3-12391-4 — FUSELAGE SECTION

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

3-12391-4: FUSELAGE SECTION.

The FUSELAGE SECTION is a the manufacturer industrial component. Key specifications include material: NICKEL ALLOY, overall_width: 17.000 INCHES NOMINAL IN, overall_length: 20.500 INCHES NOMINAL IN, aircraft_location: AFT FUSELAGE, material_thickness: 0.030 INCHES NOMINAL IN, aircraft_station_number: FS483.00 TO FS582.09. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-486-6677, 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

3-12391-4

NSN: 1560-01-486-6677
FSC: 1560 — Airframe Structural Components
CAGE: 76823 — NORTHROP GRUMMAN SYSTEMS CORPORATION DBA NORTHROP GRUMMAN IS DIV NORTHROP GRUMMAN AERONAUTICS SYSTEMS (USA)

SPECIFICATIONS

material	NICKEL ALLOY
overall_width	17.000 INCHES NOMINAL IN
overall_length	20.500 INCHES NOMINAL IN
special_features	MANUFACTURED SUGGEST NAME: (EJECTOR-AFT FUSELAGE); SHEET HASTEALLOY; SAME AS -3 EXCEPT WHERE ECN 01A0449 IS APPLIED USING 3 SEPERATE -21 SHROUD COMPONENTS; C/O -5 STIFFENERS AND -21 SHROUD
aircraft_location	AFT FUSELAGE
material_thickness	0.030 INCHES NOMINAL IN
aircraft_station_number	FS483.00 TO FS582.09
aircraft_mission_design_series	T-38
material_document_and_classification	AMS5536 ASSN STD SINGLE MATERIAL RESPONSE
NSN	1560-01-486-6677

COMPONENT DIAGRAM

KEY FEATURES

•

AIRCRAFT STATION NUMBER: FS483.00 TO FS582.09

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS5536 ASSN STD SINGLE MATERIAL RESPONSE

•

MATERIAL THICKNESS: 0.030 INCHES NOMINAL IN

•

AIRCRAFT LOCATION: AFT FUSELAGE

•

MATERIAL: NICKEL ALLOY

TECHNICAL CHARACTERISTICS

AIRCRAFT STATION NUMBER	FS483.00 TO FS582.09
MATERIAL DOCUMENT AND CLASSIFICATION	AMS5536 ASSN STD SINGLE MATERIAL RESPONSE
OVERALL LENGTH	20.500 INCHES NOMINAL IN
OVERALL WIDTH	17.000 INCHES NOMINAL IN
MATERIAL THICKNESS	0.030 INCHES NOMINAL IN
SPECIAL FEATURES	MANUFACTURED SUGGEST NAME: (EJECTOR-AFT FUSELAGE); SHEET HASTEALLOY; SAME AS -3 EXCEPT WHERE ECN 01A0449 IS APPLIED USING 3 SEPERATE -21 SHROUD COMPONENTS; C/O -5 STIFFENERS AND -21 SHROUD
AIRCRAFT LOCATION	AFT FUSELAGE
MATERIAL	NICKEL ALLOY
AIRCRAFT MISSION DESIGN SERIES	T-38

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 — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 3-12391-4?

3-12391-4 is a FUSELAGE SECTION.

What is the NSN for 3-12391-4?

3-12391-4 is cataloged in the U.S. Government catalog under NSN 1560-01-486-6677. This indicates validated use in U.S. government and defense supply chains.

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3-12391-4 — FUSELAGE SECTION

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