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1560-01-473-3988
Aircraft Structural Panel
1560014733988 014733988 17P2A6509-31
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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Marketplace 1560-01-473-3988
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Restrictions 1560-01-473-3988
IUID Required
1560-01-473-3988 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. Demilitarization of this item has been confirmed and is not currently subject to changes. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). 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 1560-01-473-3988
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-473-3988
- US Air Force (FBB4)
- Effective Date:
- 1 Apr 2000
Approved Sources 1560-01-473-3988
- Part Number
- Manufacturer
- Status
- 17P2A6509-31
- Manufacturer
- 88277 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-473-3988
- Characteristic
- Specifications
- FIIG
- Specifications
- A11700
- Material [MATT]
- Plastic Epoxy And
- Material [MATT]
- Plastic Polyamide
- Material Document And Classification [MDCL]
- Dms2288 Mfr Ref 1St Material Response And
- Material Document And Classification [MDCL]
- Dms1974 Mfr Ref 2Nd Material Response
- Aircraft Location [CZDJ]
- Center Fuselage
- Aircraft Mission Design Series [CZEK]
- C-17A
- Special Features [FEAT]
- Manufacturer Suggested Name - Panel Assembly-Fillet,Lwr Y=758.500-Y=833.500;Nha 17P2a6509-1
- 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]
- 17P2a6509-31
Management Data 1560-01-473-3988
- 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
Air Force
- Budget:
- S
- 57X3010 - Aircraft Replenishment Spares
- Aggregation Code:
- BA
- C-17 PROGRAM
- Price Validation Code:
- N
- The current standard price in Catalog Management Data (CMD) has not analyzed or coded for LP/LM.
The price has not been analyzed or reviewed for accuracy.
ZOP or Standard price challenges are permissible but must be supported with adequate justification. However, if coded for Local Purchase (LP) or Fabrication/Manufacture as indicated with an (LM) Acquisition Advice Code of “L” or “F”, then it must be evaluated locally where purchased or fabricated.
- Expendability
Recoverability
Repairability: - T
- Expendable. Reparable. Condemn at Depot. AF Recoverable Assembly Management System (AFRAMS).
NATO Stock Numbers Related to 1560-01-473-3988
Freight Information 1560-01-473-3988
1560-01-473-3988 has freight characteristics.. 1560-01-473-3988 has a variance between NMFC and UFC when transported by rail and the description should be consulted.