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1560-01-161-4581
Wing Landing Flap
1560011614581 011614581 16W021-808
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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FLAP,WING LANDING 1 EA NS Request Quotation Updated Every Day 1560-01-161-4581 RQST NE Updated Every
Day 1560-01-161-4581 RQST Updated Every Day 1560-01-161-4581 RQST NE Restrictions 1560-01-161-4581 DEMIL
Restrictions 1560-01-161-4581
1560-01-161-4581 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. 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 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. The precious metals content of this item is unknown.
Import and Export 1560-01-161-4581
- Schedule B
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- HTS Code
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End Users 1560-01-161-4581
- Belgium (ZB01)
- Effective Date:
- 1 Apr 1991
Approved Sources 1560-01-161-4581
- Part Number
- Manufacturer
- Status
- 16W021-808
- Manufacturer
- 81755 - Lockheed Martin Corporation (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-161-4581
- Characteristic
- Specifications
- FIIG
- Specifications
- A11500
- Side For Which Designed [BWJF]
- Right Side
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Freight Information 1560-01-161-4581
1560-01-161-4581 has freight characteristics managed by Belgium.. 1560-01-161-4581 has a variance between NMFC and UFC when transported by rail and the description should be consulted.