1015-14-358-5693
Affut Pied Element
1015143585693 143585693 72800 530096
Managed by France
NSN Created on 7 Sep 1979
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
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Related Documents 1015-14-358-5693 5+ Documents (More...)
1560-14-234-5439 1560142345439 142345439 is a preformed item of various shapes, and contours, which may have a sandwich or honeycomb core bonded to a metallic or nonmetallic facing material. it is used to enclose integral portions of the fuselage or to form partitions or sections within a wing, empennage, fuselage, nacelle or crew compartment. it may have mounting provisions such as predrilled holes to facilitate installation, but will have no items attached to it except bracket (s) or other securing devices to accommodate its own mounting or support. it may be mounted by means of fasteners, bonding or welding. excludes panel, interior lining, aircraft; cover access; cover, access, aircraft; floor (1), aircraft; core material, cellular, structural.
5340-15-109-4697 5340151094697 151094697 is a rod having various cross-sectional shaped bodies with one right hand and one left hand integral externally threaded end. see also turnbuckle; turnbuckle body; and rod, threaded end.
4810-01-544-1233 4810015441233 015441233 is a self-contained power transmitting device designed to convert hydraulic or pneumatic force into controlled mechanical force in the form of torque (rotational mechanical movement limited to less than 360 degrees). the linear motion of the hydraulically or pneumatically operated power piston and shaft is converted to rotary motion in the output shaft through such linkage as rack and pinion, pin and yoke, a connecting link, and the like. excludes hydraulic and pneumatic cylinders and screwjacks.
1560-17-009-7177 1560170097177 170097177 VERKLIKKER,BRANDSTO
1560-14-234-5438 1560142345438 142345438 is a preformed item of various shapes, and contours, which may have a sandwich or honeycomb core bonded to a metallic or nonmetallic facing material. it is used to enclose integral portions of the fuselage or to form partitions or sections within a wing, empennage, fuselage, nacelle or crew compartment. it may have mounting provisions such as predrilled holes to facilitate installation, but will have no items attached to it except bracket (s) or other securing devices to accommodate its own mounting or support. it may be mounted by means of fasteners, bonding or welding. excludes panel, interior lining, aircraft; cover access; cover, access, aircraft; floor (1), aircraft; core material, cellular, structural.
Restrictions 1015-14-358-5693
End Users 1015-14-358-5693
- Malaysia (YW)
- France (ZF)
Approved Sources 1015-14-358-5693
- Part Number
- Manufacturer
- Status
- 72800
- Manufacturer
- F0556 - Thales Las France Sas (Active)
- Primary Buy
- Primary Buy
- 530096
- F0016 - Arquus (Ex Panhard General Defense) (Active)
- Secondary Buy
- Secondary Buy
NATO Stock Numbers Related to 1015-14-358-5693
2510-15-209-3009 2520-99-446-6108 6220-15-204-1528 9999-37-515-0085 5310-15-139-2426 9915-15-219-4601 1730-25-105-4112 1220-14-266-0252 4030-15-175-3668 6685-14-380-3542 1560-99-601-1385 1680-99-600-3219 1005-13-103-5661 2540-15-138-4766 4920-14-441-3681 5340-14-436-9248 2910-12-148-8383 5820-15-138-1601