Premium Information is available for this item - Upgrade for $1 a day
1560-01-508-7727
Wing Landing Flap
1560015087727 015087727 17P6P5601-4
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
1
Marketplace 1560-01-508-7727
Request a Quotation from participating marketplace vendors
Related Documents 1560-01-508-7727 1+ Documents (More...)
Request a Quotation from participating marketplace vendors Request Updated Every Day 1560-01-508-7727
RQST NE Updated Every Day 1560-01-508-7727 RQST Updated Every Day 1560-01-508-7727 RQST NE Related Documents
Restrictions 1560-01-508-7727
IUID Required
1560-01-508-7727 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.
Import and Export 1560-01-508-7727
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-508-7727
- US Air Force (FBB4)
- Effective Date:
- 1 Jun 2003
Approved Sources 1560-01-508-7727
- Part Number
- Manufacturer
- Status
- 17P6P5601-4
- Manufacturer
- 88277 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-508-7727
- Characteristic
- Specifications
- FIIG
- Specifications
- 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 2 Support Assy, 4 Spar Assy; 4 Washer (An9604l) (Limited Eff); Rivet As Required; 3 Rib Assy; 1 Skin Assy; 1 Spare Assy; 1 Channel Assy; 2 Support Assy
Management Data 1560-01-508-7727
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- May 2010
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
Similar Supply Items to 1560-01-508-7727
Freight Information 1560-01-508-7727
1560-01-508-7727 has freight characteristics.. 1560-01-508-7727 has a variance between NMFC and UFC when transported by rail and the description should be consulted.