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1560-01-656-5149
Wing Landing Flap
1560016565149 016565149 5HU01100-101
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
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January 2023
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RQST NE Restrictions 1560-01-656-5149 DEMIL: D | DEMILI : 1 | CRITICALITY : F | HMIC : P | PMIC : A
Restrictions 1560-01-656-5149
1560-01-656-5149 is a Wing Landing Flap that is an aviation critical safety item or flight safety critical aircraft part. Demilitarization of this item has been confirmed and is not currently subject to changes. 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 1560-01-656-5149
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-656-5149
- US Air Force (FLL4)
- Effective Date:
- 1 Jul 2016
Approved Sources 1560-01-656-5149
- Part Number
- Manufacturer
- Status
- 5HU01100-101
- Manufacturer
- 98897 - Lockheed Martin Corp (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-656-5149
- Characteristic
- Specifications
- FIIG
- Specifications
- A11500
- Aircraft Mission Design Series [CZEK]
- F-22 Aircraft
- Part Name Assigned By Controlling Agency [CXCY]
- Flap,Wing Landing
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Freight Information 1560-01-656-5149
1560-01-656-5149 has freight characteristics.. 1560-01-656-5149 has a variance between NMFC and UFC when transported by rail and the description should be consulted.