1560-12-345-1841
Aircraft Spar
1560123451841 123451841 VG95211-ML-123451841 65202-05056Y120
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
Managed by Germany
NSN Created on 10 Feb 1998
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 1560-12-345-1841
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Related Documents 1560-12-345-1841 1+ Documents (More...)
VG95211-ML-123451841 65202-05056Y120 A principal spanwise member of the structural framework of a wing
Germany (DE) 4. 1560-12-345-1841 Marketplace Restrictions Approved Sources Datasheet Management Open
RQST NE Updated Every Day 1560-12-345-1841 RQST Updated Every Day 1560-12-345-1841 RQST NE Restrictions
Germany (DE) 4. 1560-12-345-1841 Marketplace Restrictions Approved Sources Datasheet Management Open
RQST NE Updated Every Day 1560-12-345-1841 RQST Updated Every Day 1560-12-345-1841 RQST NE Restrictions
Restrictions 1560-12-345-1841
End Users 1560-12-345-1841
- Germany (ZG)
Approved Sources 1560-12-345-1841
- Part Number
- Manufacturer
- Status
- VG95211-ML-123451841
- Manufacturer
- D3030 - Wehrtechnische Dienststelle Fur (Active)
- Definitive Standard
- Definitive Standard
- 65202-05056Y120
- C0417 - Airbus Helicopters Deutschland Gmbh (Active)
- Primary Buy
- Primary Buy
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