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1730-00-214-0818

Fuselage Jacking Pad

1730002140818 002140818 49D6296L

An item constructed of the required shape or contour with a padding material cemented or riveted to its surface. Used for jacking of fuselage without the aid of integral jacking point. View more Fuselage Jacking Pad

1730-00-214-0818 PAD,FUSELAGE JACKING 1730002140818 002140818

Managed by United States
NSN Created on 1 Jan 1963
Data Last Changed
January 2023
NATO Update Count
10
NATO Data Quality
1730-00-214-0818 PAD,FUSELAGE JACKING 1730002140818 002140818 1/1
NSN 1730-00-214-0818 (Generic Image) 1/1

1730-00-214-0818 Stock and Availability Marketplace 1730-00-214-0818

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United States (US) 4. 1730-00-214-0818 Marketplace Restrictions Approved Sources Datasheet Management
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/fsg-17/fsc-1730/us 1730-01-288-3611 Fuselage Jacking Pad 1730012883611 012883611 Jacking Pad 1730002140818
002140818 4232 Fuselage Jacking Pad 1730001604232 001604232 499-4946 1730-99-961-4568 1730-01-252-5836
Fuselage Jacking Pad 1730002140818 002140818 www.nsnlookup.com /fsg-17/fsc-1730/us 1730-00-160-
Documents 1730-01-374-7338 5+ Documents ( More... ) https//www.nsnlookup.com /fsg-17/fsc-1730/us 1730-00-214-0818
Fuselage Jacking Pad 1730002140818 002140818 Jacking Pad 1730001604232 001604232 499-4946 1730-
499-4946 1730-99-961-4568 1730-01-252-5836 1730-01-288-3611 1730-01-374-7338 1730-00-045-8366 1730-00-214-0818
Documents 1730-01-252-5836 5+ Documents ( More... ) https//www.nsnlookup.com /fsg-17/fsc-1730/us 1730-00-214-0818
Fuselage Jacking Pad 1730002140818 002140818 1730/us 1730-00-160-4232 Fuselage Jacking Pad 1730001604232
499-4946 1730-99-961-4568 1730-01-252-5836 1730-01-288-3611 1730-01-374-7338 1730-00-045-8366 1730-00-214-0818
Documents 1730-01-288-3611 5+ Documents ( More... ) https//www.nsnlookup.com /fsg-17/fsc-1730/us 1730-00-214-0818
Fuselage Jacking Pad 1730002140818 002140818 4232 Fuselage Jacking Pad 1730001604232 001604232
499-4946 1730-99-961-4568 1730-01-252-5836 1730-01-288-3611 1730-01-374-7338 1730-00-045-8366 1730-00-214-0818

1730-00-214-0818 Demil Restrictions 1730-00-214-0818

DEMIL: B | DEMILI: | CRITICALITY: X | HMIC: N | PMIC: U | EDC: | ADPEC:

1730-00-214-0818 is a Fuselage Jacking Pad 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 is not suspected to be hazardous. The precious metals content of this item is unknown.

1730-00-214-0818 HTS and ScheduleB Import and Export 1730-00-214-0818

1730-00-214-0818 End Users End Users 1730-00-214-0818

Portugal (ZP01)
Effective Date:
1 Apr 1991
Greece (ZU01)
Effective Date:
1 Apr 1991

1730-00-214-0818 Manufacturers Approved Sources 1730-00-214-0818

1730-00-214-0818 Technical Data Datasheet 1730-00-214-0818

Characteristic
Specifications
FIIG
T244-F
Mounting Type For Which Designed [BCNX]
Left Hand
Shape [SHPE]
Rectangular
Padding Material [ASRC]
Rubber, Synthetic
Usage Design [ALCD]
For Model F-84 Aircraft

1730-00-214-0818 Related Items NATO Stock Numbers Related to 1730-00-214-0818

1730-00-214-0818 Freight Data Freight Information 1730-00-214-0818

1730-00-214-0818 has freight characteristics.. 1730-00-214-0818 has a variance between NMFC and UFC when transported by rail and the description should be consulted.