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True Blue Power

®

 

16 

Manual Number 9017680  

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

 

 

Revision C, January 2, 2015

 

SECTION 5 

CONFORMANCE

 

 

5.1 

CONTINUED AIRWORTHINESS STATEMENT

 

 
No periodic scheduled maintenance or calibration is necessary for continued airworthiness of the TI1200 
Series Static Inverter. If the unit fails to perform to specifications, the unit must be removed and serviced 
by Mid-Continent Instruments and Avionics or their authorized designee.  
 

5.2 ENVIRONMENTAL 

QUALIFICATION 

STATEMENT

 

 

NOMENCLATURE:

  

Static Electrical Power Inverter 

 

MODEL NUMBER:

   

TI1200, TI1202 

TSO NUMBER:

  C73 

   

MANUFACTURERS SPECIFICATIONS: 

 

Minimum Performance Specifications: Test Specification (TS)

 

501, Test Data Sheet (TDS) 501 

 

QUALIFICATION STANDARD: 

RTCA DO-160G  

 

 

CONDITIONS 

SECTION 

DESCRIPTION OF TEST 

Temperature and Altitude 
 Low 

Temperature 

 High 

Temperature 

 

In-Flight Loss of Cooling 

 Decompression 
 Overpressure 

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 

Category S2 

Humidity 6 

Category 

Operational Shock and 
Crash Safety 

7 Category 

Vibration 

Category R, Curve C, C1 

Category U, Curve G 

[(RCC1)(UG)] 

Explosion 9 

Category 

Waterproofness 10 

Category 

Fluids 11 

Category 

Sand and Dust 

12 

Category X 

Fungus 13 

Category 

Salt Spray 

14 

Category X 

Magnetic Effect 

15 

Category Z 

Power Input 

16 

Category X 

Voltage Spike 

17 

Category X 

Audio Frequency Conducted 
Susceptibility 

18 Category 

Induced Signal Susceptibility 

19 

Category X 

Radio Frequency Susceptibility 

20 

 

Category X 

Emission of Radio Freq Energy 

21 

 Category B 

Lightning Induced Transient 
Susceptibility 

22 Category 

Lightning Direct Effects 

23 

Category X 

Icing 24 

Category 

ESD 25 

Category 

Flammability 26  Category 

 
 

Содержание TI1200

Страница 1: ... Series Static 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 Manual Number 9017680 Wichita KS 67226 Rev C January 2 2015 ...

Страница 2: ...www 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...

Страница 3: ... division of Mid Continent Instrument Co Inc Revision C January 2 2015 REVISION DETAIL Rev Date Approved Detail A 04 27 12 JRC Initial release B 07 23 12 JDS Page 9 view overlaps Page 15 TS and TDS 501 was 500 C 01 02 15 BMC Added TI1202 model ...

Страница 4: ...ARNESS 8 3 3 1 Wire Gauge Selection 8 3 3 2 Pin Assignment Information 8 3 3 3 Harness Verification 11 3 4 MOUNTING 11 3 5 INSTALLATION COMPLETION 11 SECTION 4 OPERATION 4 1 ELECTRICAL PERFORMANCE 13 4 2 PROTECTIVE FEATURES 14 SECTION 5 CONFORMANCE 5 1 CONTINUED AIRWORTHINESS STATEMENT 15 5 2 ENVIRONMENTAL QUALIFICATION STATEMENT 15 NUMBER LIST OF TABLES AND FIGURES 1 1 Electrical Attributes Table...

Страница 5: ...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 and a remote on off function The rugged extrusion that houses the unit is designed to help dissipate heat and pro...

Страница 6: ... C January 2 2015 Qualifications Model TI1200 Model TI1202 Qualification FAA TSO C73 Environmental Qualification RTCA DO 160G Environmental Category F3 Y S2BB RCC1 UG XXXXXXZXXXXXBXXXXX Altitude 15 000 ft to 55 000 ft See Figure 4 3 Temperature 55 C to 70 C 67 F to 158 F See Figure 4 1 Table 1 3 ...

Страница 7: ...h 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 aircraft control cabl...

Страница 8: ...nstruct the cable harness with regards to the instructions below and using 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...

Страница 9: ...ach can be used If a single pole breaker is used install the breaker on the wire from pin B If a double pole breaker is installed route both pins B and D through the circuit breaker Remote On Off Control see section 4 2 1 Remote ON OFF Control Connecting this pin to either DC Negative or to aircraft ground will enable the AC output of the inverter By utilizing a switch between this pin and ground ...

Страница 10: ...cuit Breakers 110VAC Outlet s not supplied INVERTER ENABLE Remote ON OFF 2 1 A B GFI Ground Fault Indicator not supplied Optional Notes I Wiring diagrams above represent various examples of typical installations II It is recommended to attach case to the aircraft metal structure III The recommended outlet protection may consist of either A single 10A circuit breaker for all outlet s single or doub...

Страница 11: ...y Four 20 mounting holes should be provided in the aircraft in accordance with Figure 3 5 Secure the unit with 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 ot...

Страница 12: ...True Blue Power 12 Manual Number 9017680 a division of Mid Continent Instrument Co Inc Revision C January 2 2015 Figure 3 5 TI1200 Series Outline Drawing ...

Страница 13: ...raft accessories including laptops personal electronics onboard systems and many others See Section 1 2 1 for tolerance ranges The unit is designed as a two stage solid state switch mode power supply The power transformation utilizes a first stage push pull methodology followed by an H bridge AC forming second stage The primary stage utilizes current mode control providing instantaneous load prote...

Страница 14: ...e When the input voltage drops below the operating range of the unit See Section 1 2 1 absolute minimum input of 20VDC the unit senses an under voltage condition and disables the output The unit will dynamically monitor the input voltage such that if the input returns to within the normal operating range the output will be enabled and allow the unit to operate normally 4 2 4 Over Temperature The T...

Страница 15: ...tput 4 2 6 Temperature Regulated Cooling The unit is equipped with two internal brushless DC fans for cooling to extend the power range and long term life The fans are activated at a specified point determined by the continuous monitoring of the internal temperature The fans operate very quietly to reduce the audible noise in any environment The two fans provide independent redundancy for protecti...

Страница 16: ...Altitude Low Temperature High Temperature 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 Category U Cu...

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