1560-12-183-3081
Aircraft Spar
1560121833081 121833081 VG95211-ML-121833081 1120-30406.03 1120-30406-03
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 3 Apr 1980
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality

Marketplace 1560-12-183-3081
Need Help?
Request a Quotation from participating marketplace vendors
Request a Quotation from participating marketplace vendors
Related Documents 1560-12-183-3081 1+ Documents (More...)
VG95211-ML-121833081 1120-30406.03 1120-30406-03 A principal spanwise member of the structural framework
Germany (DE) 4. 1560-12-183-3081 Marketplace Restrictions Approved Sources Datasheet Management Open
RQST NE Updated Every Day 1560-12-183-3081 RQST Updated Every Day 1560-12-183-3081 RQST NE Restrictions
Germany (DE) 4. 1560-12-183-3081 Marketplace Restrictions Approved Sources Datasheet Management Open
RQST NE Updated Every Day 1560-12-183-3081 RQST Updated Every Day 1560-12-183-3081 RQST NE Restrictions
Restrictions 1560-12-183-3081
End Users 1560-12-183-3081
- Germany (ZG)
Approved Sources 1560-12-183-3081
- Part Number
- Manufacturer
- Status
- VG95211-ML-121833081
- Manufacturer
- D3030 - Wehrtechnische Dienststelle Fur (Active)
- Definitive Standard
- Definitive Standard
- 1120-30406.03
- C0418 - Airbus Helicopters Deutschland Gmbh (Active)
- Primary Buy
- Primary Buy
- 1120-30406-03
- C0418 - Airbus Helicopters Deutschland Gmbh (Active)
- Secondary Buy
- Secondary Buy
Similar Supply Items to 1560-12-183-3081

















