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1560-01-167-6721

Airfoil Rib

1560011676721 011676721 16B7204-11

A principal chordwise rib that gives cross-sectional shape, strength and rigidity to a portion of a wing, stabilizer, and the like. See also RIB (1), STIFFENER, AIRCRAFT View more Airfoil Rib

1560-01-167-6721 RIB,AIRFOIL 1560011676721 011676721

Managed by United States
NSN Created on 3 Dec 1983
Data Last Changed
May 2023
NATO Update Count
14
NATO Data Quality
1560-01-167-6721 RIB,AIRFOIL 1560011676721 011676721 1/1
NSN 1560-01-167-6721 (Generic Image) 1/1

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1560-01-167-6721 Related Documents Related Documents 1560-01-167-6721 3+ Documents (More...)

United States (US) 4. 1560-01-167-6721 Marketplace Restrictions Approved Sources Datasheet Management
RIB,AIRFOIL RQST NS Request Quotation Updated Every Day 1560-01-167-6721 RQST NE Updated Every
Day 1560-01-167-6721 RQST Updated Every Day 1560-01-167-6721 RQST NE Restrictions 1560-01-167-6721 DEMIL
day Upgrade your Account Upgrade 1560-01-245-2813Airfoil Rib1560012452813 012452813 16B7204-13 16B7204-11
TreatedEnd Item Identification [AGAV] 1560-01-245-2813 https//www.nsnlookup.com /fsg-15/fsc-1560/us 1560-01-167-6721
Airfoil Rib 1560011676721 011676721 Upgrade for $1 a day Upgrade your Account Upgrade 1560-01-167
9530-01-327-9172 9530013279172 013279172 is a metallic product of ferrous or nonferrous material. it is produced as a solid section in straight lengths or short barlike forms of cored or solid cross section. it may be round, square, hexagon, oval, half-oval, or half-round shape whose width, diameter, or distance between parallel faces is 3/8 inch or 10.0mm or greater. rectangular shape cross-sectional dimensions are limited to those established in appendix c, fiig a131. it is round to a maximum diameter of 24 inches or 610.0mm. for a rectangular shape less than 3/32 inch or 2.5mm thickness, see wire (1), nonelectrical.

1560-01-167-6721 Demil Restrictions 1560-01-167-6721

DEMIL: B | DEMILI: | CRITICALITY: X | HMIC: P | PMIC: A | EDC: | ADPEC: 0

1560-01-167-6721 is a Airfoil Rib that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item is a US Munitions List Item and must be mutilated to scrap. 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.

1560-01-167-6721 HTS and ScheduleB Import and Export 1560-01-167-6721

1560-01-167-6721 End Users End Users 1560-01-167-6721

Israel (YD01)
Effective Date:
1 Apr 1991
Netherlands (ZN01)
Effective Date:
1 Apr 1991
Denmark (ZS01)
Effective Date:
1 Apr 1991
Norway (ZT01)
Effective Date:
1 Apr 1991

1560-01-167-6721 Manufacturers Approved Sources 1560-01-167-6721

1560-01-167-6721 Technical Data Datasheet 1560-01-167-6721

Characteristic
Specifications
FIIG
A11400
Aircraft Location [CZDJ]
Ventral Fin,Aft
Aircraft Mission Design Series [CZEK]
F-16
Material [MATT]
Aluminum Alloy 2124

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1560-01-167-6721 Freight Data Freight Information 1560-01-167-6721

1560-01-167-6721 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 013455. A Sub NMFC of X. It has a NMFC Description of ALUM FORMS STRUCTURAL. 1560-01-167-6721 is rated as class 60 when transported by Less-Than Truckload (LTL) freight. 1560-01-167-6721 is rated as class 60 when transported by Less-Than Carload (LCL) rail or ocean freight. It has a Uniform Freight Classification (UFC) number of 05820 which rates the freight between FCL and LCL. 1560-01-167-6721 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 576 for ocean manifesting and military sealift. 1560-01-167-6721 is not classified as a special type of cargo when transported by water. 1560-01-167-6721 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.