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1560-01-590-7369

Wing Landing Flap

1560015907369 015907369 17N6P0639-566

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

Managed by United States

NSN Created on 18 Dec 2010

Data Last Changed
January 2023

NATO Update Count
2

NATO Data Quality

1560-01-590-7369 FLAP,WING LANDING 1560015907369 015907369 1/1 — NSN 1560-01-590-7369 (Generic Image) 1/1

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1560-01-590-7369 RQST NE

Restrictions 1560-01-590-7369

IUID Required

1560-01-590-7369 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. 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.

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End Users 1560-01-590-7369

US Air Force (FBB4)
Effective Date:: 1 Dec 2010; AMC 0 AMSC 0 AMSC P IMC E DSOR CN

Approved Sources 1560-01-590-7369

Part Number
Manufacturer
Status
17N6P0639-566: 88277 - The Boeing Company (Active); Primary Buy; RNCC 3 RNVC 2 DAC 5

Datasheet 1560-01-590-7369

Characteristic
Specifications
FIIG: A11500
End Item Identification [AGAV]: C-17A

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Freight Information 1560-01-590-7369

1560-01-590-7369 has freight characteristics.. 1560-01-590-7369 has a variance between NMFC and UFC when transported by rail and the description should be consulted.