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1560-01-642-4621
Wing Landing Flap
1560016424621 016424621 74G180003-1405
A movable airfoil, whether hinged, pivoted or mounted on tracks, forming part of the leading or trailing edge of a wing of an aircraft. It is designed for the specific purpose of lowering the landing speed by varying the effective camber and may be used in accelerated takeoffs and improved climbs. Excludes leading edge devices that prevent stalls by ducting air over the top of a wing through extended slats. Excludes SLAT,AIRCRAFT. View more Wing Landing Flap
January 2023
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United States (US) 4. 1560-01-642-4621 Marketplace Restrictions Approved Sources Datasheet Management
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Restrictions 1560-01-642-4621
1560-01-642-4621 is a Wing Landing Flap that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. The DCMO has forced the Demilization requirements for this item as the ICP has not collaborated. This item is a US Munitions List or Commerce Control List Item which must be destroyed to prevent restoration or repair. Only authorized parties may possess this item. This item may be hazardous as it is in a Federal Supply Class for potentially hazardous items. A MSDS should be available from the supplier for the end user to evaluate any hazards. This item does not contain a precious metal.
Import and Export 1560-01-642-4621
- Schedule B
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- HTS Code
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End Users 1560-01-642-4621
- Spain (YB01)
- Effective Date:
- 1 Feb 2015
Approved Sources 1560-01-642-4621
- Part Number
- Manufacturer
- Status
- 74G180003-1405
- Manufacturer
- 76301 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-642-4621
- Characteristic
- Specifications
- FIIG
- Specifications
- A11500
- End Item Identification [AGAV]
- F/A-18 Aircraft
- Part Name Assigned By Controlling Agency [CXCY]
- Trailing Edge Flap Assembly, Lh
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Freight Information 1560-01-642-4621
1560-01-642-4621 has freight characteristics.. 1560-01-642-4621 has a variance between NMFC and UFC when transported by rail and the description should be consulted.