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1560-01-122-8633
Aircraft Structural Panel
1560011228633 011228633 5-85637-54
A preformed item of various shapes, and contours, which may have a sandwich or honeycomb core bonded to a metallic or nonmetallic facing material. It is used to enclose integral portions of the fuselage or to form partitions or sections within a wing, empennage, fuselage, nacelle or crew compartment. It may have mounting provisions such as predrilled holes to facilitate installation, but will have no items attached to it except bracket (s) or other securing devices to accommodate its own mounting or support. It may be mounted by means of fasteners, bonding or welding. Excludes PANEL, INTERIOR LINING, AIRCRAFT; COVER ACCESS; COVER, ACCESS, AIRCRAFT; FLOOR (1), AIRCRAFT; CORE MATERIAL, CELLULAR, STRUCTURAL. View more Aircraft Structural Panel
January 2023
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Restrictions 1560-01-122-8633
1560-01-122-8633 is a Aircraft Structural Panel 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 1560-01-122-8633
- Schedule B
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- HTS Code
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End Users 1560-01-122-8633
- US Air Force (FXX5)
- Effective Date:
- 1 Apr 1991
Approved Sources 1560-01-122-8633
- Part Number
- Manufacturer
- Status
- 5-85637-54
- Manufacturer
- 81205 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-122-8633
- Characteristic
- Specifications
- FIIG
- Specifications
- A11700
- Material [MATT]
- Titanium
- Material Document And Classification [MDCL]
- Ams 4900,Annealed Assn Std Single Material Response
- Side For Which Designed [BWJF]
- Right Side
- Overall Length [ABHP]
- 2.700 Inches Nominal
- Overall Width [ABMK]
- 2.100 Inches Nominal
- Thickness [ABNM]
- 0.030 Inches Nominal
- End Item Identification [AGAV]
- Kc-135
Management Data 1560-01-122-8633
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Freight Information 1560-01-122-8633
1560-01-122-8633 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 106280. A Sub NMFC of X. It has a NMFC Description of PLATES STRUCTURAL I/S NOI. 1560-01-122-8633 is rated as class 50 when transported by Less-Than Truckload (LTL) freight. 1560-01-122-8633 is rated as class 50 when transported by Less-Than Carload (LCL) rail or ocean freight. It has a Uniform Freight Classification (UFC) number of 54650 which rates the freight between FCL and LCL. 1560-01-122-8633 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. 1560-01-122-8633 is not classified as a special type of cargo when transported by water. 1560-01-122-8633 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.