Premium Information is available for this item - Upgrade for $1 a day
1620-01-429-2221
Landing Gear Axle
1620014292221 014292221 2010104-1
A bar or spindle, on which or with which, an aircraft landing gear wheel rotates. View more Landing Gear Axle
January 2023
10

Marketplace 1620-01-429-2221
Request a Quotation from participating marketplace vendors
Related Documents 1620-01-429-2221 2+ Documents (More...)
United States (US) 4. 1620-01-429-2221 Marketplace Restrictions Approved Sources Datasheet Management
AXLE,LANDING GEAR RQST NS Request Quotation Updated Every Day 1620-01-429-2221 RQST NE Updated Every
Landing Gear Axle 1620014292221 014292221 for $1 a day Upgrade your Account Upgrade 1620-01-429
-2221Landing Gear Axle1620014292221 014292221 2010104 Request a Quotation from participating marketplace
Restrictions 1620-01-429-2221
1620-01-429-2221 is a Landing Gear Axle 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 1620-01-429-2221
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1620-01-429-2221
- Taiwan, Province of China (YE01)
- Effective Date:
- 1 Feb 2015
Approved Sources 1620-01-429-2221
- Part Number
- Manufacturer
- Status
- 2010104-1
- Manufacturer
- 6K4C8 - Goodrich Corporation (Active)
- Primary Buy
- Primary Buy
- 2010104-1
- 17576 - Goodrich Corp (Replaced)
- Original Design
- Original Design
NATO Stock Numbers Related to 1620-01-429-2221
Freight Information 1620-01-429-2221
1620-01-429-2221 has freight characteristics managed by the Department of Energy (DOE).. 1620-01-429-2221 has a variance between NMFC and UFC when transported by rail and the description should be consulted.