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1615-01-493-9906
Rotary Wing Blade
1615014939906 014939906 114R1702-40 1141702-40
An airfoil that is a component of a rotary wing. View more Rotary Wing Blade
January 2023
2
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Related Documents 1615-01-493-9906 2+ Documents (More...)
United States (US) 4. 1615-01-493-9906 Marketplace Restrictions Approved Sources Datasheet Management
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Rotary Wing Blade 1615014939906 014939906 Upgrade your Account Upgrade 1615-01-493-9906Rotary Wing
Blade1615014939906 014939906 114R1702-40 1141702 NumberManufacturerStatus114R1702-40 77272 - The Boeing
Restrictions 1615-01-493-9906
1615-01-493-9906 is a Rotary Wing Blade that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item has been confirmed as a Critical Munitions List Item or a Sensitive Commerce Control List Item and cannot be in the possession of any party anywhere in the World who is not an authorized NATO Government. Any other possessor of this item should mutilate it now as possession violates international and local laws. This item is a confirmed Commerce Control List Item (CCLI). This item is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 1615-01-493-9906
- Schedule B
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- HTS Code
- Subscribe to View HTS Code
End Users 1615-01-493-9906
- United Kingdom (ZK01)
- Effective Date:
- 1 Jan 2002
Approved Sources 1615-01-493-9906
- Part Number
- Manufacturer
- Status
- 114R1702-40
- Manufacturer
- 77272 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
- 1141702-40
- 77272 - The Boeing Company (Active)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 1615-01-493-9906
- Characteristic
- Specifications
- FIIG
- Specifications
- A504T0
- Special Features [FEAT]
- Rotor Blade-Deice
- End Item Identification [AGAV]
- Ch-47D, Forward Rotor
NATO Stock Numbers Related to 1615-01-493-9906
Freight Information 1615-01-493-9906
1615-01-493-9906 has freight characteristics.. 1615-01-493-9906 has a variance between NMFC and UFC when transported by rail and the description should be consulted.