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1560-01-507-4945

Wing Landing Flap

1560015074945 015074945 17P6P5601-3

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

1560-01-507-4945 FLAP,WING LANDING 1560015074945 015074945

Managed by United States
NSN Created on 29 Apr 2003
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
1560-01-507-4945 FLAP,WING LANDING 1560015074945 015074945 1/1
NSN 1560-01-507-4945 (Generic Image) 1/1

1560-01-507-4945 Stock and Availability Marketplace 1560-01-507-4945

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1560-01-507-4945 Related Documents Related Documents 1560-01-507-4945 1+ Documents (More...)

United States (US) 4. 1560-01-507-4945 Marketplace Restrictions Approved Sources Datasheet Management
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RQST NE Restrictions 1560-01-507-4945 DEMIL: D | DEMILI : 7 | CRITICALITY : X | HMIC : P | PMIC : A

1560-01-507-4945 Demil Restrictions 1560-01-507-4945

DEMIL: D | DEMILI: 7 | CRITICALITY: X | HMIC: P | PMIC: A | EDC: A | ADPEC: 0

IUID Required

1560-01-507-4945 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.

1560-01-507-4945 HTS and ScheduleB Import and Export 1560-01-507-4945

1560-01-507-4945 End Users End Users 1560-01-507-4945

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

1560-01-507-4945 Manufacturers Approved Sources 1560-01-507-4945

1560-01-507-4945 Technical Data Datasheet 1560-01-507-4945

Characteristic
Specifications
FIIG
A11500
Aircraft Mission Design Series [CZEK]
C-17A Aircraft
Material [MATT]
Glass Fiber
Part Name Assigned By Controlling Agency [CXCY]
Panel Instl-Structural, Inbd Trailing Edge, Inbd Flap
Special Features [FEAT]
Eff From 17A001-004; C/O 1 Support Assy; 4 Spar Assy; 44 Washers (An96004l); Rivets As Required; 3 Rib Assy; 1 Skin Assy; 1 Spar Assy; 1 Channel; Nha 17P6p5601-1

1560-01-507-4945 Management Data Management Data 1560-01-507-4945

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Oct 2005
Department of the Air Force (DF)
EA
Subscribe
1

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1560-01-507-4945 Freight Data Freight Information 1560-01-507-4945

1560-01-507-4945 has freight characteristics.. 1560-01-507-4945 has a variance between NMFC and UFC when transported by rail and the description should be consulted.