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True Blue Power

®

 

Manual Number 9018067  

a division of Mid-Continent Instrument Co., Inc.

 

 

Revision C, May 27, 2014 

 

SECTION 1 

GENERAL DESCRIPTION 

 

1.1

 

INTRODUCTION 

 
The model TI250 series Static Electrical Power Inverter is a lightweight power inverter that translates a 20 
to 36 VDC input to a 115 VAC output at 60 Hertz and provides 250 watts (VA) of power. The alternating 
current output is defined as a pure sine wave with less than 2% of total harmonic distortion for clean, 
noise-free, harmonic-free power to supply nearly any common commercial or consumer load rated for a 
nominal input of 115VAC. The TI250 series Inverter is FAA certified to TSO C73 and tested to rigorous 
environmental standards and levels of RTCA DO-160. The small size and light weight in conjunction with 
its installation flexibility (inside or outside the pressure vessel) make it an ideal choice for aircraft power 
needs while reducing the challenges associated with other similar products.  
 
Highlighted features include short circuit protection, overload capability, low voltage shut-down, 
temperature monitoring, a self-resettable over-temperature disable, a remote on/off function, and a fault 
indication output. The TI250 has the same connector of legacy designs plus ground fault interrupter 
protection. The rugged extrusion that houses the unit is designed to help dissipate heat and provide 
mechanical strength against vibration or other possibilities of damage. The TI250 is engineered to run 
cooler and features a fanless design, which saves energy, reduces weight and allows flexible installation 
locations. At only 2.2 pounds, it is lighter and smaller than competing inverters. Additionally, the primary 
stage of the TI250 utilizes current mode control for increased reliability and safety.   
 

1.2 TECHNICAL 

SPECIFICATIONS

 

 

ELECTRICAL ATTRIBUTES:

 

Input Voltage: 

Rated 28VDC nominal; 20-36VDC certified 

Input Current (full load):  

9 amps nominal; 13 amps max 

Input Current (no load) 

150 milliamps 

Input Current (ON/OFF = OFF) 

50 milliamps 

Recommended Circuit Breaker: 

15 amps 

Output Voltage: 

115VAC ±3% at 60 Hertz ±0.1% (single phase) 

Output Power: 

250 watts (250 VA at power factor = 1) 

Output Waveform: 

Pure sine wave 

Power Factor: 

-0.8 to +0.8 

Efficiency: 

85 – 90% nominal 

Total Harmonic Distortion (THD): 

Less than 2% 

Table 1.1 

 

PHYSICAL ATTRIBUTES:

 

Weight: 2.2 

pounds 

Dimensions:  
(not including connector mate) 

6.74 inches long  x  5.94 inches wide  x  2.02 inches high 

Mating Connector (and cable clamp):  MS3106A-18-9S (MCI P/N 9016905-1, -2) 
Mounting: 

Base mount – orientation not critical 

Table 1.2 

 

 

QUALIFICATIONS:

 

Certification: FAA 

TSO-C73 

Environmental Qualification: 

RTCA DO-160G Environmental Category; See Section 5.2 

Altitude: 

-15,000 feet to +55,000 feet 

Temperature: 

-55°C to +70°C  (-67°F to +158°F) 

Table 1.3 

 

Summary of Contents for TI250 Series

Page 1: ...Electrical Power Inverter True Blue Power is a division of Mid Continent Instrument Co Inc Mid Continent Instrument Co Inc dba Mid Continent Instruments and Avionics 9400 E 34th Street N Wichita KS 67226 Manual Number 9018067 PH 800 821 1212 FX 316 630 0723 Rev C May 27 2014 ...

Page 2: ...w mcico com We welcome your comments concerning this manual Although every effort has been made to keep it free of errors some may occur When reporting a specific problem please describe it briefly and include the manual part number the paragraph figure table reference and the page number Send your comments to True Blue Power c o Mid Continent Instrument Co Inc Attn Technical Publications 9400 E 3...

Page 3: ...ision of Mid Continent Instrument Co Inc Revision C May 27 2014 REVISION DETAIL Revision Date Approved Detail A 12 10 13 BAW Initial release B 02 11 14 BMC Revised Technical Specifications C 05 27 14 BMC Revised Section 3 3 1 Wire Gauge Selection ...

Page 4: ...Selection 7 3 3 2 Pin Assignment Information 7 3 3 3 Harness Verification 11 3 4 MOUNTING 11 3 5 INSTALLATION COMPLETION 12 SECTION 4 OPERATION 4 1 ELECTRICAL PERFORMANCE 14 4 2 PROTECTIVE FEATURES 14 4 2 1 Remote On Off 14 4 2 2 Over Voltage 14 4 2 3 Under Voltage 14 4 2 4 Over Temperature 14 4 2 5 Short Circuit and Over Current 14 4 2 6 Ground Fault Protection 15 4 2 7 Fault Shutdown and Indicat...

Page 5: ...rotection The rugged extrusion that houses the unit is designed to help dissipate heat and provide mechanical strength against vibration or other possibilities of damage The TI250 is engineered to run cooler and features a fanless design which saves energy reduces weight and allows flexible installation locations At only 2 2 pounds it is lighter and smaller than competing inverters Additionally th...

Page 6: ...may require as much as five inches past the unit connector to allow for back shell access to the connector 2 3 ROUTING OF CABLES The wires and cable bundle associated with the unit are heavy gauge wire and carry significant power Be aware of routing cables near other electronics or with other wire bundles that may be susceptible to high energy flow Avoid sharp bends in cabling and routing near air...

Page 7: ... the Connector Pinout of Figure 3 3 Figure 3 4 and Wiring Diagram of Table 3 3 Refer to Section 2 Pre Installation Considerations in regards to routing precautions 3 3 1 Wire Gauge Selection Use of PTFE ETFE TFE Teflon or tefzel insulated wire is recommended for aircraft use Use the following wire gauges for each of the pins in the connector Pin A and D 12 14 AWG stranded or solid Pin B and C 18 2...

Page 8: ...round or negative it will allow remote on off control of the unit When unconnected output is OFF this pin will have approximately 16 VDC present internally limited to less than 3 mA If the inverter is to be enabled at all times pin E can be connected to pin G Pin G Remote ON OFF Return This pin is internally connected to pin D Pin G may be used as the return from an ON OFF switch or left unconnect...

Page 9: ... Power 9 Manual Number 9018067 a division of Mid Continent Instrument Co Inc Revision C May 27 2014 Figure 3 4A Typical Small Aircraft Minimum Wiring Installation Figure 3 4B Typical Aircraft Wiring Installation ...

Page 10: ...0 Manual Number 9018067 a division of Mid Continent Instrument Co Inc Revision C May 27 2014 Figure 3 4C Typical Aircraft Fixed Application Installation Figure 3 4D Fully Integrated Multi Inverter Aircraft Cabin System ...

Page 11: ...ith four 20 pan head phillips screws or equivalent A lock washer under the head of each screw is recommended 3 5 INSTALLATION COMPLETION Prior to operating the unit in the aircraft it is recommended to verify the output and functionality of the unit In order to prevent accidental damage to other systems it is best not to attach the output to other equipment or power busses prior to verification Ve...

Page 12: ...r 12 Manual Number 9018067 a division of Mid Continent Instrument Co Inc Revision C May 27 2014 Connector per MS3102A 18 9P 2 0 4 75 5 0 5 50 5 94 4X Ø 22 10 32 Mounting Holes 6 0 0 7 Figure 3 5 TI250 Outline Drawing ...

Page 13: ...remote on off control of the inverter is also used to reset the inverter should an over current or GFI fault condition occur 4 2 2 Over Voltage When the input voltage exceeds the operating range of the unit See Section 1 2 1 absolute maximum input of 36VDC the unit senses an over voltage condition and disables the output The unit will dynamically monitor the input voltage such that if the input re...

Page 14: ...lt be detected the AC output will be disabled and the fault output will indicate Remove all inverter loads before re enabling the inverter 4 2 7 Fault Shutdown and Indication The TI250 monitors the AC output load its internal temperature and operation status Should the load be excessive or the inverter become too hot the inverter will disable the AC output and indicate a fault status on the fault ...

Page 15: ...emperature In Flight Loss of Cooling Decompression Overpressure 4 4 5 1 4 5 2 4 5 5 4 6 2 4 6 3 Category F3 Y Operating Low Temp 55C Operating High Temp 70C Category Y 300 minutes 40C 75 Altitude 55 000 ft 15 000 ft Temperature Variation 5 Category S2 Humidity 6 Category B Operational Shock and Crash Safety 7 Category B Vibration 8 Category R Curve C C1 RCC1 Category U Curve G Explosion 9 Category...

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