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1560-01-509-5200

Wing Landing Flap

1560015095200 015095200 17N6P0639-546

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

1560-01-509-5200 FLAP,WING LANDING 1560015095200 015095200

Managed by United States
NSN Created on 24 Jun 2003
Data Last Changed
January 2023
NATO Update Count
2
NATO Data Quality
1560-01-509-5200 FLAP,WING LANDING 1560015095200 015095200 1/1
NSN 1560-01-509-5200 (Generic Image) 1/1

1560-01-509-5200 Stock and Availability Marketplace 1560-01-509-5200

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United States (US) 4. 1560-01-509-5200 Marketplace Restrictions Approved Sources Datasheet Management
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1560-01-509-5200 Demil Restrictions 1560-01-509-5200

DEMIL: Q | DEMILI: 3 | CRITICALITY: X | HMIC: P | PMIC: A | EDC: A | ADPEC: 0

IUID Required

1560-01-509-5200 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 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 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.

1560-01-509-5200 HTS and ScheduleB Import and Export 1560-01-509-5200

1560-01-509-5200 End Users End Users 1560-01-509-5200

US Air Force (FBB4)
Effective Date:
1 Jun 2003

1560-01-509-5200 Manufacturers Approved Sources 1560-01-509-5200

1560-01-509-5200 Technical Data Datasheet 1560-01-509-5200

Characteristic
Specifications
FIIG
A11500
Aircraft Location [CZDJ]
Wing Inboard
Aircraft Mission Design Series [CZEK]
C-17A Aircraft
Material [MATT]
Glass Fiber
Part Name Assigned By Controlling Agency [CXCY]
Structural Assembly, Outboard Flap

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1560-01-509-5200 Freight Data Freight Information 1560-01-509-5200

1560-01-509-5200 has freight characteristics.. 1560-01-509-5200 has a variance between NMFC and UFC when transported by rail and the description should be consulted.