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1560-01-586-1806

Longeron

1560015861806 015861806 74A324108-2012

A principal longitudinal member of the structural framework of an aircraft fuselage, nacelle, empennage boom, or similar component. View more Longeron

1560-01-586-1806 LONGERON 1560015861806 015861806

Managed by United States
NSN Created on 17 Jun 2010
Data Last Changed
May 2023
NATO Update Count
3
NATO Data Quality
1560-01-586-1806 LONGERON 1560015861806 015861806 1/1
NSN 1560-01-586-1806 (Generic Image) 1/1

1560-01-586-1806 Stock and Availability Marketplace 1560-01-586-1806

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1560-01-586-1806 Related Documents Related Documents 1560-01-586-1806 1+ Documents (More...)

74A324108-2012 A principal longitudinal member of the structural framework of an aircraft fuselage,
United States (US) 4. 1560-01-586-1806 Marketplace Restrictions Approved Sources Datasheet Management
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1560-01-586-1806 Demil Restrictions 1560-01-586-1806

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

1560-01-586-1806 is a Longeron 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 a US Munitions List or Commerce Control List Item which must be destroyed to prevent restoration or repair. Only authorized parties may possess this item. 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.

1560-01-586-1806 HTS and ScheduleB Import and Export 1560-01-586-1806

1560-01-586-1806 End Users End Users 1560-01-586-1806

Australia (ZA01)
Effective Date:
1 Jun 2010

1560-01-586-1806 Manufacturers Approved Sources 1560-01-586-1806

1560-01-586-1806 Technical Data Datasheet 1560-01-586-1806

Characteristic
Specifications
FIIG
A11400
End Item Identification [AGAV]
F/A-18 Acft
Aircraft Location [CZDJ]
Lwr Inbd
Aircraft Station Number [CZEJ]
Y488.000 To Y557.500
Aircraft Mission Design Series [CZEK]
F/A-18
Material Document And Classification [MDCL]
Mil-T-81556 Mil Spec Single Material Response
Material [MATT]
Titanium
Overall Length [ABHP]
82.000 Inches Nominal
Part Name Assigned By Controlling Agency [CXCY]
Longeron
Special Features [FEAT]
Ti-6Al-Ti Extrusion; Opposite -2011

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1560-01-586-1806 Freight Data Freight Information 1560-01-586-1806

1560-01-586-1806 has freight characteristics managed by Australia.. 1560-01-586-1806 has a variance between NMFC and UFC when transported by rail and the description should be consulted.