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1560-01-467-2580

Wing Landing Flap

1560014672580 014672580 17N6P0639-530

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

1560-01-467-2580 FLAP,WING LANDING 1560014672580 014672580

Managed by United States
NSN Created on 20 Aug 1999
Data Last Changed
January 2023
NATO Update Count
3
NATO Data Quality
1560-01-467-2580 FLAP,WING LANDING 1560014672580 014672580 1/1
NSN 1560-01-467-2580 (Generic Image) 1/1

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1560-01-467-2580 Related Documents Related Documents 1560-01-467-2580 1+ Documents (More...)

United States (US) 4. 1560-01-467-2580 Marketplace Restrictions Approved Sources Datasheet Management
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1560-01-467-2580 Demil Restrictions 1560-01-467-2580

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

IUID Required

1560-01-467-2580 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.

1560-01-467-2580 HTS and ScheduleB Import and Export 1560-01-467-2580

1560-01-467-2580 End Users End Users 1560-01-467-2580

US Air Force (FBB4)
Effective Date:
1 Nov 1999
Former MOE Rule:
FEE4

1560-01-467-2580 Manufacturers Approved Sources 1560-01-467-2580

1560-01-467-2580 Technical Data Datasheet 1560-01-467-2580

Characteristic
Specifications
FIIG
A11500
Aircraft Location [CZDJ]
Wing
Side For Which Designed [BWJF]
Right Side
Aircraft Mission Design Series [CZEK]
C-17A
Special Features [FEAT]
Manufacturer Suggested Name - Structural Assembly,Outboard Flap;Nha 17N6p0637
Design Control Reference Or Manufacturers Code [SR-5]
Design Control Reference Or Manufacturers Code [SR-5]
88277
Design Control Reference Or Manufacturers Code [SR-5]
17N6p0639-530

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1560-01-467-2580 Freight Data Freight Information 1560-01-467-2580

1560-01-467-2580 has freight characteristics.. 1560-01-467-2580 has a variance between NMFC and UFC when transported by rail and the description should be consulted.