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5120-00-177-9406

Face Spanner Wrench Socket

5120001779406 001779406 T101513

An item designed to be driven by an external or internal drive. It has a face type spanner end. View more Face Spanner Wrench Socket

5120-00-177-9406 SOCKET,WRENCH,FACE SPANNER 5120001779406 001779406

Managed by United States
NSN Created on 12 Feb 1969
Data Last Changed
January 2023
NATO Update Count
22
NATO Data Quality
STYL Style 175 for 5120-00-177-9406 1/1
NSN 5120-00-177-9406 (Identification) 1/1

5120-00-177-9406 Stock and Availability Marketplace 5120-00-177-9406

5120-00-177-9406 Related Documents Related Documents 5120-00-177-9406 1+ Documents (More...)

T101513 SOCKET,WRENCH,FACE SPANNER 1 EA NS Request Quotation Subscribe to View Vendor Details... 5120
RQST NE Updated Every Day 5120-00-177-9406 RQST Updated Every Day 5120-00-177-9406 RQST NE Related Documents
5120-00-177-9406 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-51/fsc-5120/us 5120-00-177-9406

5120-00-177-9406 Demil Restrictions 5120-00-177-9406

DEMIL: A | DEMILI: 1 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: | ADPEC:

5120-00-177-9406 is a Face Spanner Wrench Socket that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. 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.

5120-00-177-9406 HTS and ScheduleB Import and Export 5120-00-177-9406

5120-00-177-9406 End Users End Users 5120-00-177-9406

NASA (G751)
Effective Date:
1 Apr 1991
US Navy (N9QG)
Effective Date:
1 Apr 1991
Supplementary Collaborators:
KE
Austria (WB01)
Effective Date:
1 Feb 2005
Slovenia (WL01)
Effective Date:
1 Nov 2008
Bulgaria (WU01)
Effective Date:
1 Oct 2002
Brazil (YA01)
Effective Date:
1 Dec 1999
Australia (ZA01)
Effective Date:
1 Apr 1991
Canada (ZC01)
Effective Date:
1 Apr 1991
Republic of Korea (ZH01)
Effective Date:
1 Apr 1998
Greece (ZU01)
Effective Date:
1 Apr 1991
Turkey (ZW01)
Effective Date:
1 Nov 2005

5120-00-177-9406 Manufacturers Approved Sources 5120-00-177-9406

5120-00-177-9406 Technical Data Datasheet 5120-00-177-9406

Characteristic
Specifications
FIIG
A102A0
Material [MATT]
Steel Overall
Style Designator [STYL]
Lug
Overall Length [ABHP]
0.750 Inches Nominal
Outside Diameter [ABKV]
1.250 Inches Nominal
Opening Diameter [AGNJ]
1.000 Inches Nominal
Lug Width [AHMM]
0.220 Inches Nominal
Lug Length [AJAQ]
0.250 Inches Nominal
Angle Between Lugs [CTLN]
60.0 Degrees Nominal
Drive Surface Size [ATNC]
0.500 Inches Nominal Single End
Drive End Shape [CTCT]
Square Single End Internal
End Item Identification [AGAV]
Bell Helicopter
Functional Description [FTLD]
Used To Install/Remove No. 206-040-421 Nut Onto/From No. 206-040-407 Tail Rotor Output Shaft

5120-00-177-9406 Management Data Management Data 5120-00-177-9406

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Sep 2019
Department of the Navy (DN)
EA
Subscribe
MOE
USC
Code
Statement
Order of Use
Jump To Code
Qty Per Assy
UOM
Technical Document
Quantative Expression
Department of the Navy (DN)
N
V
Discontinued Without Replacement

Navy Navy

Cognizance:
9Q

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5120-00-177-9406 Freight Data Freight Information 5120-00-177-9406

5120-00-177-9406 has freight characteristics.. 5120-00-177-9406 has a variance between NMFC and UFC when transported by rail and the description should be consulted.