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1560-01-504-7377
Wing Landing Flap
1560015047377 015047377 17P6P5601-49
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
January 2023
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RQST NE Restrictions 1560-01-504-7377 DEMIL: D | DEMILI : 1 | CRITICALITY : X | HMIC : P | PMIC : A
Wing Landing Flap 1560015047377 015047377 AssyUOMTechnical DocumentQuantative ExpressionDepartment
Restrictions 1560-01-504-7377
IUID Required
1560-01-504-7377 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.
Import and Export 1560-01-504-7377
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-504-7377
- US Air Force (FBB4)
- Effective Date:
- 1 Feb 2003
Approved Sources 1560-01-504-7377
- Part Number
- Manufacturer
- Status
- 17P6P5601-49
- Manufacturer
- 88277 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-504-7377
- Characteristic
- Specifications
- FIIG
- Specifications
- A11500
- Aircraft Mission Design Series [CZEK]
- C-17A
- Material [MATT]
- Glass Fiber
- Part Name Assigned By Controlling Agency [CXCY]
- Inbd Flap/Inbd Trlg Edge Panel
- Special Features [FEAT]
- Eff. From 17A071-184;C/O 3 Spar Assy; 10 Rib Assy; 2 Skin Assy; 1 Channel Assy; 2 Support Assy; 2 Plugs; 10 Angles; 2 Rub Strips; Polyglass/Satin Cloth,Composition Matl. Carbon Fiber Epoxy Resin Impregrated; Dms 2224, Type 1 Class W,Grade 5; Misc. Hardware;Nha 17P6-5601-503
Management Data 1560-01-504-7377
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Oct 2018
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
- MOE
- USC
- Code
- Statement
- Order of Use
- Jump To Code
- Qty Per Assy
- UOM
- Technical Document
- Quantative Expression
- Code
- Department of the Air Force (DF)
- L
- E
- Replaced By 1560-01-599-5126
- E
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Freight Information 1560-01-504-7377
1560-01-504-7377 has freight characteristics.. 1560-01-504-7377 has a variance between NMFC and UFC when transported by rail and the description should be consulted.