New
6430056-1 Emergency Battery Power Supply
$2,999.00
Model Number: TS56
Technical Description: 24.7 VDC, 3 A, 56 Wh, NiMH
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Description
Benefits
- Provides reliable power for cabin and exit lighting in the event of main electrical failure
- 24.6 VDC nominal, 3 amps maximum output power
- Utilizes Nickel Metal Hydride (NiMH) battery technology
- Can be fully recharged or maintain existing full charge via the aircraft’s primary power bus
- Direct replacement for Radiant 640-13595-00 power supplies
- 6–8 years battery life expectancy
- 2-year on-wing capacity check with no removal required
- Designed and built in Wichita, Kansas USA
- Two-year limited warranty
- FAA TSO Certified
Specifications
Capacity
56 watt-hour
Input Voltage
26 – 32 VDC
Output Power
24.6 VDC nominal, 3 amps maximum
Run Time
137 minutes @ 1.0 amps
Technology
Nickel Metal Hydride (NiMH)
Weight
2.9 lbs (1.32 kg)
Dimensions
9.1”L x 4.3”W x 2.4”H
(231.14mm x 109.22mm x 60.96mm)
Direct Replacement
Radiant 640-13595-00
Battery Life Expectancy
6 – 8 years
Protection
Short circuit, over temperature, under-voltage, over-voltage, and EMI filtering
Mating Connector
D38999/26WC35SN
Case
Anodized aluminum
Certification
FAA TSO-C173a pending
DO-293A pending
RTCA DO-160G pending
Additional information
| Weight | 0.1 lbs |
|---|---|
| Dimensions | 0.1 × 0.1 × 0.1 in |
| Brand |
Mid-Continent Instruments and Avionics |
Shipping & Delivery
SHIPPING INFORMATION
We can ship by UPS, or USPS and DHL Express. We ship nationally, and internationally.
Carriers In Use
SHIPPING COSTS
- International Shipping Quote has to be done manually due to dimensions, weight, end destination, and more. Please E-Mail us.
- Any manner or method is available, call if you need Priority 1-2 day or overnight shipping.
- We are shipping with UPS or USPS and DHL Express
Related products
ETX900-TSO
STC or Part 337 (field approval) is required for installation. If you need the 8130-3 form for international orders, it is an additional fee of $150 per battery and must be requested prior to shipping.
FAA REQUIRED STATEMENT:
“The conditions and test required for TSO approval of this article are minimum performance standards. Those installing this article either on or within a specific type or class of aircraft must determine that the article installation conditions are within the TSO standards. The article may be installed only according to 14 CFR part 43 or the applicable airworthiness requirements.”
