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1730-01-498-7585

Aircraft Engine Stand

1730014987585 014987585 5HG90190-105

A structure designed for supporting aircraft engines incident to installation in or removal from aircraft. See also STAND, MAINTENANCE, AIRCRAFT ENGINE and TEST STAND, AIRCRAFT ENGINE. View more Aircraft Engine Stand

1730-01-498-7585 STAND,AIRCRAFT ENGINE 1730014987585 014987585

Managed by United States
NSN Created on 29 Jun 2002
Data Last Changed
January 2023
NATO Update Count
3
NATO Data Quality
1730-01-498-7585 STAND,AIRCRAFT ENGINE 1730014987585 014987585 1/1
NSN 1730-01-498-7585 (Generic Image) 1/1

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United States (US) 4. 1730-01-498-7585 Marketplace Restrictions Approved Sources Datasheet Management
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1730-01-498-7585 Demil Restrictions 1730-01-498-7585

DEMIL: A | DEMILI: 7 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: A | ADPEC: 0

1730-01-498-7585 is a Aircraft Engine Stand that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. The DCMO has forced the Demilization requirements for this item as the ICP has not collaborated. 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.

1730-01-498-7585 HTS and ScheduleB Import and Export 1730-01-498-7585

1730-01-498-7585 End Users End Users 1730-01-498-7585

US Air Force (FLL5)
Effective Date:
1 Jun 2002

1730-01-498-7585 Manufacturers Approved Sources 1730-01-498-7585

1730-01-498-7585 Management Data Management Data 1730-01-498-7585

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Dec 2011
Department of the Air Force (DF)
EA
Subscribe
1

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1730-01-498-7585 Freight Data Freight Information 1730-01-498-7585

1730-01-498-7585 has freight characteristics.. 1730-01-498-7585 has a variance between NMFC and UFC when transported by rail and the description should be consulted.