1560-12-345-1134
Aircraft Spar
1560123451134 123451134 VG95211-ML-123451134 65202-05007Y103
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 2 Feb 1998
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 1560-12-345-1134
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Related Documents 1560-12-345-1134 1+ Documents (More...)
9320-01-310-5084 9320013105084 013105084 is an elastic material of compact (solid) or cellular structure having smooth, crepe or porous surface(s) and having an oval, parallelogram, square, rectangular or d-shaped cross section. it is produced in various thicknesses. strips are limited to widths of 6 inches (152.4mm) or less. it may or may not have a nonrubber backing or a wire cloth or cord insert. for items having a round cross section, see rubber round section. excludes rubber sheet, inner tube repair. see also nonmetallic angle; nonmetallic channel; nonmetallic special shaped section.
Restrictions 1560-12-345-1134
End Users 1560-12-345-1134
- Germany (ZG)
Approved Sources 1560-12-345-1134
- Part Number
- Manufacturer
- Status
- VG95211-ML-123451134
- Manufacturer
- D3030 - Wehrtechnische Dienststelle Fur (Active)
- Definitive Standard
- Definitive Standard
- 65202-05007Y103
- C0417 - Airbus Helicopters Deutschland Gmbh (Active)
- Primary Buy
- Primary Buy
NATO Stock Numbers Related to 1560-12-345-1134
1560-20-006-3207 1560-12-701-1665 1560-12-345-0608 1560-12-344-2653 1560-12-345-1843 1560-37-520-6791 1560-12-345-3086 1560-12-345-3079 1560-12-701-2413 1560-00-406-5987 1560-12-345-0605 1560-99-656-4938 1560-34-037-8675 1560-00-006-2815 1560-12-345-2878 1560-12-182-6212 1560-12-345-2378 1560-12-345-0771