1560-01-502-5145

Aircraft Frame

1560015025145 015025145 212-060-817-079S

A principal transverse structural member of the fuselage, hull, nacelle, pod, and the like. It follows the periphery and provides shape and support by attachment to the longitudinal members or skin. View more Aircraft Frame

1560-01-502-5145 FRAME,AIRCRAFT 1560015025145 015025145

Managed by United States
NSN Created on 7 Nov 2002
Data Last Changed
November 2023
NATO Update Count
3
NATO Data Quality
1560-01-502-5145 FRAME,AIRCRAFT 1560015025145 015025145 1/1
NSN 1560-01-502-5145 (Generic Image) 1/1

1560-01-502-5145 Stock and Availability Marketplace 1560-01-502-5145

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212-060-817-079S A principal transverse structural member of the fuselage, hull, nacelle, pod, and the
United States (US) 4. 1560-01-502-5145 Marketplace Restrictions Approved Sources Datasheet Management
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1560-01-502-5145 Demil Restrictions 1560-01-502-5145

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

1560-01-502-5145 is a Aircraft Frame 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.

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