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1620-01-424-5986
Landing Gear Torque Arm Assembly
1620014245986 014245986 2010107-106
A landing gear component consisting of an arm and bushing. Designed to connect the inner and outer cylinder of an aircraft landing gear and retain the wheel in an alignment. View more Landing Gear Torque Arm Assembly
January 2023
9
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Related Documents 1620-01-424-5986 1+ Documents (More...)
United States (US) 4. 1620-01-424-5986 Marketplace Restrictions Approved Sources Datasheet Management
ARM ASSEMBLY,TORQUE,LANDING GEAR RQST NS Request Quotation Updated Every Day 1620-01-424-5986 RQST
Restrictions 1620-01-424-5986
1620-01-424-5986 is a Landing Gear Torque Arm Assembly 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.
Import and Export 1620-01-424-5986
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1620-01-424-5986
- Taiwan, Province of China (YE01)
- Effective Date:
- 1 Feb 2015
Approved Sources 1620-01-424-5986
- Part Number
- Manufacturer
- Status
- 2010107-106
- Manufacturer
- 6K4C8 - Goodrich Corporation (Active)
- Primary Buy
- Primary Buy
- 2010107-106
- 17576 - Goodrich Corp (Replaced)
- Original Design
- Original Design
Datasheet 1620-01-424-5986
- Characteristic
- Specifications
- FIIG
- Specifications
- A52500
- End Item Identification [AGAV]
- Pacer Dawn
- Special Features [FEAT]
- Upper Torque Arm-Rh 1;Bushing 6;Fitting 4
NATO Stock Numbers Related to 1620-01-424-5986
Freight Information 1620-01-424-5986
1620-01-424-5986 has freight characteristics managed by the Department of Energy (DOE).. 1620-01-424-5986 has a variance between NMFC and UFC when transported by rail and the description should be consulted.