Ventura 20NKBN25-U3 Aircraft Ni-Cad Battery 20FP25H1C-R FAA/EASA

Description

　　Aircraft Ni-Cad Battery 20 NKBN 25-U3

　　Additional product information

　　Part Number p/n

　　20 NKBN 25-U3

　　Condition

　　New

　　Airplane Type

　　All L 410

　　Tag

　　Serviceable Yellow Tag

　　Remarks

　　N/A

　　20NKBN-25-TD-U3

　　Rechargeable batteries 20NKBN-25-TD-U3 provide autonomous launch of auxiliary power units and engines of aircraft,helicopters and unmanned aerial vehicles;smoothing of voltage ripples in the on-board DC power supply system with a nominal voltage of 27 V in-flight power supply of the first category electric power receivers(necessary for the completion of the flight and safe landing)in the event of a failure or disconnection of primary sources(in case of emergency operation of the power supply system).

　　Details

　　1.Nominal capacity 25.0 A×h.

　　2.Nominal voltage 24.0 V.

　　3.Continuous discharge current up to 250 A.

　　4.The amplitude of the discharge current at the starter load up to 650 A.

　　5.Range of working temperatures:

　　–providing charging and discharging characteristics from-20 to+50°C,

　　–while maintaining performance from-60 to+60°C.

　　6.Resistance to mechanical stress:

　　–vibration:frequency 10-2000 Hz,acceleration 10 g,

　　–impacts:acceleration 12 g,duration of action 2-20 ms.

　　7.Weight with electrolyte,no more than 25 kg.

　　8.Overall dimensions(max.)392×175.5×229 mm.

　　9.Charge safety,day–30.

　　10.Warranty period in cold and temperate climates is 5 years.

　　11.Warranty period in tropical climates is 3 years.

　　12.Service life in a tropical climate,not less than 3 years.

　　Payment&delivery

　　The main principle and goal of Aviamisto has always been the high quality of products and services,as well as their prompt delivery to customers.

　　Aviation rechargeable battery 20NKBN-25-U3

　　Autonomous launch of main and auxiliary aircraft engines or turbo starters.

　　the provision of power in the ground conditions of individual receivers with non-operating main and auxiliary aircraft engines and the absence of power supply from aerodrome sources of electricity;

　　aunch in flight of a stalled aircraft engine or a turbo starter;

　　power in flight of receivers of the 1st category in case of emergency operation of the power supply system.

　　Type of execution in accordance with GOST 15 150-69

　　Characteristics Aggregates and Avionics

　　Ambient temperature From-60 up to+60

　　Supply voltage 24

　　Purpose

　　Aircraft IL-62,IL-76,IL-86,IL-96,IL-106,IL-112

　　Helicopter Mi-8MTV,Mi-171,Mi-172

　　Onboard Systems Ground equipment and engine system

　　20НКБН-25-У3