Premium Information is available for this item - Upgrade for $1 a day
1560-01-483-2181
Wing Landing Flap
1560014832181 014832181 L1832003-151
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
May 2023
6
Marketplace 1560-01-483-2181
Request a Quotation from participating marketplace vendors
Related Documents 1560-01-483-2181 1+ Documents (More...)
Request a Quotation from participating marketplace vendors Request Updated Every Day 1560-01-483-2181
RQST NE Related Documents 1560-01-483-2181 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-15
Restrictions 1560-01-483-2181
IUID Required
1560-01-483-2181 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 1560-01-483-2181
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-483-2181
- US Air Force (FXX4)
- Effective Date:
- 1 Mar 2001
Approved Sources 1560-01-483-2181
- Part Number
- Manufacturer
- Status
- L1832003-151
- Manufacturer
- 43999 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-483-2181
- Characteristic
- Specifications
- FIIG
- Specifications
- A11500
- Aircraft Location [CZDJ]
- Flap Assy, Wing Outer Panel No.3
- Aircraft Mission Design Series [CZEK]
- B-1B
- Material [MATT]
- Glass Fiber And Aluminum Alloy
- Special Features [FEAT]
- Used As: Composite Wing Flap Assembly; Opposite -152
Management Data 1560-01-483-2181
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Feb 2023
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
- Oct 2021
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
- Oct 2020
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
- Oct 2019
- 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 1560-01-183-0141
- E
- Department of the Air Force (DF)
- L
- R
- Refer To Net Price 43001.18
- NET PRICE 43001.18
- R
Similar Supply Items to 1560-01-483-2181
Freight Information 1560-01-483-2181
1560-01-483-2181 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 011790. A Sub NMFC of Z. It has a NMFC Description of AIRCRAFT PARTS NOI. 1560-01-483-2181 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. It has a Uniform Freight Classification (UFC) number of 04720 which rates the freight between FCL and LCL. 1560-01-483-2181 has a variance between NMFC and UFC when transported by rail and the description should be consulted. It has a Water Commodity Code (WCC) of 671 for ocean manifesting and military sealift. 1560-01-483-2181 is not classified as a special type of cargo when transported by water. 1560-01-483-2181 is not a consolidation and does not exceed 84" in any dimension. It should be compatible with a standard 72" Aircraft Cargo Door when transported by air.