1560-12-345-1605
Aircraft Spar
1560123451605 123451605 VG95211-ML-123451605 65202-05056Y131
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 6 Feb 1998
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 1560-12-345-1605
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Related Documents 1560-12-345-1605 1+ Documents (More...)
VG95211-ML-123451605 65202-05056Y131 A principal spanwise member of the structural framework of a wing
Germany (DE) 4. 1560-12-345-1605 Marketplace Restrictions Approved Sources Datasheet Management Open
RQST NE Updated Every Day 1560-12-345-1605 RQST Updated Every Day 1560-12-345-1605 RQST NE Restrictions
Germany (DE) 4. 1560-12-345-1605 Marketplace Restrictions Approved Sources Datasheet Management Open
RQST NE Updated Every Day 1560-12-345-1605 RQST Updated Every Day 1560-12-345-1605 RQST NE Restrictions
Restrictions 1560-12-345-1605
End Users 1560-12-345-1605
- Germany (ZG)
Approved Sources 1560-12-345-1605
- Part Number
- Manufacturer
- Status
- VG95211-ML-123451605
- Manufacturer
- D3030 - Wehrtechnische Dienststelle Fur (Active)
- Definitive Standard
- Definitive Standard
- 65202-05056Y131
- C0417 - Airbus Helicopters Deutschland Gmbh (Active)
- Primary Buy
- Primary Buy
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