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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
January 2023
22

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Restrictions 5120-00-177-9406
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.
Import and Export 5120-00-177-9406
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
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
Approved Sources 5120-00-177-9406
- Part Number
- Manufacturer
- Status
- T101513
- Manufacturer
- 97499 - Bell Textron Inc (Active)
- Primary Buy
- Primary Buy
Datasheet 5120-00-177-9406
- Characteristic
- Specifications
- FIIG
- Specifications
- 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
Management Data 5120-00-177-9406
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Sep 2019
- Department of the Navy (DN)
- EA
- Subscribe
- EA
- MOE
- USC
- Code
- Statement
- Order of Use
- Jump To Code
- Qty Per Assy
- UOM
- Technical Document
- Quantative Expression
- Code
- Department of the Navy (DN)
- N
- V
- Discontinued Without Replacement
- V
Navy
- Cognizance:
- 9Q
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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.