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CCU2 Connections Manual
Simkits & The Real Cockpit are trademarks from TRC Development Page 1
CCU2 Connections, Wiring Diagrams
Modifications &
Schematics
© TRC Development 2005 Nothing from this document may be reproduced in writing or electronically
without written permission of TRC Development b.v.
The names “The Real Cockpit” and “SimKits” are registered tradenames of TRC Development b.v.
TRC Development b.v. – The Netherlands – www.therealcockpit.com - www.simkits.com
CCU2 Connections Manual
Simkits & The Real Cockpit are trademarks from TRC Development Page 2
Contents 1. CCU2 Connections ....................................................................................................... 3
Instruments controlled by CCU2 ..................................................................................... 4 2. The Central Control Unit ................................................................................................ 5
List and position of the I/O connectors ............................................................................ 5 4. Connectors and their I/O lines ........................................................................................ 6
The CCU2 needs 2 different positive voltages of 5 volts. .................................................. 6 Modified Servos ............................................................................................................ 6 Rotary Encoders............................................................................................................ 6 Potentiometers .............................................................................................................. 7 CN1 to CN10 Do not exist on the CCU2 Board................................................................ 7 CN13 Fuel selector + Shut off .................................................................................... 8 CN14 Digital Clock .................................................................................................... 8 CN15 Flaps ............................................................................................................... 8 CN16 Trim wheel....................................................................................................... 9 CN17 Starter Switch .................................................................................................. 9 CN18 Rudder Pedals................................................................................................. 9 CN19 Yoke ............................................................................................................. 10 CN20 Compass....................................................................................................... 10 CN21 Airspeed Indicator.......................................................................................... 10 CN22 Tachometer ................................................................................................... 10 CN23 Vertical Speed Indicator ................................................................................. 11 CN24 Attitude Indicator ............................................................................................ 11 CN25 Turn Coordinator............................................................................................ 11 CN26 VOR 1 Indicator ............................................................................................. 11 CN27 VOR 2 Indicator ............................................................................................. 11 CN28 ADF Indicator ................................................................................................ 12 CN29 Heading Indicator........................................................................................... 12 CN30 Altimeter........................................................................................................ 12 CN31 Warning Lights & Switch................................................................................. 13 CN32 Servo expansion (connects to servo expansion board) ..................................... 13 CN33 Circuit breakers (4 outputs, 15 inputs) ............................................................. 13 CN34 Switches (16 inputs)....................................................................................... 14 CN35 Servo Ctrld. Fuel Left/Right *) ......................................................................... 14 CN36 Servo Ctrld. EGT/Fuel Flow *) ......................................................................... 14 CN37 Servo Ctrld. Oil Temp/Pressure *) ................................................................... 14 CN38 Servo Ctrld. Suction G./AMM. Indicator *) ........................................................ 15
5. Schematics................................................................................................................. 16 6. Wiring Diagrams ......................................................................................................... 16
CCU2 Connections Manual
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1. CCU2 Connections The CCU2 can drive many different gauges and is able to read out many different instruments, like Throttles, Switches, Trim wheel etc. compared to the CCU1.
(Note: the connections in the above picture between the different instruments and the CCU2 board are just for illustration only. Please see Chapter 2 for exact connections) This document describes how the instruments are connected and how they are driven by the CCU2 and what the signals and their description mean. Although that the document is very clear and can be read by non-technical persons, for full understanding we do recommend that the reader has a basic knowledge of electronics Below you find a list of supported gauges for the aircraft as they are present in Microsoft FS2004. Not all gauges of each aircraft is supported yet, but will be in future with new hardware and software. Some gauges are identical from a hardware viewpoint. There is a so-called “General Instrument” which is a gauge driven by a single servo motor and which has a set of gear wheels inside to enable the output of the pointer to turn up to 360 degrees, while the servo shaft output only produces a 190 degrees turn. Using different face plates (dials) and using the calibration software to inform the driver how to behave, with this “General Instrument” gauges like an Airspeed Indicator, Tachometer and Vertical Speed Indicator for different aircraft can be installed. Therefore the hardware (except the faceplate) for an Airspeed Indicator for a Cessna 172 Skyhawk and a Boeing 737 are basically the same. Using the calibration software, the driver is informed that the pointer can move up to a maximum of 450 Knots for the Boeing and up to a maximum of 145 knots for the Cessna. One can even design a customized faceplate using the available blank, pre cutted faceplates (made from high quality glossy paper) which can be printed in a high resolution inkjet printer like any today available photo quality printer and using one of the available calibtration scales which are close to the one you design yourself. When you like to expand your cockpit with more instruments and gauges, we do recommend the use of the Multi Controller, an expansion board offering 23 I/O lines, which are each programmable to read out a switch, to drive a LED or to drive a single pointer gauge per each I/O line. Up to 32 of these board can be configured in addition to the CCU2. All controllers (including the CCU2) are connected to the PC via USB.
CCU2 Connections Manual
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Instruments controlled by CCU2
ADF Indicator
Airspeed Indicators, choice out of the following types (see the website for the latest additions): - Airliner 450 Knots - Beechcraft Baron 58 - Bell 206B Jet Ranger - Cessna 172 Skyhawk - Cessna 182 Skylane - Cessna Caravan - Extra 300S - Mooney Bravo - Schweizer 232 Sailplane - Sopwith Camel - Vaught Corsair
Altimeter
Attitude Indicator
Elevator Trim Control
Exhaust Gas Temperature & Fuel Flow Indicator (dual indicators)
Flaps Control & Indicator
Fuel Tank Indicator (dual indicators for left and right tank)
Gyro Suction Indicator & Ammeter (dual indicators)
Heading Indicator (with Autopilot Heading Bug)
2 Throttle Controls *)
2 Mixture Controls *)
2 Propeller Controls *)
Oil Temperature & Oil Pressure Indicator (dual indicators)
Switches
Tacho meter, choice of face plate for (see the website for the latest additions): - Cessna 172 Skyhawk - Cessna 182 Skylane - Sopwith Camel - Vaught Corsair
Turn Coordinator
Vertical Speed Indicator, choice of face plate for (see the website for the latest additions): - Beechcraft Baron 58 - Bell 206B Jet Ranger - Cessna 172 Skyhawk - Cessna Caravan - Vaught Corsair
VOR1 Indicator
VOR2 Indicator
Wet Compass
Yoke Control
Rudder Pedals *)
8 Additional Single pointer gauges *)
*) These additional instruments need a future software release.
CCU2 Connections Manual
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2. The Central Control Unit
List and position of the I/O connectors NOTE: The position of the texts on the picture on the left is not identical to the position of the text on the board itself. The CCU2 is prepared for future expansion with more I/O lines and will be able to control instruments for a twin engine aircraft. Therefore more I/O lines are made available. At the same time a number of smaller connectors have been combined into 2 larger connectors. The additional I/O lines will become supported in the near future via software updates. NOTE: The position of the text on the picture on the left is not identical to the position of the text on the board itself. CN11 Handbrake, Avionics Switch, Gear, Light Control, Master Switch CN12 Analog outputs, 8 pcs.*), Quartz Counter CN13 Fuel selector + Shut off CN14 Digital Clock CN15 Flaps, Throttle1/2, Mixture1/2, Prop1/2 CN16 Trim wheel CN17 Starter Switch CN18 Rudder Pedals CN19 Yoke CN20 Compass CN21 Airspeed Indicator CN22 Tachometer CN23 Vertical Speed Indicator CN24 Attitude Indicator CN25 Turn Coordinator CN26 VOR 1 Indicator CN27 VOR 2 Indicator CN28 ADF Indicator CN29 Heading Indicator CN30 Altimeter CN31 Warning Lights & Switch CN32 Future Expansion CN33 Circuit breakers (15 outputs) CN34 Switches (16 inputs) CN35 Servo Ctrld. Fuel Left/Right CN36 Servo Ctrld. EGT/Fuel Flow CN37 Servo Ctrld. Oil Temp/Pressure CN38 Servo Ctrld. Suction G./AMindicator *) These connections are for future expansion and are not yet supported by the firmware and software.
CN
1C
N2
CN
3C
N4
CN
5C
N6
CN
7C
N8
CN
9C
N10
CN
11C
N12
CN
43
CN
13
CN
14
CN
15
CN
16
CN
17
CN
18
CN
19
CN
20
CN
21
CN
22
CN
23
CN
24
CN
25
CN
26
CN
27
CN
35
CN
36
CN
37
CN
38
CN
30
CN
31
CN
32
CN
29
CN
28
CN
33
CN
34
CN
11C
N12
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4. Connectors and their I/O lines The description below informs you on what the I/O lines of each connector mean. Warning: connecting hardware to this I/O lines which draw excessive current, input high currents or short circuit outputs may damage the delicate electronics on the board. Damages caused by improper connection of hardware are not covered by the limited warranty. For each connector the signal names are mentioned. These signal names can be found back on the schematics (last page). When necessary a description of the signal is given.
- The term “Digital Input” means and input towards the CCU2. - The term “Digital Output” means a signal which is coming from the CCU2 towards
the device. - The term “Analog input” means that this input can read an analog value between
0 and 5 volts with a resolution of approx. 1024 different values. - The term “Analog output” means that this ouput can produce a voltage between 0
and 5 volts which can be set by a digital value of 8 bits by software. - The Term “Ground” or “Gnd” is the common ground of all electronics signals. - The term “+5v.” or “Vcc” is the 5 volts power needed to drive the electronics on
the CCU2 board and some electronics inside the gauges. - The term “+5v.X” is the 5 volts power needed to drive the servo motors and is
derived from the separately connected Power Supply. The CCU2 needs 2 different positive voltages of 5 volts. One 5v. is supplied through the USB connection from the controlling PC (CN41) and is used to power the electronics except the servo motors. The other 5v. (marked as 5v.X in the schematics and literature) is powered by an external (PC AT) power supply via CN42. This is designed in this way because the servo motors draw more power than can be delivered through the USB connector from the controlling PC. Both 5v. supplies must be connected in order for the electronics and gauges to function properly. Modified Servos In some instruments, so-called modified servos are used. An normal servo is and electro motor driven by electronics inside the servo motor. Via a number of gears, a small electric motor drives the output axis. The output axis is also connected to a normal potentiometer. The output axis is limited in hardware to turn maximum of approx. 180 degrees. The potentiometer is used to feed back the position of the output axis to the electronics of the servo. The output axis of the servo can be controlled by a pulse width applied to the servo to turn it into a certain position. This feature is used in most gauges. However, some gauges need a continously rotating movement. For this we have choosen to use a standard servo motor and modify it in such a way, that the output axis can turn clockwise and anti clockwise without limitations. Due to such modification, the position of the output axis cannot be determined anymore by the built-in potentiometer. Therefore the mechanics inside the gauge now are also connected to 360 degrees turnable potentiometers, called PIHER position sensors. These position sensors however, only measure a part of the 360 degrees. Their electronic sensitivity is approx. 240 degrees. By using 2 of such sensors and placing them in line but 180 degrees shifted, the CCU2 electronics and software now can pickup the position of the output axis over the full 360 degrees. Finally, by software a precise position of approx. 0.5 degrees is being calculated. Rotary Encoders A rotary encoder is a mechanical dual switch which can rotate continously. During this rotation the 2 switches are closed and opened over 32 times for a full revolution, but not exactly at the same time. The direction of the turn can be determined by the phase of which of the 2 switches are closed first and which last.
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The software of the CCU2 reads out both switches and translates this into a signal telling the flight simulator software that the certain knob is turned left or right and at what speed. Potentiometers In principle, all analog inputs do measure the position/value of a potentiometer (turn or slide). Throughout the whole design of all instruments, a 10Kohm potentiometer is used which is on one side connected to +5v. (Vcc) and on the other side to Ground. The wiper of the potentiometer is connected to the analog input on the CCU2. Potentiometers are used in a.o.: Yoke, Throttle, Mixture, Propeller, Flap Switch, Trim and the Piher Sensors (in essence a potentiometer) in the gauges Altimeter, Heading Indicator, ADF and Compass. CN1 to CN10 Do not exist on the CCU2 Board CN11 Handbrake, Avionics Switch, Gears, Dimmer and Master Switch Pin 1 – Ground Pin 2 – Handbrake HNDB, Digital Input. The pin is forced high, when not connected, via a resistor on the CCU2. When connected to Ground, the Handbrake is active. Pin 3 – Ground Pin 4 – Avionics Switch AVSW, Digital Input. The pin is forced high, when not connected, via a resistor on the CCU2. When connected to Ground, the Handbrake is active. Pin 5 – Not Connected Pin 6 – Ground Pin 7 - Gear Switch GEAR1, Digital Input. The pin is forced high, when not connected, via a resistor on the CCU2. When connected to Ground, the Gear Switch is active. Pin 8 – +5v. Pin 9 - Ground Pin 10 - Gear Light GEAR2, Digital Output. When the Gear is down, a digital “high” (5 volt / max. 20mA) is present on this output. Pin 11 – +5v. Pin 12 - Ground Pin 13 - Gear Light GEAR3, Digital Output. When the Gear is working, a digital “high” (5 volt / max. 20mA) is present on this output. Pin 14 – +5v. Pin 15 – Ground Pin 16 – Dimmer POTM, Analog Input. A potentiometer of 10Kohm is connected between Ground and 5 volts. The input (pin2) is connected to the wiper of the potentiometer. Pin 17 – +5v. Pin 18 – Ground Pin 19 – Master Switch MSW1, Digital Input. The pin is forced high, when not connected, via a resistor on the CCU2. When connected to Ground, the Master Switch 1 (ALT) is active. Pin 20 – Master Switch MSW2, Digital Input. The pin is forced high, when not connected, via a resistor on the CCU2. When connected to Ground, the Master Switch 2 (BAT) is active. CN 12 - Quartz Counter & Future Expansion Pin 1 – Not Connected Pin 2 – Ground Pin 3 – Quartz Counter QCNT, Digital Output. The pin is forced low periodically with 1 HZ. Intervals, when activated by Flight Simulator Software or propriety software and can drive a Quarz Counter via a Transistor Circuit. Never connect a coil of a mechanical counter directly to this output to avoid damages on the CCU2. (Quartz Counter signals are not yet supported) Pin 4 – Lamp output (background lighting) Pin 5 to Pin 20 – Future expansion
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CN13 Fuel selector + Shut off Pin 1 – Ground Pin 2 – FSS1 Digital Input. The pin is forced high, when not connected, via a resistor on the CCU2. When connected to Ground, the FSS1 input is active. Pin 3 – FSS2 Digital Input. The pin is forced high, when not connected, via a resistor on the CCU2. When connected to Ground, the FSS2 input is active. Pin 4 – FSS3 Digital Input. The pin is forced high, when not connected, via a resistor on the CCU2. When connected to Ground, the FSS3 input is active. Pin 5 – FSS4 Digital Input. Pin 6 – No connection Pin 7 – No connection Pin 8 – No connection Pin 9 – No connection Pin 10 – No connection
Tank Switch Table (as connected for TRC Link operation): Left: FSS1 = 0, FSS2 = 1 Both: FSS1 = 1, FSS2 = 0 Right: FSS1 = 0, FSS2 = 0 Fuel Switch Table (as connected for TRC Link operation): On: FSS3 = 1 Off: FSS3 = 0
CN14 Digital Clock Pin 1 – Ground Pin 2 – +5v. Pin 3 – DCS2 Pin 4 – DCS3 Pin 5 – DCS4 Pin 6 – DCS5 Pin 7 – DCS6 Pin 8 – DCS7 Pin 9 – Lamp Pin 10 – DCS1 These I/O lines are dedicated as a combination to drive the sub-assembly Digital Clock and cannot be controlled by propriety software, but only via the SDK. CN15 Flaps Pin 1 – Ground Pin 2 – +5v. Pin 3 – Flaps FLA1 Digital Output Servo Signal, Flaps position indication Pin 4 – Flaps FLA2 Analog Input to read out the position of a 10K potentiometer, which positions are an indication for the desired flaps position. Pin 5 – 2nd Throttle THR2, Analog Input to read out the position of a 10K potentiometer, which positions are an indication for the desired 2nd throttle position.*) Pin 6 – 2nd Micture MIX2, Analog Input to read out the position of a 10K potentiometer, which positions are an indication for the desired 2nd mixture position.*) Pin 7 – 2nd Propeller Adjust PRP2, Analog Input to read out the position of a 10K potentiometer, which positions are an indication for the desired 2nd propeller adjust position.*) Pin 8 – Primary Throttle THR Pin 9 – Primary Mixture MIX Pin 10 – Primary Propeller Adjust PRP
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CN16 Trim wheel Pin 1 – Ground Pin 2 – +5v. Pin 3 – TRW1 Pin 4 – TRW2 Pin 5 – TRW3 Pin 6 – Trim wheel AIR2 Analog Input, relocated by modification from CN21 pin 4. Reads out the position of the Trim Wheel. Pin 7 – No connection Pin 8 – No connection Pin 9 – No connection Pin 10 – No connection CN17 Starter Switch Pin 1 – Ground Pin 2 – No connection Pin 3 – Starter Switch STA1 Digital Input. The pin is forced high, when not connected, via a resistor on the CCU2. When connected to Ground, the STA1 input is active. Pin 4 – Starter Switch STA2 Digital Input. The pin is forced high, when not connected, via a resistor on the CCU2. When connected to Ground, the STA2 input is active. Pin 5 – Starter Switch STA3 Digital Input. The pin is forced high, when not connected, via a resistor on the CCU2. When connected to Ground, the STA3 input is active. Pin 6 – Starter Switch STA4 Digital Input. The pin is forced high, when not connected, via a resistor on the CCU2. When connected to Ground, the STA4 input is active. Pin 7 – No connection Pin 8 – No connection Pin 9 – No connection Pin 10 – No connection
As wired for operation under TRC Link: OFF = STA1 to Ground R = STA2 to Ground L = STA3 to Ground BOTH = All inputs open Start = STA4 to Ground
CN18 Rudder Pedals Pin 1 – Ground Pin 2 – +5v. Pin 3 – Rudder Pedals RUD1 – Analog in – Main analog input Pin 4 – Rudder Pedals RUD2 – Analog in – Toe brake left Pin 5 – Rudder Pedals RUD3 – Analog in – Toe brake right Pin 6 – RUD4 – Analog in Pin 7 – RUD5 – Analog in Pin 8 – NC Pin 9 – NC Pin 10 – NC (Rudder Pedals are not yet supported up to TRC Link version 2.7)
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CN19 Yoke Pin 1 – Ground Pin 2 – +5v. Pin 3 – YOK1 Digital Output. Servo Signal for future implementation of control loading (force feedback) Pin 4 – YOK2 Digital Output. Servo Signal for future implementation of control loading (force feedback) Pin 5 – Yoke YOK3 Analog Input, PITCH Pin 6 – Yoke YOK4 Analog Input, ROLL Pin 7 – NC Pin 8 – NC Pin 9 – NC Pin 10 – NC CN20 Compass Pin 1 – Ground Pin 2 – +5v. X Pin 3 – Compass CMP1 Digital Output, Servo Signal Pin 4 – Compass CMP2 Analog Input for position sensor 1 Pin 5 – Compass CMP2 Analog Input for position sensor 2 Pin 6 – +5v. Pin 7 – Ground Pin 8 – Lamp Pin 9 – NC Pin 10 – NC CN21 Airspeed Indicator Pin 1 – Ground Pin 2 – +5v. X Pin 3 – Airspeed Indicator AIR1 Digital Output, Servo Signal Pin 4 – AIR2 Analog IN, not used on this instrument, but patched to CN16 pin 6 to provide an analog read out of the position of the Trim Wheel. Pin 5 – AIR3 Analog IN, not used. Pin 6 – +5v. Pin 7 – Ground Pin 8 – Lamp Pin 9 – NC Pin 10 – NC CN22 Tachometer Pin 1 – Ground Pin 2 – +5v. X Pin 3 – Tachometer TACH Digital Output Servo Signal Pin 4 – NC Pin 5 – NC Pin 6 – NC Pin 7 – Ground Pin 8 – Lamp Pin 9 – NC Pin 10 – NC
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CN23 Vertical Speed Indicator Pin 1 – Ground Pin 2 – +5v. X Pin 3 – Vertical Speed Indicator VSPD Digital Output Servo Signal Pin 4 – NC Pin 5 – NC Pin 6 – NC Pin 7 – Ground Pin 8 – Lamp Pin 9 – NC Pin 10 – NC CN24 Attitude Indicator Pin 1 – Ground Pin 2 – +5v. X Pin 3 – Attitude Indicator ATT1 Digital Output Servo Signal Pin 4 – Ground Pin 5 – +5v. X Pin 6 – Attitude Indicator ATT2 Digital Output Servo Signal Pin 7 – Ground Pin 8 – Lamp Pin 9 – NC Pin 10 – NC CN25 Turn Coordinator Pin 1 – Ground Pin 2 – +5v. X Pin 3 – Turn Coordinator TRN1 Digital Output Servo Signal Pin 4 – Ground Pin 5 – +5v. X Pin 6 – Turn Coordinator TRN2 Digital Output Servo Signal Pin 7 – Ground Pin 8 – Lamp Pin 9 – NC Pin 10 – NC CN26 VOR 1 Indicator Pin 1 – Ground Pin 2 – +5v. X Pin 3 – VOR 1 Indicator VOR1 Digital Output Servo Signal Pin 4 – VOR 1 Indicator VOR2 Digital Output Servo Signal Pin 5 – VOR 1 Indicator VOR3 Digital Output Servo Signal Pin 6 – VOR 1 Indicator VOR4 Analog In Pin 7 – VOR 1 Indicator VOR5 Analog In Pin 8 – Lamp Pin 9 – +5v. Pin 10 – NC CN27 VOR 2 Indicator Pin 1 – Ground Pin 2 – +5v. X Pin 3 – VOR 2 Indicator VOR6 Digital Output Servo Signal Pin 4 – VOR 2 Indicator VOR7 Digital Output Servo Signal Pin 5 – VOR 2 Indicator VORx Analog In (Not Used) Pin 6 – VOR 2 Indicator VOR8 Analog In Pin 7 – VOR 2 Indicator VOR9 Analog In Pin 8 – Lamp Pin 9 – +5v. Pin 10 –
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CN28 ADF Indicator Pin 1 – Ground Pin 2 – +5v. X Pin 3 – ADF Indicator ADF1 Digital Output Servo Signal Pin 4 – ADF2 Digital Output Servo Signal (Not Used) Pin 5 – ADF Indicator ADF3 Digital Input (Rotary Encoder) Pin 6 – ADF Indicator ADF4 Digital Input (Rotary Encoder) Pin 7 – ADF Indicator ADF Indicator ADF5 Analog Input, Piher Position Sensor Pin 8 – ADF Indicator ADF6 Analog Input, Piher Position Sensor Pin 9 – ADF Indicator ADF7 Analog Input, Piher Position Sensor Pin 10 – ADF Indicator ADF8 Analog Input, Piher Position Sensor Pin 11 – Lamp Pin 12 – + 5v. Pin 13 – NC Pin 14 – NC CN29 Heading Indicator Pin 1 – Ground Pin 2 – +5v. X Pin 3 – Heading Indicator HED1 Digital Output Servo Signal Pin 4 – HED2 Digital Output Servo Signal (Not Used) Pin 5 – Heading Indicator HED3 Digital Input (Rotary Encoder) Pin 6 – Heading Indicator HED4 Digital Input (Rotary Encoder) Pin 7 – Heading Indicator HED5 Analog Input, Piher Position Sensor Pin 8 – Heading Indicator HED6 Analog Input, Piher Position Sensor Pin 9 – Heading Indicator HED7 Analog Input, Piher Position Sensor Pin 10 – Heading Indicator HED8 Analog Input, Piher Position Sensor Pin 11 – Lamp Pin 12 – + 5v. Pin 13 – NC Pin 14 – NC CN30 Altimeter Pin 1 – Ground Pin 2 – +5v. X Pin 3 – Altimeter ALT1 Digital Output Servo Signal, drives Modified Servo for 100 feet pointer Pin 4 – Altimeter ALT2 Digital Output Servo Signal, drives Servo for pressure scale Pin 5 – Altimeter ALT3 Digital Input (Rotary Encoder) Pin 6 – Altimeter ALT4 Digital Input (Rotary Encoder) Pin 7 – Altimeter ALT5 Analog Input, Piher Position Sensor, for position of 10,000 feet pointer Pin 8 – Altimeter ALT6 Analog Input, Piher Position Sensor, for position of 100 feet pointer Pin 9 – Altimeter ALT7 Analog Input, Piher Position Sensor or Photo Interruptor, for position of 10,000 feet pointer Pin 10 – Altimeter ALT8 Analog Input, Piher Position Sensor, for position of 100 feet pointer Pin 11 – Lamp Pin 12 – + 5v. Pin 13 – NC Pin 14 – NC
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CN31 Warning Lights & Switch Pin 1 – Ground Pin 2 – +5v. X Pin 3 – Warning Lights & Switch WAR1 Digital Output, Left Fuel Pin 4 – Warning Lights & Switch WAR2 Digital Output, Low Fuel Pin 5 – Warning Lights & Switch WAR3 Digital Output, Right Fuel Pin 6 – Warning Lights & Switch WAR4 Digital Output, Oil Press Pin 7 – Warning Lights & Switch WAR5 Digital Output, Left Vacuum Pin 8 – Warning Lights & Switch WAR6 Digital Output, VAC Pin 9 – Warning Lights & Switch WAR7 Digital Output, Right Vacuum Pin 10 – Warning Lights & Switch WAR8 Digital Output, Volts Pin 11 – Warning Lights & Switch WAR9 Digital Input, TEST – if connected to Ground all lights will go on. Pin 12 – Warning Lights & Switch WAR10 Digital Input, DIM – if connected to Ground all lights will dim. Pin 13 – Warning Lights & Switch WAR11 Digital Output, Line Pin 14 – + 5v. CN32 Servo expansion (connects to servo expansion board) Pin 1 – Ground Pin 2 – +5v. X Pin 3 – AUT1 Digital Output Pin 4 – AUT2 Digital Output Pin 5 – AUT3 Digital Output Pin 6 – AUT4 Digital Output Pin 7 – AUT5 Digital Output Pin 8 – AUT6 Digital Output Pin 9 – AUT7 Digital Output Pin 10 – AUT8 Digital Output Pin 11 – AUT9 Digital Input (Not Used) Pin 12 – AUT10 Digital Input (Not Used) Pin 13 – Lamp Pin 14 – + 5v. CN33 Circuit breakers (4 outputs, 15 inputs) Pin 1 – Ground Pin 2 – CB1 Digital Output Signal is output as a 4 bit value and is decode by the Pin 3 – CB2 Digital Output Circuit Breakers circuitry to control up to 15 CB’s. Pin 4 – CB3 Digital Output The value of the 4 bits must be applied during 300 Pin 5 – CB4 Digital Output milliseconds in order for the CB to pop out. Pin 6 – CB5 Digital Input, AVN FAN Pin 7 – CB6 Digital Input, AUTO PILOT Pin 8 – CB7 Digital Input, GPS Pin 9 – CB8 Digital Input, NAV COM1 Pin 10 – CB9 Digital Input, NAV COM2 Pin 11 – CB10 Digital Input, ADF Pin 12 – CB11 Digital Input, XPNDR Pin 13 – CB12 Digital Input, FLAP Pin 14 – CB13 Digital Input, INST Pin 15 – CB14 Digital Input, AVN BUS1 Pin 16 – CB15 Digital Input, AVN BUS2 Pin 17 – CB16 Digital Input, TURN COORD Pin 18 – CB17 Digital Input, INST LTS Pin 19 – CB18 Digital Input, ALT FLD Pin 20 – CB19 Digital Input, WARN
Output table: CB4 CB3 CB2 CB1 0 0 0 0 - No circuit breakers 0 0 0 1 - AVN FAN 0 0 1 0 - AUTO PILOT 0 0 1 1 - GPS 0 1 0 0 - NAV COM1 0 1 0 1 - NAV COM2 0 1 1 0 - ADF 0 1 1 1 - XPNDR 1 0 0 0 - FLAP 1 0 0 1 - INST 1 0 1 0 - AVN BUS1 1 0 1 1 - AVN BUS2 1 1 0 0 - TURN COORD 1 1 0 1 - INST LTS 1 1 1 0 - ALT FLD 1 1 1 1 - WARN
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CN34 Switches (16 inputs) Pin 1 – Ground Pin 2 – +5v. X Pin 3 – Switches SW1 Digital Input Pin 4 – Switches SW2 Digital Input Fuel Pump, OFF when Grounded Pin 5 – Switches SW3 Digital Input BCN, OFF when Grounded Pin 6 – Switches SW4 Digital Input Land, OFF when Grounded Pin 7 – Switches SW5 Digital Input Taxi, OFF when Grounded Pin 8 – Switches SW6 Digital Input Nav, OFF when Grounded Pin 9 – Switches SW7 Digital Input Strobe, OFF when Grounded Pin 10 – Switches SW8 Digital Input Pitot Heat, OFF when Grounded Pin 11 – Switches SW9 Digital Input Alt Static Air, OFF when Grounded Pin 12 – Switches SW10 Digital Input (Not Used) Pin 13 – Switches SW11 Digital Input (Not Used) Pin 14 – Switches SW12 Digital Input (Not Used) Pin 15 – Switches SW13 Digital Input (Not Used) Pin 16 – Switches SW14 Digital Input (Not Used) Pin 17 – Switches SW15 Digital Input (Not Used) Pin 18 – Switches SW16 Digital Input (Not Used) Pin 19 – NC Pin 20 – NC CN35 Servo Ctrld. Fuel Left/Right *) Pin 1 – Ground Pin 2 – +5v X Pin 3 – Fuel SFL1 Digital Output Servo Signal Pin 4 – Ground Pin 5 – +5v X Pin 6 – Fuel SFL2 Digital Output Servo Signal Pin 7 – Ground Pin 8 – Lamp Pin 9 – NC Pin 10 – NC CN36 Servo Ctrld. EGT/Fuel Flow *) Pin 1 – Ground Pin 2 – +5v X Pin 3 – EGT/Fuel Flow SEC1 Digital Output Servo Signal Pin 4 – Ground Pin 5 – +5v X Pin 6 – EGT/Fuel Flow SEC2 Digital Output Servo Signal Pin 7 – Ground Pin 8 – Lamp Pin 9 – NC Pin 10 – NC CN37 Servo Ctrld. Oil Temp/Pressure *) Pin 1 – Ground Pin 2 – +5v X Pin 3 – Oil Temp/Pressure SOP1 Digital Output Servo Signal Pin 4 – Ground Pin 5 – +5v X Pin 6 – Oil Temp/Pressure SOP2 Digital Output Servo Signal Pin 7 – Ground Pin 8 – Lamp Pin 9 – NC Pin 10 – NC
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CN38 Servo Ctrld. Suction G./AMM. Indicator *) Pin 1 – Ground Pin 2 – +5v X Pin 3 – Suction G./AMM SSA1 Digital Output Servo Signal Pin 4 – Ground Pin 5 – +5v X Pin 6 – Suction G./AMM SSA2 Digital Output Servo Signal Pin 7 – Ground Pin 8 – Lamp Pin 9 – NC Pin 10 – NC
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5. Schematics The following schematics are included in this document: Central Control Unit version 2. Attitude Indicator Altimeter / ADF / Heading Indicator (combined PCB for 3 different gauges) Altimeter / ADF / Heading Indicator with Zero Indicator (combined PCB for 3 different gauges) Circuit Breakers Digital Clock Dual Small Gauge General Instrument (Airspeed, Vertical Speed, Tachometer) Turn & Bank Indicator VOR1 + VOR2 Warning Panel Wet Compass
6. Wiring Diagrams The following wiring diagrams are included in this document:
Keylock Starter Switch
Cable Yoke
Cable Trim Wheel
Cable Throttle, Mixture, Propeller and Flaps
Cable Tank Switch
Cable Master Switches, Light Regulation, Gear Switch and Indicators
Cable Rudder Pedals
D0
D1
D2
D3
D4
D5
D6
D7
+3.3V
+3.3V
+3.3V
+5V
+5V
+5V
+5V
+5V
+3.3V +3.3V+3.3V
+5X
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5X
+5X
+5V
+3.3V
+12X
+5V +5V +5V +5V +5V+5V+5V
+5V
+12X
SEL0SEL1
SEL2
SEL4
SEL5
SEL6
SEL3
SEL8SEL9
SEL10SEL11
SEL12SEL13
SEL14SEL15
FLR1
FLR2
EGT1
EGT2
OTP1
OTP2
SAM1
SAM2
THR
MIX
PRP
FLA2
RUD1
RUD2
RUD3
RUD4
RUD5
YOK3
YOK4
CMP2
TRW4
THR2
VOR4
VOR5
ADF5
ADF6
HED5
HED6
ALT5
ALT6
ALT7
ALT8
ADCCS
ADCCK
ADCAD
ADCCS
ADCAD
ADCCK
ADCCS
ADCAD
ADCCK
ADCCS
ADCAD
ADCCK
lamp
POTM
DCS4
DCS5
DCS6
DCS7
VOR8
VOR9
D[0..7]
ADF7
ADF8
HED7
HED8
CMP3
MIX2
PRP2
Date Page of2004 TRC Development b.v. - Netherlandsc
Rev. Board RemarksO
0.6 240402 PC02081.0 170502 PC02152.0 241203 PC0338
CCU-2BS/OntwerpBS/DiverseBS/CN14+5V,IC5+12V,etc.
41Date Page of2004 TRC Development b.v. - Netherlandsc
Rev. Board RemarksO
0.6 240402 PC02081.0 170502 PC02152.0 241203 PC0338
CCU-2BS/OntwerpBS/DiverseBS/CN14+5V,IC5+12V,etc.
41Date Page of2004 TRC Development b.v. - Netherlandsc
Rev. Board RemarksO
0.6 240402 PC02081.0 170502 PC02152.0 241203 PC0338
CCU-2BS/OntwerpBS/DiverseBS/CN14+5V,IC5+12V,etc.
41
* = option
Patch below present on all CCU's delivered as from May 4, 2004.
1
2
3
4
5 6
+5V
GND
GND
+12Vyellow
red
black
NC
DiskdriveCN42h
+5V
GND
GND
+12Vyellow
red
black
NC
DiskdriveCN42h
EOC19
ADDR17
CLK18
A5 6
A6 7
A7 8
CS15
Dout16
Vcc
20
Vss
10
A0 1
A1 2
A2 3
A3 4
A4 5
A8 9
A9 11
A10 12
Ref+14
Ref-13
TLC1543CIC8 TLC1543CIC8
5 6IC9IC9
10k0R1810k0R18
1
2
3
4 +5V
GND
GND
+12Vyellow
red
black
DiskdriveCN42r
+5V
GND
GND
+12Vyellow
red
black
DiskdriveCN42r
1u00C39
25V1u00C39
25V
32x20KV1 32x20KV1
PM3PM3
27p0
C30
27p0
C30
9 8IC9IC9
10k0R2310k0R23
A17
A06 DAC5 14
DAC6 15
DAC7 16
SDA3
SCL4
NC5
DAC0 9
DAC1 10
DAC2 11
DAC3 12
DAC4 13
Vmax2
Vcc
1
Vee
8
TDA8444TIC5 TDA8444TIC5
12IC9IC9
10k0R910k0R9
1u00C38
25V1u00C38
25V
3k30R6
06033k30
R6
0603
12McXT112McXT1
1u00C36
25V1u00C36
25V
10k0R1410k0R14
1k50
R5
08051k50
R5
0805
11 10IC9IC9
10n0C3510n0C35
EOC19
ADDR17
CLK18
A5 6
A6 7
A7 8
CS15
Dout16
Vcc
20
Vss
10
A0 1
A1 2
A2 3
A3 4
A4 5
A8 9
A9 11
A10 12
Ref+14
Ref-13
TLC1543CIC7 TLC1543CIC7
PM2PM2
10k0R110k0R1
1u00C41
25V
*1u00C41
25V
*
10k0R2110k0R21
10k0R1210k0R12
10n0
C7
10n0
C7
10n0
C2
10n0
C2
13 12
IC9IC9
10k0R1710k0R17
220uC37
6V3220uC37
6V3
10k0R1910k0R19
PM1PM1
10n0
C9
10n0
C9
10n0
C26
10n0
C26
220uC40
6V3
*220uC40
6V3
*
Vss
7
Vcc
14
IC9 74AHCT14IC9 74AHCT14
Vcc
8
SDA5
Vss
4
A2 3TST7
A1 2
A0 1
SCL6
M24C02IC3 M24C02IC3
redLD1redLD1
10k0R1010k0R10
27p0
C31
27p0
C31
10n0
C27
10n0
C27
10k0R1110k0R11
EOC19
ADDR17
CLK18
A5 6
A6 7
A7 8
CS15
Dout16
Vcc
20
Vss
10
A0 1
A1 2
A2 3
A3 4
A4 5
A8 9
A9 11
A10 12
Ref+14
Ref-13
TLC1543CIC6 TLC1543CIC6
10n0C3410n0C34
470ER2470ER2
Vcc
24
Vss
12
A023
E119E018
A122
A221
A320
Y0 1
Y1 2
Y2 3
Y3 4
Y4 5
Y5 6
Y6 7
Y7 8
Y8 9
Y9 10
Y10 11
Y11 13
Y12 14
Y13 15
Y14 16
Y15 17
74HCT154IC2 74HCT154IC2
10n0
C28
10n0
C28
10k0R810k0R8
10k0R2210k0R22
10n0
C29
10n0
C29
27E0
R4
080527E0
R4
0805
Reset25
AVcc21
AGND18
XTALin19
XTALout20
PC7 / RD 41
PC6 / WR 40
BKPT61
Discon 1
EA24
D048
A07
PSEN80
A18
A29
A310
A411
A512
A615
A716
A826
A927
A1028
A1129
A1234
A1335
A1436
A1537
D149
D250
D351
D457
D558
D659
D760
CLK244
PC0 / RxD0 30
PC1 / TxD0 31
PC2 / INT0 32
PC3 / INT1 33
PC4 / T0 38
PC5 / T139
PB0 / T2 44
PB1 / T2EX 45
PB2 / RxD1 46
PB3 / TxD1 47
PB4 / INT4 52
PB5 / INT5 53
PB6 / INT6 54
PB7 / T2out 55
SDA 64
SCL 65
Wakeup 66
Vcc
2
Vcc
22
Vcc
42
Vcc
62
Vss
3
Vss 5Vss 6Vss 13Vss 14Vss 17
Vss
23
Vss
43
Vss 56
Vss
63
Vss 72Vss 78
USBD- 77
USBD+ 79
PA0 / T0out 68
PA1 / T1out 69
PA2 / OE 70
PA3 / CS 71
PA4 / FWR 73
PA5 / FRD 74
PA6 / RxD0out 75
PA7 / RxD1out 76
NC67
AN2131QIC1 AN2131QIC1
10k0R1310k0R13
10n0
C3
10n0
C3
1
2
3
4
CN43ProgramCN43Program
1u00C45
25V
*1u00C45
25V
*
1u00C32
25V1u00C32
25V
10k0R2010k0R20
1u00C44
25V
*1u00C44
25V
*
In 1
-
2
Out8
Ref
3
-
6
-
7
On 4nc5
MC33375-3.3VIC4MC33375-3.3VIC4
1u00C33
25V1u00C33
25V1
2
3
4
3888
D-
D+
T
+
CN41USB-B
D-
D+
T
+
CN41USB-B
10n0
C6
10n0
C6
100kR120100kR120
1u00C43
25V
*1u00C43
25V
*
10n0
C5
10n0
C5
220uC46
6V3
*220uC46
6V3
*
3k30R7
06033k30R7
0603
10n0
C8
10n0
C8
1u00C42
25V
*1u00C42
25V
*
10k0R1610k0R16
3 4IC9IC9
27E0
R3
080527E0
R3
0805
TIP120T1TIP120T1
D0D0
D4
D3
D6
D2
D1 D1
D5
D7
D4
D0
D3 D3
D7
D2
D5
D6
D1
D5
D7
D2
D4
D6
D0
D1
D2
D3
D4
D5
D6
D7
D0
D1
D2
D3
D4
D5
D6
D7
D0
D1
D2
D3
D4
D5
D6
D7
D0
D1
D2
D3
D4
D5
D6
D7
+5V +5V +5V
+5V +5V
+5V
+5V
SEL0 SEL1 SEL2
FLA1
TRW1
YOK1
YOK2
CMP1
AIR1
TACH
VSPD
ATT1
ATT2
TRN1
TRN2
VOR1
VOR2
VOR3
VOR6
VOR7
ADF1
ADF2
HED1
HED2
SEL2SEL1SEL0
SEL5
SEL3
QCNT
CB1
CB2
CB3
CB4
AUT1
AUT2
AUT3
AUT4
AUT5
AUT6
AUT7
AUT8
WAR1
WAR2
WAR3
WAR4
WAR5
WAR6
WAR7
WAR8
D[0..7]
ALT1
ALT2
VORx
WAR11
SEL3
SOP2
SEL4
SOP1
SEC1
SEC2
SEL6
SSA1
SSA2
SFL1
SFL2
GEAR1
GEAR2
SEL5
Date Page of2004 TRC Development b.v. - Netherlandsc
Rev. Board RemarksO
0.6 240402 PC02081.0 170502 PC02152.0 241203 PC0338
CCU-2BS/OntwerpBS/DiverseBS/CN14+5V,IC5+12V,etc.
42Date Page of2004 TRC Development b.v. - Netherlandsc
Rev. Board RemarksO
0.6 240402 PC02081.0 170502 PC02152.0 241203 PC0338
CCU-2BS/OntwerpBS/DiverseBS/CN14+5V,IC5+12V,etc.
42Date Page of2004 TRC Development b.v. - Netherlandsc
Rev. Board RemarksO
0.6 240402 PC02081.0 170502 PC02152.0 241203 PC0338
CCU-2BS/OntwerpBS/DiverseBS/CN14+5V,IC5+12V,etc.
42
* = option
OE11 OE2 19
IC1174HCT541IC1174HCT541
1k80R341k80R34
OE11 OE2 19
IC1574HCT541IC1574HCT541
4 17
5 16
9 11
4 16
6 14
1k80R401k80R40
9 11
3 17
Vcc
20
Vss
10
1k80R421k80R42
1k80R551k80R55
Vcc
20
Vss
10
3 18
6 15
Vcc
20
Vss
10
10n0
C16
10n0
C16
1k80R381k80R38
7 13
OE11 OE2 19
IC1074HCT541IC1074HCT541
4 16
2 18
5 15
7 14
5 16
1k80R351k80R35
10n0
C14
10n0
C14
8 12
1k80R511k80R51
Vcc
20
Vss
10
5 15
1k80R541k80R54
1k80R291k80R29
2 18
1k80R461k80R46
1k80R281k80R28
1k80R301k80R30
10n0
C11
10n0
C11
3 17
1k80R271k80R27
1k80R471k80R47
8 13
6 15
9 11
1k80R481k80R48
OE11 OE2 19
IC1374HCT541IC1374HCT541
3 17
1k80R451k80R45
6 146 14
10n0
C10
10n0
C10
1k80R261k80R26
1k80R311k80R31
4 16
4 16
7 14
1k80R361k80R36
9 12
1k80R441k80R44
1k80R531k80R53
10n0
C15
10n0
C15
1k80R391k80R39
7 13
2 18
1k80R491k80R49
1k80R411k80R41
5 15
5 15
1k80R251k80R25
1k80R321k80R32
OE11 OE2 19
IC1274HCT541IC1274HCT541
8 13
Vcc
20
Vss
10
7 13
2 18
1k80R241k80R24
6 14
2 19
8 12
3 17
LE11 OE 1
IC1674HCT573IC1674HCT573
6 14
7 13
9 12
1k80R331k80R33
1k80R431k80R43
Vcc
20
Vss
10
1k80R371k80R37
4 17
9 11
8 12
4 16
1k80R521k80R52
7 13
8 12
3 17
Vcc
20
Vss
10
1k80R501k80R50
9 11
3 18
2 19
10n0
C13
10n0
C13
LE11 OE 1
IC1474HCT573IC1474HCT573
5 15
8 12
2 18
10n0
C12
10n0
C12
D4
D1
D5
D4
D0
D7
D1
D5
D0
D2 D2
D5
D6
D7
D3
D5
D3
D4
D3
D2D2
D1
D3
D1
D3
D6
D0
D0
D6
D0
D7
D2
D5
D0
D7
D3
D7
D7
D1
D2
D0
D5
D0
D1
D2
D1
D6 D6 D6
D1
D5
D6
D4
D4
D7
D3
D6
D3
D2
D4 D4
D7
D5
D4
+5V+5V+5V+5V
+5V+5V+5V+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V +5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V +5V
+5V
+5V
+5V
+5V
+5V
+5V
HNDB
AVSW
MSW1
MSW2
FSS1
FSS2
FSS3
FSS4 CB12
SW10
CB19
SW2
CB8
SW14
SW15
DCS1
ALT3
STA3
AUT9
TRW2
CB18
SW1 SW9
SW4
HED3
CB14
STA1
AUT10
CB15
WAR9
SW3
CB6
HED4
STA2
SW8
SW6
CB9
CB16
TRW3
SW13
ALT4
CB13
WAR10
DCS3
CB17
CB5
SW16
SW12
SW11
CB7
DCS2
STA4
SW7
SW5
CB11
CB10
SEL15 SEL15SEL14 SEL14SEL13 SEL13SEL12 SEL12
SEL9SEL8 SEL8
D[0..7]
SEL11 SEL11SEL10 SEL10SEL9
ADF3
ADF4
GEAR3
Date Page of2004 TRC Development b.v. - Netherlandsc
Rev. Board RemarksO
0.6 240402 PC0208PC0215
2.0 241203 PC0338
CCU-2BS/OntwerpBS/DiverseBS/CN14+5V,IC5+12V,etc.
43
1705021.0
Date Page of2004 TRC Development b.v. - Netherlandsc
Rev. Board RemarksO
0.6 240402 PC0208PC0215
2.0 241203 PC0338
CCU-2BS/OntwerpBS/DiverseBS/CN14+5V,IC5+12V,etc.
43
1705021.0
Date Page of2004 TRC Development b.v. - Netherlandsc
Rev. Board RemarksO
0.6 240402 PC0208PC0215
2.0 241203 PC0338
CCU-2BS/OntwerpBS/DiverseBS/CN14+5V,IC5+12V,etc.
43
1705021.0
* = option
47k0R6147k0R61
47k0R6647k0R66
416
515
10n0
C22
10n0
C22
416
911
47k0R11247k0R112
47k0R8047k0R80
713
47k0R9147k0R91
614
47k0R11947k0R119
47k0R5747k0R57
Vcc
20
Vss
10
317
47k0R11847k0R118
47k0R10847k0R108
10n0
C24
10n0
C24
OE11 OE2 19
IC2374HCT541IC2374HCT541
OE11 OE2 19
IC1974HCT541IC1974HCT541
515
614
47k0R10447k0R104
515
911
317
47k0R10047k0R100
10n0
C18
10n0
C18
713
218
218
47k0R7647k0R76
47k0R11747k0R117
47k0R8547k0R85
OE11 OE2 19
IC2574HCT541IC2574HCT541
47k0R9647k0R96
614
47k0R6247k0R62
47k0R6747k0R67
614
713
47k0R11347k0R113
47k0R8147k0R81
47k0R7247k0R72
47k0R5847k0R58
Vcc
20
Vss
10
812
416
317
47k0R10947k0R109
218
47k0R8847k0R88
218
10n0
C21
10n0
C21
Vcc
20
Vss
10
713
OE11 OE2 19
IC2074HCT541IC2074HCT541
47k0R10547k0R105
713
812
515
47k0R10147k0R101
911
Vcc
20
Vss
10
515
416
317
47k0R8647k0R86
47k0R7747k0R77
47k0R6347k0R63
47k0R6847k0R68
47k0R9747k0R97
812 812
911
47k0R7347k0R73
47k0R11447k0R114
47k0R8247k0R82
47k0R6447k0R64
47k0R5947k0R59
317
614
10n0
C23
10n0
C23
614
515
Vcc
20
Vss
10
47k0R11047k0R110
317
416
47k0R8947k0R89
10n0
C19
10n0
C19
47k0R8747k0R87
911
47k0R10647k0R106
911
218
812
47k0R10247k0R102
OE11 OE2 19
IC2274HCT541IC2274HCT541
614
713
515
416
47k0R7847k0R78
OE11 OE2 19
IC2474HCT541IC2474HCT541
10n0
C25
10n0
C25
47k0R6947k0R69
47k0R9847k0R98
47k0R7447k0R74
47k0R11547k0R115
47k0R8347k0R83
47k0R6047k0R60
47k0R6547k0R65
218
416
218
713
812
812
47k0R11147k0R111
47k0R5647k0R56
614
47k0R9047k0R90
Vcc
20
Vss
10
218
OE11 OE2 19
IC1874HCT541IC1874HCT541
10n0
C20
10n0
C20
47k0R10747k0R107
OE11 OE2 19
IC2174HCT541IC2174HCT541
Vcc
20
Vss
10
317
47k0R10347k0R103
317
911
911
713
515
812
47k0R7947k0R79
416
47k0R7047k0R70
47k0R9947k0R99
47k0R8447k0R84
Vcc
20
Vss
10
47k0R7547k0R75
47k0R11647k0R116
+5X
+5X
+5X
+5X
+5X
+5X
+5X
+5X
+5X
+5X+5X
+5X
+5X
+5X
+5X
+5X
+5X
+5X
+5X
+5X
+5X
+5X
+5X
+5X
+5X
+5X
+5X
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5X
HNDB
AVSW
THR
FLR1
lamp
EGT1
lamp
OTP1
lamp
SAM1
lamp
PRP
POTM
lamp
MSW2
FSS1
FSS3FSS2
DCS2
DCS4
DCS6
lamp DCS1
DCS3
DCS5
DCS7
FSS4
TRW1
FLA2
TRW3
TRW2
FLA1
RUD1
RUD3 RUD4
RUD2
RUD5
STA1 STA2
STA4STA3
YOK1
YOK3 YOK4
YOK2
CMP1 CMP2
CMP3
lamp
AIR1
TACH
VSPD
ATT1
TRN1
VOR1
VOR3
VOR5
AUT9
AUT7
AUT5
AUT3
AUT1
WAR9
WAR7
WAR5
WAR3
WAR1
lamp
ALT7
ALT5
ALT3
ALT1
ADF3
ADF1
VOR6 VOR7
lamp
ADF2
HED2
HED4
HED6
lamp
lamp
HED1
HED3
HED5
ALT2
ALT4
ALT6
ALT8
WAR2
WAR4
WAR6
WAR8
WAR10
ATT2
lamp
TRN2
lamp
VOR2
VOR4
lamp
AUT2
AUT4
AUT6
AUT8
AUT10
CB2
CB4
CB6
CB8
CB10
CB12
CB14
CB16
CB18
SW1
SW3
SW5
SW7
SW9
SW11
SW13
SW15
CB1
CB3
CB5
CB7
CB9
CB11
CB13
CB15
CB17
CB19
SW2
SW4
SW6
SW8
SW10
SW12
SW14
SW16
lamp
lamp
lamp
lamp
lamp
SSA2
SOP2
SEC2
SFL2
SFL1
SEC1
SOP1
SSA1
VOR9
HED8HED7
lamp
ADF4
ADF6
ADF8
ADF5
ADF7
lamp
VOR8VORx
WAR11
MIX2
GEAR2
THR2
PRP2
MIX
TRW4
SAM2
OTP2
EGT2
FLR2
MSW1
QCNT
GEAR3
GEAR1
lamp
Date Page of2004 TRC Development b.v. - Netherlandsc
Rev. Board RemarksO
0.6 240402 PC02081.0 170502 PC02152.0 241203 PC0338
CCU-2BS/OntwerpBS/DiverseBS/CN14+5V,IC5+12V,etc.
44Date Page of2004 TRC Development b.v. - Netherlandsc
Rev. Board RemarksO
0.6 240402 PC02081.0 170502 PC02152.0 241203 PC0338
CCU-2BS/OntwerpBS/DiverseBS/CN14+5V,IC5+12V,etc.
44Date Page of2004 TRC Development b.v. - Netherlandsc
Rev. Board RemarksO
0.6 240402 PC02081.0 170502 PC02152.0 241203 PC0338
CCU-2BS/OntwerpBS/DiverseBS/CN14+5V,IC5+12V,etc.
44
* = option
Future Expansion
Future Expansion.
Future Expansion
Future Expansion
Master switch
Quartz counter
Dimmer
Handbrake
Avionics switch
Gears
LAMP connection present on all CCU's delivered as from May 4, 2004. -->
1 2
3 4
5 6
7 8
9 10
11
13
12
14
CN28ADF indicatorCN28ADF indicator
1 2
3 4
5 6
7 8
9 10
CN15FlapsCN15Flaps
1 2
3 4
5 6
7 8
9 10
CN22TachometerCN22Tachometer
1 2
3 4
5 6
7 8
9 10
11
13
12
14
15 16
17 18
19 20
CN33Circuit breakersCN33Circuit breakers
1 2
3 4
5 6
7 8
9 10
CN19YokeCN19Yoke
1 2
3 4
5 6
7 8
9 10
CN26VOR1 indicatorCN26VOR1 indicator
1 2
3 4
5 6
7 8
9 10
11
13
12
14
CN30AltimeterCN30Altimeter
1 2
3 4
5 6
7 8
9 10
CN16Trim wheelCN16Trim wheel
1 2
3 4
5 6
7 8
9 10
CN23Vertical speed ind.CN23Vertical speed ind.
1 2
3 4
5 6
7 8
9 10
CN13Fuel sel. + shut offCN13Fuel sel. + shut off
1 2
3 4
5 6
7 8
9 10
CN20CompassCN20Compass
1 2
3 4
5 6
7 8
9 10
11
13
12
14
CN29Heading ind.CN29Heading ind.
1 2
3 4
5 6
7 8
9 10
CN27VOR2 indicatorCN27VOR2 indicator
1 2
3 4
5 6
7 8
9 10
CN35S-Fuel Left/RightCN35S-Fuel Left/Right
1 2
3 4
5 6
7 8
9 10
11
13
12
14
CN31Warning lights + switchCN31Warning lights + switch
1 2
3 4
5 6
7 8
9 10
CN17Starter switchCN17Starter switch
1 2
3 4
5 6
7 8
9 10
CN24Attitude indicatorCN24Attitude indicator
1 2
3 4
5 6
7 8
9 10
11
13
12
14
15 16
17 18
19 20
CN34SwitchesCN34Switches
1 2
3 4
5 6
7 8
9 10
CN14Digital ClockCN14Digital Clock
1 2
3 4
5 6
7 8
9 10
CN21Airspeed ind.CN21Airspeed ind.
1 2
3 4
5 6
7 8
9 10
11
13
12
14
CN32Future Servo ExpansionCN32Future Servo Expansion
1 2
3 4
5 6
7 8
9 10
11
13
12
14
15 16
17 18
19 20
CN12CN12
1 2
3 4
5 6
7 8
9 10
CN38S-Suction G./AM ind.CN38S-Suction G./AM ind.
1 2
3 4
5 6
7 8
9 10
CN37S-Oil temp./PressureCN37S-Oil temp./Pressure
1 2
3 4
5 6
7 8
9 10
CN18Rudder pedalsCN18Rudder pedals
1 2
3 4
5 6
7 8
9 10
11
13
12
14
15 16
17 18
19 20
CN11CN11
1 2
3 4
5 6
7 8
9 10
CN25Turn coordinatorCN25Turn coordinator
1 2
3 4
5 6
7 8
9 10
CN36S-EGT/Cyl. head temp.CN36S-EGT/Cyl. head temp.
1
2
3
1
2
3
+5v
+5v
Servo A Connector (Roll)
Servo B Connector (Pitch)
Roll (Servo A)
Pitch (Servo B)
1
3
5
7
9
2
4
6
8
10Lamp
+5v.
+5v.
To CN 24 of CCU via Ribbon cable
Copyright 2003 TRC Development b.v. - Netherlands
Rev. Date Board Remarks Page 1 of 1
Attitude Indicator1.0 230603 CR/Design
+5X
+5X
+5X
+5V
+5V +5V
+5V +5V
+5V+5V
+5V +5V
+5V
+5V
+5V
+5V
Date Page of2003 TRC Development b.v. - The Netherlandsc
Rev. Board RemarksO
0 130502 PC0211 1 280502 PC0218
ALT+ADFB S/DesignBS/connectors
11* option
10k0P1
top
1M00R7
1206
*1M00R4
axial10k0P4
bot
StraightCN1Servo 1
1
2
3
CN4lamp*
FlatcableCN5
1 2
3 4
5 6
7 8
9 10
11
13
12
14
1M00R1
axial10k0P2
bot
1M00R8
1206
*
StraightCN2Servo 2
1
2
3
1M00R5
1206
*1M00R2
axial StraightCN3Rotary Encoder
1
2
3
10k0P3
top
1M00R6
1206
*
1M00R3
axial
+5X
+5V
+5V +5V
+5V +5V
+5V+5V
+5V +5V
+5V
+5V
+5V
+5V
+5X
+5X
+5V +5V
+5V+5V
Date Page ofC o p y r i g h t 2 0 0 3 T R C D e v e l o p m e n t b . v . - T h e N e t h e r l a n d sRev. Board R e m a r ks1 2 8 0 502 P C 0 2 182 1 8 0 7 02 P C 0 2 233 1 5 1 0 02 P C 0 2 29
1 6 1 2 024 P C 0 2 39
ALT+ADF -2 B S / c o n n ectorsB S / + 4 7 0 p F , 3 p . conn.B S / n u lsensorB S / C 3 m o v e d
11* o p tion
470pC4*
1206
10k0P1
top*
330ER10
axi al
*
470pC1
radial
AngleC N 2S e r v o 2
1
2
3
1M00R7
1 2 0 6
*1M00
R4
axial
*
1 0k0P4
bot
C N 4lamp*
F la t ca bleC N 5
1 2
3 4
5 6
7 8
9 10
11
13
12
14
4 k 7 0R 1 1
1 2 0 6
M M H FC N 6
1
2
3
4
5
6
1M00R1
axial
*
470pC2
radial
AngleC N 1S e r v o 1
1
2
3
1 0k0P2
bot
1M00R8
1 2 0 6
330ER9
1206
1M00R5
1 2 0 61M00
R2
axial
*
4 k 7 0R 1 2
axial
*
470pC3*
1206
10k0P3
top
*
AngleC N 3D i g i Pot
1
2
3
1M00R6
1 2 0 6
1M00R3
axial
*
+5V
+5V
+12V
+12V
+12V
+12V
+12V
+12V
+12V
+12V +12V +12X +12X
X X
+12V
+5V
+12X +12X
X X
X
X
X
X
X
X
+12X
+12X
+12X
+12X
+12X
+12X
+12Y +12Y
+12Y
+12Y
YY
Y
Y
+12V +12V +12V
CB1
CB2
CB3
CB4
CB5
CB6
CB7
CB8
CB9
CB10
CB11
CB12
CB13
CB14
CB15
CB16
CB17
CB18
CB19
CB2
CB4
CB6
CB8
CB10
CB12
CB14
CB16
CB18
CB1
CB3
CB5
CB7
CB9
CB11
CB13
CB15
CB17
CB19
Date Page ofc
Rev. Board RemarksO
0 241003 PC----
TRC circ. breakersBS/Ontwerp
11Date Page ofc
Rev. Board RemarksO
0 241003 PC----
TRC circ. breakersBS/Ontwerp
11Date Page of2003 TRC Development b.v. - The Netherlandsc
Rev. Board RemarksO
0 241003 PC----
TRC circ. breakersBS/Ontwerp
11* option
PCB 1 PCB 2 PCB 3
RY6RY6
7 10
IC3IC3
Vee
8
Vcc
9
ULN2003AIC2ULN2003AIC2
1 2
3 4
5 6
7 8
9 10
11
13
12
14
15 16
17 18
19 20
Boxed headerCN4Boxed headerCN4
RY9RY9
RY11RY11
R22R22
R36R36
1 16
IC3IC3
R3R3
R31R31
RY10RY10
R15R15
R43R43
RY14RY14
3 14
IC2IC2
RY1RY1
R1180E1206
R1180E1206
7 10
IC2IC2
R10R10
1
2
3
4+5V
GND
GND
+12Vyellow
red
black
Diskdrive ConnectorCN1
+5V
GND
GND
+12Vyellow
red
black
DiskdriveCN1
RY6RY6
3 14
IC4IC4
R19R19
R33R33
RY5RY5
R28R28
R45180E1206
R45180E1206
6 11
IC3IC3
RY7RY7
RY10RY10
RY9RY9
RY13RY13 RY13RY13
R12R12
R40R40
RY3RY3
4 13
IC3IC3
R7R7
R21R21
1 2
3 4
5 6
7 8
9 10
11
13
12
14
15 16
17 18
19 20
Boxed headerCN2Boxed headerCN2
Vee
8
Vcc
9
ULN2003AIC4ULN2003AIC4
2 15
IC2IC2
RY4RY4
R30R30
6 11
IC2IC2
RY4RY4
RY14RY14
R25R25
R42R42
RY12RY12
1 2
3 4
5 6
7 8
9 10
Boxed headerCN6Boxed headerCN6
RY15RY15
RY8RY8
4 13
IC4IC4
5 12
IC2IC2
7 10
IC4IC4
RY12RY12
5 12
IC3IC3
R9R9
R37R37
6 11
IC4IC4
R4R4
1 16
IC2IC2
R16R16
R27R27
RY8RY8
RY3RY3
1 2
3 4
5 6
7 8
9 10
Boxed headerCN5Boxed headerCN5
3 14
IC3IC3
1 2
3 4
5 6
7 8
9 10
11
13
12
14
15 16
17 18
19 20
Boxed headerCN3Boxed headerCN3
RY7RY7
RY1RY1
2 15
IC3IC3
R39R39
Vee
8
Vcc
9
ULN2003AIC3ULN2003AIC3
RY11RY11
R6R6
R34R34
2 15
IC4IC4
4 13
IC2IC2
RY2RY2
A02
Q2 10
OE23
A13
LE1
Vcc
24
Q3 8
Vss
12
Q6 5
A221
Q5 6
Q4 7
Q1 9
Q7 4
Q0 11
A322
Q9 17
Q14 16
Q13 13
Q11 19
Q12 14
Q10 20
Q8 18
Q15 15
74HC4514IC174HC4514IC1
R18R18
1 16
IC4IC4
RY15RY15
R24R24
5 12
IC4IC4
RY2RY2
RY5RY5R13R13
+5V
+5V
+5V
+5V
+5V
+5V
+5V
+5V
DCS3
DCS5
DCS1
DCS2
DCS4
DCS6
DCS4
DCS5
DCS6
DCS1
DCS2
DCS3
Date Page of2003 TRC Development b.v., Hollandc
Rev. Board RemarksO
0 291002 PC02321.1 280303 PC0305
Digital Clock 1BS/DesignBS/proc,knob,backl,p5<>7
11* option
39k0
R1
0603
SKHHCRSW2
IC23
14
Boxed headerCN1
1 2
3 4
5 6
7 8
9 10
3V3Z1 68k0
R12
0603
150k
R3
0603
10n0
C2
1E00R16
1206
220E
R14
0603
IC2 LPV321
Vee
2
Vcc
5
SKHHCRSW3
1u00C6
25V
*
12k0R6
0603
1u00
C3
25V
10k0
R13
0603
10k0
R4
0603
10n0
C4
D20291A0LCD1
S1 5
S2 6
S3 7
S4 8
S5 9
S6 10
S7 11
S8 12
S9 13
S10 14
S11 15
S12 16
S13 17
S14 18
S16 20S15 19
S17 21
C1 1
C2 2
C3 3
C4 4
A 23
K 22
1E00R17
1206
SKHHCRSW1
FCX789AT1
12k0
R2
0603
12k0R7
0603
100E
R9
0805
10k0R11
0603
68k0
R10
0603
1u00
C5
25V
MSM6775IC1
Vss
42
Vcc
32
SEG151
SEG252
SEG353
SEG454
SEG555
SEG656
SEG757
SEG858
SEG959
SEG1060
SEG1161
SEG1262
SEG1363
SEG1464
SEG1565
SEG1666
SEG1767
SEG1868
SEG1969
SEG2070
SEG2171
SEG2272
SEG2373
SEG2474
SEG2575
SEG2676
SEG2777
SEG2878
SEG2979
SEG3080
SEG3181
SEG3282
SEG3383
SEG3484
SEG3585
SEG3686
SEG3787
SEG3888
SEG3989
SEG4090
SEG4191
SEG4292
SEG4393
SEG4494
SEG4595
SEG4696
SEG4797
SEG4898
SEG4999
SEG50100
SEG511
SEG522
SEG533
SEG544
SEG555
SEG566
SEG577
SEG588
SEG599
SEG6010
SEG6111
SEG6212
SEG6313
SEG6414
SEG6515
SEG6616
SEG6717
SEG6818
SEG6919
SEG7020
SEG7121
SEG7222
SEG7323
SEG7424
SEG7525
SEG7626
SEG7727
SEG7828
SEG7929
SEG8030
COM150
COM249
COM348
COM447
COM546
NC 31
LOAD 33
CLOCK 34
DATA 35
BLANK 36
DSEL2 37
DSEL1 38
OSC-R 39
OSC-C 40
OSC-IN 41
VLC1 45
VLC2 44
VLC3 43
12k0R8
0603
*
12k0R5
0603
1E00R15
1206
1n00
C1
0805
1
2
3
1
2
3
+5v
+5v
Servo A Connector
Servo B Connector
Servo A
Servo B
1
3
5
7
9
2
4
6
8
10Lamp
+5v.
+5v.
To CN 13, CN14, CN15 or CN16
of CCU via Ribbon cable
Copyright 2003 TRC Development b.v. - Netherlands
Rev. Date Board Remarks Page 1 of 1
Dual SmallGauge1.0 230603 CR/Design
+5X
Ser vo Connector (Black wire = pin 3)
1
2
+5X
Date Page of2003 TRC Development b.v. - The Netherlandsc
Rev. Board RemarksO
0 280502 PC0213
Gen. Instr.B S/Design
11* option
CN3lamp*
3
via 10 wire ribbon cableConnected to CN21, CN 22 or CN23 of CCU
1 2
3 4
5 6
7 8
9 10
1
2
3
1
2
3
+5v
+5v
Servo A Connector (Turn Indicator)
Servo B Connector (Bank Indicator) Turn Coordinator
( Servo A)Airplane,
Bank Indicator (Ball, Servo B)
1
3
5
7
9
2
4
6
8
10Lamp
+5v.
+5v.
To CN 25 of CCU via Ribbon cable
Copyright 2003 TRC Development b.v. - Netherlands
Rev. Date Board Remarks Page 1 of 1
Turn & BankIndicator1.0 230603 CR/Design
Yellow
Black
Red
Yellow
Black
Red
+5V
+5V
+5V
+5X
+5X
+5X
+5X +5V+5V
+5V +5V
Date Page of2003 TRC Development b.v. - The Netherlandsc
Rev. Board RemarksO
0 130502 PC0210
VOR 1+2BS/Ontwerp
11* option
10k0P1
top
1M00R1
axial
AngleC N2Servo 2
1
2
3
1M00R2
axial10k0P2
bot
1M00R3
1206
*AngleC N3
Servo 3
1
2
3
FlatcableC N5
1 2
3 4
5 6
7 8
9 10
1M00R4
1206
*
AngleC N1Servo 1
1
2
3
CN4lamp*
+5X
+5V
+5V
+5V
+5V +5V +5V +5V +5V
+5V +5V +5V +5V +5V
+5V+5V +5V +5V +5V
+5V +5V+5V
+5V
+5V+5V +5V
+5V+5V
+5V
Date Page of2003 TRC Development b.v. - The Netherlandsc
Rev. Board RemarksO
0 130502 PC0213
WarningB S/Design
11* option
SW1
redLD20-TEST-
redLD19Volts
120ER9
0805
IC1
611
orangeLD4Low Fuel
IC2
1 16
IC2
5 12
120ER15
0805
IC1
1 16
120ER16
0805
redLD12Oil P.
120ER17
0805
IC1
710
redLD21-TEST-
120ER25
0805
120ER18
0805
120ER14
0805
orangeLD5Low Fuel
120ER22
0805
120ER19
0805
120ER7
0805
IC2
215
120ER3
0805
IC1
2 15
orangeLD1L LF
IC2
6 11
120ER4
0805
120ER24
0805
120ER13
0805
IC1 ULN2003A
Vcc
9
Vee
8
120ER10
0805
redLD8Oil P.
orangeLD16R VAC
120ER2
0805
redLD22-TEST-
orangeLD15VAC
IC1
3 14
orangeLD6Low Fuel
120ER20
0805
orangeLD14VAC
orangeLD2Low Fuel
IC2
3 14
120ER5
0805
redLD11Oil P.
IC2
7 10
redLD9Oil P.
120ER12
0805120ER8
0805
IC1
413
redLD23-TEST-
FlatcableC N1
1 2
3 4
5 6
7 8
9 10
11
13
12
14
120ER1
0805
orangeLD13L VAC
orangeLD7R LF
IC2 ULN2003A
Vcc
9
Vee
8
orangeLD3Low Fuel
redLD18VoltsIC2
413
120ER23
0805
IC1
5 12
redLD10Oil P.
120ER21
0805
120ER6
0805
redLD24-TEST-
redLD17Volts
redLD25-TEST-
120ER11
0805
+5V
+5V
+5V
+5V +5V
+5V+5V
+5X
+5X
Date Page of2003 TRC Development b.v. - The Netherlandsc
Rev. Board RemarksO
0 280502 PC0213
CompassB S/Design
11* option
10k0P1
top
CN3lamp*
StraightCN1Ser vo
1
2
3
1M00R1
axial
10k0P2
bot
1M00R4
1206
*
1M00R2
axial
FlatcableCN2
1 2
3 4
5 6
7 8
9 10
1M00R3
1206
*
10 pole flatcable connectorshown without strain relief
1
Starter Switch (Key Lock) connecting cable
4 wires cut off
To CN17
70 cm.
Rev. Date Remarks Product
1.1 01-09-2003 Key Lock Cable
1.2 01-10-2003 (Starter Switch)
Copyright 2003 TRC Development b.v. - Holland
1 wire cut offIndicator, keylock seen fro m the back side
10 pole flatcable connectorshown without strain relief
(cable not folded!)
1
Starter Switch (Key Lock) connecting cable + PCB
4 wires cut off
To CN17
70 cm.
1 wire cut off
Keylock seen from the back side
Rev. Date Remarks Product
1.1 22-03-2004 Key Lock Cable + PCB
(Starter Switch)
Copyright 2003 TRC Development b.v. - Holland
Starter Switch for Flight Simulators
Bottom View - connections 1(for general use)
10
Contact specificationsContact configurationRated current/Maximum peak current ARated voltage/Maximum switching voltage V ACRated load in AC1 VARated load in AC15 (230 VAC) VAStandard contact material
Technical dataMechanical life AC/DC cyclesElectrical life at rated load AC1 cyclesOperate/release time (bounce included) msInsulation according to EN 61810-5Insulation between contacts (1.2/50µs) kVDielectric strenght between open contacts V ACAmbient temperature range °CProtection category
1 CO (SPDT)16/30
250/400*4,000750
AgCdO
10 · 106/20 · 106100 · 103
10/10 - (15/12 sens.)3.6 kV/33 (4mm)
1,000–40…+85
IP 50
Thickness of possible front panel: 1 to 2,5 mm.
The Starter Switch for Flight Simulation is constructed around a Rotary Switch combined with high quality stainless steel mechanics
The Starter Switch has totally 5 positions, whereof the 5th position is spring returned to the 4th position. The 5th position functions as a starter position.
Once mounted, the key cannot be removed and is therefore safe for loss.
The switch functions are:
- OFF- Right Magneto- Left Magneto- Both Magnetos- Start (spring returned to position “Both”)
The Starter witch can be controlled from the Central Control Unit as offered by SimKits via connector CN17 on the CCU or from any existing electronics.
Mounting InstructionsThe Starter Switch comes assembled. To mount the switch into a panel, loosen the small screws on the copper bushing to release the key.Now loosen the nut from the Threaded Bush, and mount it in a panel, together with the metal parts as shown in the picture below. Do not forget to use the Round Mounting Ring.The panel hole must be 10 mm. (0,3937”). When the Starter Switch is mounted into the TRC472 panel, the Filler Ring with flattened edges should be used.
It is strongly recommended to turn the small screws properly towards the key. Note: the small screws must be screwed in equally to keep the key in the middle.Finalize the mounting by securing the screws with Locktite to avoid loosening during use.
Parts Number 871 722 802 34 91
All measurements are in millimeters.(1 Inch = 25.4 mm.)
Panel cut-out
Starter Switch for Flight Simulators
Bottom View - connections 1(for general use)
10
Contact specificationsContact configurationRated current/Maximum peak current ARated voltage/Maximum switching voltage V ACRated load in AC1 VARated load in AC15 (230 VAC) VAStandard contact material
Technical dataMechanical life AC/DC cyclesElectrical life at rated load AC1 cyclesOperate/release time (bounce included) msInsulation according to EN 61810-5Insulation between contacts (1.2/50µs) kVDielectric strenght between open contacts V ACAmbient temperature range °CProtection category
1 CO (SPDT)16/30
250/400*4,000750
AgCdO
10 · 106/20 · 106100 · 103
10/10 - (15/12 sens.)3.6 kV/33 (4mm)
1,000–40…+85
IP 50
Thickness of possible front panel: 1 to 2,5 mm.
The Starter Switch for Flight Simulation is constructed around a Rotary Switch combined with high quality stainless steel mechanics
The Starter Switch has totally 5 positions, whereof the 5th position is spring returned to the 4th position. The 5th position functions as a starter position.
Once mounted, the key cannot be removed and is therefore safe for loss.
The switch functions are:
- OFF- Right Magneto- Left Magneto- Both Magnetos- Start (spring returned to position “Both”)
The Starter witch can be controlled from the Central Control Unit as offered by SimKits via connector CN17 on the CCU or from any existing electronics.
Mounting InstructionsThe Starter Switch comes assembled. To mount the switch into a panel, loosen the small screws on the copper bushing to release the key.Now loosen the nut from the Threaded Bush, and mount it in a panel, together with the metal parts as shown in the picture below. Do not forget to use the Round Mounting Ring.The panel hole must be 10 mm. (0,3937”). When the Starter Switch is mounted into the TRC472 panel, the Filler Ring with flattened edges should be used.
It is strongly recommended to turn the small screws properly towards the key. Note: the small screws must be screwed in equally to keep the key in the middle.Finalize the mounting by securing the screws with Locktite to avoid loosening during use.
Parts Number 871 722 802 34 91
All measurements are in millimeters.(1 Inch = 25.4 mm.)
Panel cut-out
Starter Switch for Flight Simulators
Bottom View - connections 1(for general use)
10
Contact specificationsContact configurationRated current/Maximum peak current ARated voltage/Maximum switching voltage V ACRated load in AC1 VARated load in AC15 (230 VAC) VAStandard contact material
Technical dataMechanical life AC/DC cyclesElectrical life at rated load AC1 cyclesOperate/release time (bounce included) msInsulation according to EN 61810-5Insulation between contacts (1.2/50µs) kVDielectric strenght between open contacts V ACAmbient temperature range °CProtection category
1 CO (SPDT)16/30
250/400*4,000750
AgCdO
10 · 106/20 · 106100 · 103
10/10 - (15/12 sens.)3.6 kV/33 (4mm)
1,000–40…+85
IP 50
Thickness of possible front panel: 1 to 2,5 mm.
The Starter Switch for Flight Simulation is constructed around a Rotary Switch combined with high quality stainless steel mechanics
The Starter Switch has totally 5 positions, whereof the 5th position is spring returned to the 4th position. The 5th position functions as a starter position.
Once mounted, the key cannot be removed and is therefore safe for loss.
The switch functions are:
- OFF- Right Magneto- Left Magneto- Both Magnetos- Start (spring returned to position “Both”)
The Starter witch can be controlled from the Central Control Unit as offered by SimKits via connector CN17 on the CCU or from any existing electronics.
Mounting InstructionsThe Starter Switch comes assembled. To mount the switch into a panel, loosen the small screws on the copper bushing to release the key.Now loosen the nut from the Threaded Bush, and mount it in a panel, together with the metal parts as shown in the picture below. Do not forget to use the Round Mounting Ring.The panel hole must be 10 mm. (0,3937”). When the Starter Switch is mounted into the TRC472 panel, the Filler Ring with flattened edges should be used.
It is strongly recommended to turn the small screws properly towards the key. Note: the small screws must be screwed in equally to keep the key in the middle.Finalize the mounting by securing the screws with Locktite to avoid loosening during use.
Parts Number 871 722 802 34 91
All measurements are in millimeters.(1 Inch = 25.4 mm.)
Panel cut-out
Side View
33 mm.
65 mm.
TopView
Round Mounting Ring
Threaded Bush
12
3
4
5
678
9
10
1112
Co
mm
on
Filler ring with flattenededges for TRC 472 panel mounting.
Filler ring with flattenededges for TRC 472 panel mounting.
Connections 1 2 3 4 5 COff x xRight x xLeft x xBoth x xStart x x
Picture of Starter Switch,
mounted in TRC472 Panel.(Panel not included)
For Flight Simulation use, only pins 1 to 5(positions 6-12 are mechanically locked).
12
3
4
5
678
9
10
1112
Bottom View - connections 2(for use on the CCU1 or CCU2)
10 pole flatcable connectorshown without strain relief
(cable not folded!)
1
4 wires cut
To CN17
1 wire cut
Connection Table
Connector CN17 Starter SwitchPin 1 CommonPin 3 Pin 1Pin 4 Pin 2Pin 5 Pin 3Pin 6 Pin 5
Co
mm
on
10 pole flatcable connectorshown without strain relief
1
4 wires cut off
To CN19
2 x (separate) 50 cm. Shielded Audio cable
2 wires cut off
Top View Roll
Top View Pitch
Yoke connecting cable
Rev. Date Remarks Product
1.2 01-10-2003 Cable Yoke
1.3 29-04-2004
Copyright 2003 TRC Development b.v. - Holland
10 pole flatcable connectorshown without strain relief
1
Trim Wheel connecting cable
2
1 3
4 wires cut off
3 wires cut off
To CN16
Rev. Date Remarks Product
1.1 01-09-2003 Cable Trim Wheel
1.2 01-10-2003
Copyright 2003 TRC Development b.v. - Holland
10 pole flatcable connectorshown without strain relief
1
Flaps/Throttle/Mixture/Prop
To CN15
Rev. Date Remarks Product
1.0 29-04-2004 Cable Throttle/Mix/Prop
Copyright 2003 TRC Development b.v. - Holland
Throttle 1
Mixture 1
Prop 1
Th
rottle
2M
ixtu
re 2
Pro
p 2
Fla
p p
ote
ntio
me
ter
Flap Indicator
14
3
2
10 pole flatcable connectorshown without strain relief
1
6 wires cut off
To CN13
Tank Switch / Fuel cut-off connecting cable
Rev. Date Remarks Product
1.1 01-09-2003 Cable Tank Switch /
1.2 01-10-2003 Fuel Cut-off
Copyright 2003 TRC Development b.v. - Holland
Tank Switch seen from the back
Tank Sw. FSS1 FSS2 Left 0 1 Both 1 0 Right 0 0
Fuel Switch FSS3 On 1 Off 0
Fuel Switch seen from the back
Total length 75 cm.
1
4 3
2
Gear Switch
seen from the back
1
20
Switches connecting cable
Some wires cut off (5, 6, 14)
20 pole flatcable connectorshown without strain relief
To CN 11
Ha
nd
bra
ke
AV Switch
(Switches seen from the back)
Top View Potentiometer
10 Kohm
4 cm.
ALT
(Switches seen from the back)
BATT
Master SwitchGear Lights Light Regulation
Rev. Date Remarks Product
1.0 01-03-2004 CN12 Cable Assembly
for CCU v. 2
Copyright 2003 TRC Development b.v. - Holland
10 pole flatcable connectorshown without strain relief
1
3 wires cut off
To CN18
Rudder Pedals connecting cable
Rev. Date Remarks Product
1.1 01-09-2003 Cable Tank Switch /
1.2 01-10-2003 Fuel Cut-off
Copyright 2003 TRC Development b.v. - Holland
7-pole DIN Connector seen from the back
Total length 60 cm.
Throttle Mixture Prop connection
Throttle
Mixture
Prop
white (1)grey (2)purple (3)
blue (1)green (2)yellow(3)
orange (1)red (2)brown (3)
To CN 4
To CN 5
To CN 6
80 cm.
Rev. Date Remarks Product
1.1 01-09-2003 Cable Throttle/Mix/Prop
1.2 01-10-2003
Copyright 2003 TRC Development b.v. - Holland
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