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321-802-5889
321-733-7477
Model or part number: 214-782-234-001
Rotor Blade Tip Sock NSN 1730-01-044-6922.
NSN 1730-01-044-6922 Datasheet
Factory New, New Material, New Surplus, Overhauled, Serviceable, Repairable, and AS Removed / Used material will be accompanied by a Certificate of Conformance, and any other documents/trace when applicable. We have a 7 year record retention.
We are committed to quality and follow an AS9120 quality management system. AeroBase Group is HAZMAT certified and registered with DDTC,
ITAR, and Aviation Suppliers Association (ASA). All products are 100% inspected.
Quality Commitment »
Delivery of IN-STOCK orders ship same-day when order is placed before 2:00 PM EST.
Delivery dates for NON-STOCK items are estimates based on current backlog and are subject to confirmation at the time of order.
An item designed to secure or restrain movement of unfolded rotary wing blades while the aircraft is on the ground. It consists of a suitable rotary blade attaching device(s), with provisions for securing to the aircraft structure, deck loops, ground loops, or stakes. It may include assemblies consisting of rigid or semirigid tubing, or the like, with blade attaching facility(ies) at one end, and the other end designed to attach to the fuselage or contoured to fit the aircraft fuselage, with provisions for securing purposes. It may include a warning streamer to indicate removal before flight. It may be equipped with a tightening device. For blade securing devices which necessitate folding of the rotary wing blades, see rack, rotary wing blade. Excludes lock (as modified); tie down, aircraft mooring; and tie down, cargo, aircraft.
Packing shall be accomplished to meet the performance test requirements of astm-d4169, distribution cycle 18, assurance level 1.
Packing shall be accomplished using boxes fabricated in accordance with astm-d5118, class weather-resistant.
Options can be exercised as to specific method of preservation or dod approved packaging materials to be used. however, basic preservation method shall be retained, supplemental data shall be complied with, and unit package dimensions shall not be increased by more than one inch. equal or better protection shall be given the item and there shall be no increase in the package cost.
No special marking.
Physical protection.
A-a-59136, cushioning material, closed cell, foam plank.
No requirement.
Other Parts, Nesoi, For Use In Other Military Aircraft, Spacecraft and Spacecraft Launch Vehicles (excluding Parts Of Communication Satellites)
Type Goods Parts For Military
Parts Of Aircraft and Associated Equipment, Spacecraft (including Satellites) and Spacecraft Launch Vehicles, N.e.s.
No special type of cargo code applicable.
Aircraft parts, to include test/tool sets and equipment (other than armament systems).
Construction materials: includes paint and related materials, prefabricated building, wood products, metal and composition mater.
Shipment is not a consolidation, but does exceed 84 inches in one or more dimensions.
Other or no special handling required (sh)
| 08/16 | 02/17 | 07/17 |
|---|---|---|
| 18.00 | 18.00 | 18.00 |
| Code | Definition |
|---|---|
| FN | Factory New. Parts manufactured by the OEM and includes manufacturer certification. |
| NE | New. Parts manufactured by the OEM. May include manufacturer certification or company certification. |
| NS | New Surplus. New material item purchased from excess inventory. |
| OH | Overhauled. Product has been rebuilt and tested in accordance with the manufacturer's specifications by a repair shop (MRO). |
| SV | Serviceable product. |
| AR | As Removed. Product removed from aircraft or platform with no guarentee on the functionality of the part. |
| RP | Repairable. Product can be repaired by a MRO and be given a FAA 8130 or EASA Form 1 certification. |
| Part Number | RNVC | RNAAC | DAC | CAGE |
|---|---|---|---|---|
| 214-782-234-001 | 2 | ZZ | 5 | 97499 |
| 214-782-234-1 | 9 | KE | 1 | 97499 |
| 214-782-234-001 | 2 | ZZ | 5 | 97499 |
| 214-782-234-1 | 9 | KE | 1 | 97499 |
| Name | No. Items | |||
|---|---|---|---|---|
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