL THICKNESS: 0.040 INCHES MINIMUM AND 0.060 INCHES MAXIMUM IN

•

AIRCRAFT LOCATION: INLET DUCT

•

MATERIAL: ALUMINUM ALLOY 7075

•

AIRCRAFT MISSION DESIGN SERIES: T-38C

TECHNICAL CHARACTERISTICS

MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH	2.400 INCHES MINIMUM AND 2.600 INCHES MAXIMUM IN
OVERALL WIDTH	59.900 INCHES MINIMUM AND 60.100 INCHES MAXIMUM IN
MATERIAL THICKNESS	0.040 INCHES MINIMUM AND 0.060 INCHES MAXIMUM IN
SPECIAL FEATURES	SPLICE, INLET DUCT-UPPER, LEADING EDGE TO F.S. 325.00
AIRCRAFT LOCATION	INLET DUCT
MATERIAL	ALUMINUM ALLOY 7075
AIRCRAFT MISSION DESIGN SERIES	T-38C

SUBSTITUTES & CROSS-REFERENCES 1

75-11476-4Reference document

Same NSN cross-reference

Reference document — Secondary reference

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Normally procured from the manufacturer (OEM)Demilitarization required — critical (Q)

Ready to buy 75-11476?

Compare prices from verified sellers on eBay

Buy on eBay →

As an eBay Partner, PartsTable may earn a commission. Your price is not affected.

FREQUENTLY ASKED QUESTIONS

What is 75-11476?

75-11476 is a SUPPORT,STRUCTURAL COMPONENT,AIR.

What parts can replace 75-11476?

There is 1 known substitute for 75-11476: 75-11476-4. Substitute compatibility should be verified for your specific system.

What is the NSN for 75-11476?

75-11476 is cataloged in the U.S. Government catalog under NSN 1560-01-497-7693. This indicates validated use in U.S. government and defense supply chains.

Community Feedback

75-11476 — SUPPORT,STRUCTURAL COMPONENT,AIR

Request a Quote — 75-11476