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1680-01-468-8961

Aircraft Interior Lining Panel

1680014688961 014688961 17P1B4202-501

A preformed metallic/nonmetallic item specifically designed for mounting on the inside of the fuselage of an aircraft. It is of a special size, shape, and thickness to conform to the contour of the aircraft. It conceals cavities, controls, tubing, wiring and the like, as well as provides a sound barrier. Pockets, trays or shelves may be included. Excludes: PANEL, STRUCTURAL, AIRCRAFT. View more Aircraft Interior Lining Panel

1680-01-468-8961 PANEL,INTERIOR LINING,AIRCRAFT 1680014688961 014688961

Managed by United States
NSN Created on 26 Oct 1999
Data Last Changed
January 2023
NATO Update Count
4
NATO Data Quality
1680-01-468-8961 PANEL,INTERIOR LINING,AIRCRAFT 1680014688961 014688961 1/1
NSN 1680-01-468-8961 (Generic Image) 1/1

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1680-01-468-8961 Related Documents Related Documents 1680-01-468-8961 1+ Documents (More...)

17P1B4202-501 A preformed metallic/nonmetallic item specifically designed for mounting on the inside
United States (US) 4. 1680-01-468-8961 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 1680-01-468-8961 RQST Updated Every Day 1680-01-468-8961 RQST NE Restrictions

1680-01-468-8961 Demil Restrictions 1680-01-468-8961

DEMIL: A | DEMILI: 1 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: | ADPEC: 0

1680-01-468-8961 is a Aircraft Interior Lining 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 is not suspected to be hazardous. This item does not contain a precious metal.

1680-01-468-8961 HTS and ScheduleB Import and Export 1680-01-468-8961

1680-01-468-8961 End Users End Users 1680-01-468-8961

US Air Force (FBB5)
Effective Date:
1 Oct 1999

1680-01-468-8961 Manufacturers Approved Sources 1680-01-468-8961

1680-01-468-8961 Technical Data Datasheet 1680-01-468-8961

Characteristic
Specifications
FIIG
A11700
Material [MATT]
Plastic
Aircraft Location [CZDJ]
Cockpit, Lower Aft
Side For Which Designed [BWJF]
Left Side
Aircraft Mission Design Series [CZEK]
C-17
Overall Length [ABHP]
27.000 Inches Nominal
End Item Identification [AGAV]
C-17
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]
17P1b4202-501

1680-01-468-8961 Management Data Management Data 1680-01-468-8961

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Aug 2005
Department of the Air Force (DF)
EA
Subscribe
1

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1680-01-468-8961 Freight Data Freight Information 1680-01-468-8961

1680-01-468-8961 has freight characteristics.. 1680-01-468-8961 has a variance between NMFC and UFC when transported by rail and the description should be consulted.