74A231630-1005 — HINGE,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

74A231630-1005: HINGE,AIRCRAFT.

The HINGE,AIRCRAFT is a the manufacturer industrial component. Key specifications include height: 1.731 INCHES MINIMUM AND 1.746 INCHES MAXIMUM IN, material: TITANIUM ALLOY, overall_length: 3.090 INCHES NOMINAL IN, aircraft_location: UPPER-VERTICAL STABILIZER, end_item_identification: F/A18E/F, aircraft_mission_design_series: 7D35/W3. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-504-7783, 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

74A231630-1005

NSN: 1560-01-504-7783
FSC: 1560 — Airframe Structural Components
CAGE: 76823 — NORTHROP GRUMMAN SYSTEMS CORPORATION DBA NORTHROP GRUMMAN IS DIV NORTHROP GRUMMAN AERONAUTICS SYSTEMS (USA)

SPECIFICATIONS

height	1.731 INCHES MINIMUM AND 1.746 INCHES MAXIMUM IN
material	TITANIUM ALLOY
overall_length	3.090 INCHES NOMINAL IN
special_features	DIA OF HINGE HOLES ARE 0.376 IN (AFTER INSTALLATION OF BUSHINGS); 2 UNTHREADED MOUNTING HOLES DIA ARE 0.530 IN, NOMINAL IN
aircraft_location	UPPER-VERTICAL STABILIZER
end_item_identification	F/A18E/F
aircraft_mission_design_series	7D35/W3
criticality_code_justification	AGAV
part_name_assigned_by_controlling_agency	HINGE ASSY,UPPER-VERTICAL STABILIZER
NSN	1560-01-504-7783

COMPONENT DIAGRAM

KEY FEATURES

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

HEIGHT: 1.731 INCHES MINIMUM AND 1.746 INCHES MAXIMUM IN

•

AIRCRAFT LOCATION: UPPER-VERTICAL STABILIZER

•

MATERIAL: TITANIUM ALLOY

TECHNICAL CHARACTERISTICS

CRITICALITY CODE JUSTIFICATION	AGAV
OVERALL LENGTH	3.090 INCHES NOMINAL IN
HEIGHT	1.731 INCHES MINIMUM AND 1.746 INCHES MAXIMUM IN
SPECIAL FEATURES	DIA OF HINGE HOLES ARE 0.376 IN (AFTER INSTALLATION OF BUSHINGS); 2 UNTHREADED MOUNTING HOLES DIA ARE 0.530 IN, NOMINAL IN
AIRCRAFT LOCATION	UPPER-VERTICAL STABILIZER
PART NAME ASSIGNED BY CONTROLLING AGENCY	HINGE ASSY,UPPER-VERTICAL STABILIZER
END ITEM IDENTIFICATION	F/A18E/F
MATERIAL	TITANIUM ALLOY
AIRCRAFT MISSION DESIGN SERIES	7D35/W3

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 1

74A231630Reference document

Same NSN cross-reference

Reference document — Drawing number reference only

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Insurance item — stocked against contingency demandDemilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 74A231630-1005?

74A231630-1005 is a HINGE,AIRCRAFT.

What parts can replace 74A231630-1005?

There is 1 known substitute for 74A231630-1005: 74A231630. Substitute compatibility should be verified for your specific system.

What is the NSN for 74A231630-1005?

74A231630-1005 is cataloged in the U.S. Government catalog under NSN 1560-01-504-7783. This indicates validated use in U.S. government and defense supply chains.

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74A231630-1005 — HINGE,AIRCRAFT

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