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1560-01-510-2885

Wing Landing Flap

1560015102885 015102885 17N6P0635-566

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

1560-01-510-2885 FLAP,WING LANDING 1560015102885 015102885

Managed by United States
NSN Created on 16 Jul 2003
Data Last Changed
January 2023
NATO Update Count
2
NATO Data Quality
1560-01-510-2885 FLAP,WING LANDING 1560015102885 015102885 1/1
NSN 1560-01-510-2885 (Generic Image) 1/1

1560-01-510-2885 Stock and Availability Marketplace 1560-01-510-2885

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United States (US) 4. 1560-01-510-2885 Marketplace Restrictions Approved Sources Datasheet Management
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1560-01-510-2885 Demil Restrictions 1560-01-510-2885

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

IUID Required

1560-01-510-2885 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.

1560-01-510-2885 HTS and ScheduleB Import and Export 1560-01-510-2885

1560-01-510-2885 End Users End Users 1560-01-510-2885

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

1560-01-510-2885 Manufacturers Approved Sources 1560-01-510-2885

1560-01-510-2885 Technical Data Datasheet 1560-01-510-2885

Characteristic
Specifications
FIIG
A11500
Aircraft Location [CZDJ]
Wing Inboard
Aircraft Mission Design Series [CZEK]
C-17A
Material [MATT]
Glass Fiber
Part Name Assigned By Controlling Agency [CXCY]
Structural Assy,Inboard Flap
Special Features [FEAT]
Nha 17N6p0624-514; C/0 1 Fairing Inst

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1560-01-510-2885 Freight Data Freight Information 1560-01-510-2885

1560-01-510-2885 has freight characteristics.. 1560-01-510-2885 has a variance between NMFC and UFC when transported by rail and the description should be consulted.