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1560-01-586-0979

Longeron

1560015860979 015860979 74A321110-2009

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

1560-01-586-0979 LONGERON 1560015860979 015860979

Managed by United States
NSN Created on 17 Jun 2010
Data Last Changed
June 2023
NATO Update Count
4
NATO Data Quality
1560-01-586-0979 LONGERON 1560015860979 015860979 1/1
NSN 1560-01-586-0979 (Generic Image) 1/1

1560-01-586-0979 Stock and Availability Marketplace 1560-01-586-0979

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1560-01-586-0979 Related Documents Related Documents 1560-01-586-0979 1+ Documents (More...)

74A321110-2009 A principal longitudinal member of the structural framework of an aircraft fuselage,
United States (US) 4. 1560-01-586-0979 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 1560-01-586-0979 RQST Updated Every Day 1560-01-586-0979 RQST NE Restrictions

1560-01-586-0979 Demil Restrictions 1560-01-586-0979

DEMIL: Q | DEMILI: 3 | CRITICALITY: X | HMIC: P | PMIC: A | EDC: A | ADPEC: 0

1560-01-586-0979 is a Longeron that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item has been confirmed as a Critical Munitions List Item or a Sensitive Commerce Control List Item and cannot be in the possession of any party anywhere in the World who is not an authorized NATO Government. Any other possessor of this item should mutilate it now as possession violates international and local laws. This item is a confirmed Commerce Control List Item (CCLI). 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.

1560-01-586-0979 HTS and ScheduleB Import and Export 1560-01-586-0979

1560-01-586-0979 End Users End Users 1560-01-586-0979

Australia (ZA01)
Effective Date:
1 Jun 2010

1560-01-586-0979 Manufacturers Approved Sources 1560-01-586-0979

1560-01-586-0979 Technical Data Datasheet 1560-01-586-0979

Characteristic
Specifications
FIIG
A11400
End Item Identification [AGAV]
F-18
Aircraft Location [CZDJ]
Fus Ctr Sect, Lwr
Aircraft Station Number [CZEJ]
Y374.800-Y488.000,X7.000-X6.000
Aircraft Mission Design Series [CZEK]
F/A-18 Hornet
Material Document And Classification [MDCL]
Mil-T-81556 Mil Spec Single Material Response
Material [MATT]
Titanium
Overall Length [ABHP]
120.000 Inches Nominal
Part Name Assigned By Controlling Agency [CXCY]
Longeron
Special Features [FEAT]
Ti-6Al-4V Ti Extrusion; Opposite-2010 Except As Shown

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1560-01-586-0979 Freight Data Freight Information 1560-01-586-0979

1560-01-586-0979 has freight characteristics managed by Australia.. 1560-01-586-0979 has a variance between NMFC and UFC when transported by rail and the description should be consulted.