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1560-01-476-7442

Aircraft Spar

1560014767442 014767442 40592-00

A principal spanwise member of the structural framework of a wing, stabilizer, other airfoil, and the like. It is designed to absorb bending loads applied to the airfoil. View more Aircraft Spar

1560-01-476-7442 SPAR,AIRCRAFT 1560014767442 014767442

Managed by United States
NSN Created on 20 Jul 2000
Data Last Changed
January 2023
NATO Update Count
2
NATO Data Quality
1560-01-476-7442 SPAR,AIRCRAFT 1560014767442 014767442 1/1
NSN 1560-01-476-7442 (Generic Image) 1/1

1560-01-476-7442 Stock and Availability Marketplace 1560-01-476-7442

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1560-01-476-7442 Related Documents Related Documents 1560-01-476-7442 1+ Documents (More...)

40592-00 A principal spanwise member of the structural framework of a wing, stabilizer, other airfoil
United States (US) 4. 1560-01-476-7442 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 1560-01-476-7442 RQST Updated Every Day 1560-01-476-7442 RQST NE Restrictions

1560-01-476-7442 Demil Restrictions 1560-01-476-7442

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

1560-01-476-7442 is a Aircraft Spar 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.

1560-01-476-7442 HTS and ScheduleB Import and Export 1560-01-476-7442

1560-01-476-7442 End Users End Users 1560-01-476-7442

Belgium (ZB01)
Effective Date:
1 Jul 2000

1560-01-476-7442 Manufacturers Approved Sources 1560-01-476-7442

1560-01-476-7442 Technical Data Datasheet 1560-01-476-7442

Characteristic
Specifications
FIIG
A11400
Aircraft Location [CZDJ]
Covered Fin Assy
End Item Identification [AGAV]
Covered Fuselage Assy On The L21b Super Piper Cub Acft; 77294 New Piper Aircraft

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1560-01-476-7442 Freight Data Freight Information 1560-01-476-7442

1560-01-476-7442 has freight characteristics.. 1560-01-476-7442 has a variance between NMFC and UFC when transported by rail and the description should be consulted.