Premium Information is available for this item - Upgrade for $1 a day
1620-01-413-1165
Landing Gear Cylinder And Piston Assembly
1620014131165 014131165 396106-7
The main shock absorption portion of an aircraft landing gear, consisting of the main cylinder and piston and other associated parts. May be with or without axle(s). Excludes LANDING GEAR, FIXED and LANDING GEAR, RETRACTABLE. View more Landing Gear Cylinder And Piston Assembly
January 2023
9
Marketplace 1620-01-413-1165
Request a Quotation from participating marketplace vendors
Related Documents 1620-01-413-1165 2+ Documents (More...)
Request a Quotation from participating marketplace vendors Request Updated Every Day 1620-01-413-1165
RQST NE Updated Every Day 1620-01-413-1165 RQST Updated Every Day 1620-01-413-1165 RQST NE Restrictions
Assembly Account Upgrade 1620-01-413-1165Landing Gear Cylinder And Piston Assembly1620014131165 014131165
Restrictions 1620-01-413-1165
1620-01-413-1165 is a Landing Gear Cylinder And Piston Assembly that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item is a US Munitions List Item and must be mutilated to scrap. This item is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 1620-01-413-1165
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1620-01-413-1165
- United Kingdom (ZK01)
- Effective Date:
- 1 Dec 1996
Approved Sources 1620-01-413-1165
- Part Number
- Manufacturer
- Status
- 396106-7
- Manufacturer
- 98897 - Lockheed Martin Corp (Active)
- Primary Buy
- Primary Buy
Datasheet 1620-01-413-1165
- Characteristic
- Specifications
- FIIG
- Specifications
- A525C0
- End Item Identification [AGAV]
- Lockheed Hercules C-130 Aircraft
Similar Supply Items to 1620-01-413-1165
Freight Information 1620-01-413-1165
1620-01-413-1165 has freight characteristics.. 1620-01-413-1165 has a variance between NMFC and UFC when transported by rail and the description should be consulted.