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5120-01-446-4704

Final Drive Assembly Alignment Pin

5120014464704 014464704 GTLLA1088

A special designed pin used in the assembling of the final drive. View more Final Drive Assembly Alignment Pin

5120-01-446-4704 ALIGNMENT PIN,FINAL DRIVE ASSEMBLY 5120014464704 014464704

Managed by United States
NSN Created on 3 Jul 1997
Data Last Changed
January 2023
NATO Update Count
2
NATO Data Quality
5120-01-446-4704 ALIGNMENT PIN,FINAL DRIVE ASSEMBLY 5120014464704 014464704 1/1
NSN 5120-01-446-4704 (Generic Image) 1/1

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5120-01-446-4704 Related Documents Related Documents 5120-01-446-4704 1+ Documents (More...)

-664-9612 Final Drive Assembly Alignment Pin 2C5255G01RNCC: 3 | RNVC: 2 | DAC: B 13 Jul 2017 5120-01-446-4704

5120-01-446-4704 Demil Restrictions 5120-01-446-4704

DEMIL: A | DEMILI: | CRITICALITY: X | HMIC: N | PMIC: A | EDC: A | ADPEC: 0

5120-01-446-4704 is a Final Drive Assembly Alignment Pin that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. This item does not contain a precious metal.

5120-01-446-4704 HTS and ScheduleB Import and Export 5120-01-446-4704

5120-01-446-4704 End Users End Users 5120-01-446-4704

Italy (ZR01)
Effective Date:
1 Jul 1997

5120-01-446-4704 Manufacturers Approved Sources 5120-01-446-4704

5120-01-446-4704 Technical Data Datasheet 5120-01-446-4704

Characteristic
Specifications
FIIG
A23900
End Item Identification [AGAV]
Ch47 C Helicopter

5120-01-446-4704 Related Items NATO Stock Numbers Related to 5120-01-446-4704

5120-01-446-4704 Freight Data Freight Information 5120-01-446-4704

5120-01-446-4704 has freight characteristics managed by Italy.. 5120-01-446-4704 has a variance between NMFC and UFC when transported by rail and the description should be consulted.