Ccu 2 Connections March 2005

7/30/2019 Ccu 2 Connections March 2005

1/41

CCU2 Connections Manual

CCU2 Connections,

Wiring DiagramsModifications

&Schematics


2/41


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


3/41


1. CCU2 Connections

The CCU2 can drive many different gauges and is able to read out many differentinstruments, like Throttles, Switches, Trim wheel etc. compared to the CCU1.

(Note: the connect ions in the above picture b etween the di f ferent inst ruments and the CCU2 board are just

for i l l us t ra t i on on ly . P lease see Chapter 2 for exac t c onnect i ons)

This document describes how the instruments are connected and how they are driven by the


4/41


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 *)


5/41


2. The Central Control Unit

List and position of the I/O connectors

NOTE: The position of the texts on the picture on theleft is not identical to the position of the text on theboard itself.

The CCU2 is prepared for future expansion with moreI/O lines and will be able to control instruments for atwin engine aircraft. Therefore more I/O lines are made

available. At the same time a number of smallerconnectors have been combined into 2 largerconnectors. 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 theleft is not identical to the position of the text on theboard itself.

CN11 Handbrake, Avionics Switch, Gear, LightControl, Master Switch

CN12 Analog outputs, 8 pcs.*), Quartz CounterCN13 Fuel selector + Shut offCN14 Digital ClockCN15 Flaps, Throttle1/2, Mixture1/2, Prop1/2CN16 Trim wheelCN17 Starter SwitchCN18 Rudder PedalsCN19 Yoke

CN20 CCN43

CN35

CN36

CN37

CN38

CN30

CN31

CN32

CN29

CN28

CN33

CN34


6/41


4. Connectors and their I/O linesThe 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. Damagescaused 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 backon 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 towardsthe device.

- The term Analog input means that this input can read an analog value between0 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 isderived 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 isdesigned in this way because the servo motors draw more power than can be deliveredthrough the USB connector from the controlling PC.

B th 5 li t b t d i d f th l t i d t f ti


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The software of the CCU2 reads out both switches and translates this into a signal telling theflight simulator software that the certain knob is turned left or right and at what speed.

PotentiometersIn 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 onone side connected to +5v. (Vcc) and on the other side to Ground. The wiper of thepotentiometer is connected to the analog input on the CCU2.

Potentiometers are used in a.o.: Yoke, Throttle, Mixture, Propeller, Flap Switch, Trim and thePiher Sensors (in essence a potentiometer) in the gauges Altimeter, Heading Indicator, ADFand Compass.

CN1 to CN10 Do not exist on the CCU2 Board

CN11 Handbrake, Avionics Switch, Gears, Dimmer and Master SwitchPin 1 GroundPin 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 ConnectedPin 6 GroundPin 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 /

20 A) i t thi t t


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CN13 Fuel selector + Shut offPin 1 Ground

Pin 2 FSS1 Digital Input. The pin is forced high, when not connected, via a resistor on theCCU2. 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 theCCU2. When connected to Ground, the FSS3 input is active.

Pin 5 FSS4 Digital Input.Pin 6 No connectionPin 7 No connection

Pin 8 No connectionPin 9 No connectionPin 10 No connection

Tank Switch Table (as connected for TRC Link operation):Left: FSS1 = 0, FSS2 = 1

Both: FSS1 = 1, FSS2 = 0Right: FSS1 = 0, FSS2 = 0

Fuel Switch Table (as connected for TRC Link operation):

On: FSS3 = 1Off: FSS3 = 0

CN14 Digital Clock

Pin 1 GroundPin 2 +5v.Pin 3 DCS2

Pin 4 DCS3

Pi 5 DCS4


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CN16 Trim wheelPin 1 Ground

Pin 2 +5v.Pin 3 TRW1Pin 4 TRW2

Pin 5 TRW3Pin 6 Trim wheel AIR2 Analog Input, relocated by modification from CN21 pin 4. Reads outthe position of the Trim Wheel.

Pin 7 No connectionPin 8 No connectionPin 9 No connection

Pin 10 No connection

CN17 Starter Switch

Pin 1 GroundPin 2 No connectionPin 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 aresistor 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 connectionPin 8 No connection

Pin 9 No connectionPin 10 No connection

As wired for operation under TRC Link:

OFF STA1 t G d


10/41


CN19 YokePin 1 Ground

Pin 2 +5v.Pin 3 YOK1 Digital Output. Servo Signal for future implementation of control loading (forcefeedback)

Pin 4 YOK2 Digital Output. Servo Signal for future implementation of control loading (forcefeedback)Pin 5 Yoke YOK3 Analog Input, PITCH

Pin 6 Yoke YOK4 Analog Input, ROLLPin 7 NCPin 8 NC

Pin 9 NCPin 10 NC

CN20 CompassPin 1 Ground

Pin 2 +5v. X

Pin 3 Compass CMP1 Digital Output, Servo SignalPin 4 Compass CMP2 Analog Input for position sensor 1

Pin 5 Compass CMP2 Analog Input for position sensor 2Pin 6 +5v.Pin 7 Ground

Pin 8 LampPin 9 NCPin 10 NC

CN21 Airspeed IndicatorPin 1 Ground

Pin 2 +5v. X

Pi 3 Ai d I di t AIR1 Di it l O t t S Si l


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CN23 Vertical Speed IndicatorPin 1 Ground

Pin 2 +5v.X

Pin 3 Vertical Speed IndicatorVSPD Digital Output Servo Signal

Pin 4 NCPin 5 NCPin 6 NC

Pin 7 GroundPin 8 LampPin 9 NC

Pin 10 NC

CN24 Attitude Indicator

Pin 1 Ground

Pin 2 +5v. X

Pin 3 Attitude IndicatorATT1 Digital Output Servo SignalPin 4 Ground

Pin 5 +5v. X

Pin 6 Attitude IndicatorATT2 Digital Output Servo Signal

Pin 7 Ground

Pin 8 LampPin 9 NC

Pin 10 NC

CN25 Turn Coordinator

Pin 1 Ground

Pin 2 +5v. X

Pin 3 Turn CoordinatorTRN1 Digital Output Servo SignalPin 4 Ground

Pi 5 5 X


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CN28 ADF Indicator

Pin 1 Ground

Pin 2 +5v. X

Pin 3 ADF IndicatorADF1 Digital Output Servo SignalPin 4 ADF2 Digital Output Servo Signal (Not Used)Pin 5 ADF IndicatorADF3 Digital Input (Rotary Encoder)

Pin 6 ADF IndicatorADF4 Digital Input (Rotary Encoder)Pin 7 ADF Indicator ADF IndicatorADF5 Analog Input, Piher Position SensorPin 8 ADF IndicatorADF6 Analog Input, Piher Position Sensor

Pin 9 ADF IndicatorADF7 Analog Input, Piher Position SensorPin 10 ADF IndicatorADF8 Analog Input, Piher Position SensorPin 11 Lamp

Pin 12 + 5v.Pin 13 NCPin 14 NC

CN29 Heading IndicatorPin 1 Ground

Pin 2 +5v. X

Pin 3 Heading IndicatorHED1 Digital Output Servo SignalPin 4 HED2 Digital Output Servo Signal (Not Used)Pin 5 Heading IndicatorHED3 Digital Input (Rotary Encoder)

Pin 6 Heading IndicatorHED4 Digital Input (Rotary Encoder)Pin 7 Heading IndicatorHED5 Analog Input, Piher Position SensorPin 8 Heading IndicatorHED6 Analog Input, Piher Position Sensor

Pin 9 Heading IndicatorHED7 Analog Input, Piher Position SensorPin 10 Heading IndicatorHED8 Analog Input, Piher Position SensorPin 11 Lamp

Pi 12 5


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CN31 Warning Lights & SwitchPin 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 FuelPin 5 Warning Lights & Switch WAR3 Digital Output, Right FuelPin 6 Warning Lights & Switch WAR4 Digital Output, Oil Press

Pin 7 Warning Lights & Switch WAR5 Digital Output, Left VacuumPin 8 Warning Lights & Switch WAR6 Digital Output, VACPin 9 Warning Lights & Switch WAR7 Digital Output, Right Vacuum

Pin 10 Warning Lights & Switch WAR8 Digital Output, VoltsPin 11 Warning Lights & Switch WAR9 Digital Input, TEST if connected to Ground alllights will go on.

Pin 12 Warning Lights & Switch WAR10 Digital Input, DIM if connected to Ground alllights 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 OutputPin 4 AUT2 Digital Output

Pin 5 AUT3 Digital OutputPin 6 AUT4 Digital OutputPin 7 AUT5 Digital Output

Pin 8 AUT6 Digital OutputPin 9 AUT7 Digital OutputPin 10 AUT8 Digital Output

( )


14/41


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 GroundedPin 5 Switches SW3 Digital Input BCN, OFF when GroundedPin 6 Switches SW4 Digital Input Land, OFF when Grounded

Pin 7 Switches SW5 Digital Input Taxi, OFF when GroundedPin 8 Switches SW6 Digital Input Nav, OFF when GroundedPin 9 Switches SW7 Digital Input Strobe, OFF when Grounded

Pin 10 Switches SW8 Digital Input Pitot Heat, OFF when GroundedPin 11 Switches SW9 Digital Input Alt Static Air, OFF when GroundedPin 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 NCPin 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


15/41


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 SignalPin 7 Ground

Pin 8 LampPin 9 NCPin 10 NC


16/41


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


17/41


18/41

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

+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

D[0..7]

ALT1

ALT2

VORx

SEL4 SEL6SEL5

OE11

OE219

IC1174HCT541IC1174HCT541

1k80R341k80R34

OE11 OE2 19


9

4

6 14

1k80R401k80R40

9 11

3 17 1k80R421k80R42

Vcc

20

Vss

10

1k80R381k80R38

7 13

OE11

OE219


4 16

2 18

5

1k80R351k80R35

8 12

Vcc

20

Vss

10

5 15

1k80R291k80R29

1k80R461k80R46

1k80R281k80R28

1k80R301k80R30

10n0

C11

10n0

C11

3 17

1k80R271k80R27

1k80R471k80R47

9 11

O1

IC74IC74

1k80R451k80R45

6 6 14

10n0

C10

10n0

C10

1k80R261k80R26

1k80R311k80R31

4 16

1k80R361k80R36

1k80R441k80R44

1k80R391k80R39

7 13

2 18

1k80R411k80R41

5 15

1k80R251k80R25

1k80R321k80R32

OE11

OE219


V

7

2

1k80R241k80R24

8 12

3 17

LE11 OE 1


6 14

1k80R331k80R33

1k80R431k80R43

Vcc

20

Vss

10

1k80R371k80R37

9 11

4 16

7 13

8

3

LE11 OE 1


5 15

8 12

2 18

10n0

C12

10n0

C12


19/41


20/41


21/41

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 CCUvia Ribbon cable

Copyright 2003 TRC Development b.v. - Netherlands

Rev. Date Board Remarks Page 1 of 1

AttitudeIndicator1.0 230603 CR/Design


22/41

+5X

+5X

+5X

+5V

+5V +5V

+5V +5V

+5V+5V

+5V +5V

+5V

+5V

+5V

+5V

Date Page of

2003 TRC Development b.v. - The NetherlandscRev. Board Remarks

O

0 1 30 50 2 P C0 21 1

1 2 80 50 2 P C0 21 8

ALT+ADF

BS/Design

BS/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


23/41

+5X

+5V

+5V +5V

+5V +5V

+5V+5V

+5V +5V

+5V

+5V

+5V

+5V

+5X

+5X

+5V+5V

+5V+5V

Date Page of

Co p yr i g h t 2003 T RC Deve l o p men t b .v . - T he Ne t her l and s

R ev. Board Remarks

1 2 80 502 P C0 218

2 1 80 702 P C0 223

3 1 51 002 P C0 229

1612024 PC0239

ALT+ADF -2BS/connectors

BS/+470pF, 3p. conn.

BS/nulsensor

BS / C3 mo ved

11* opt ion

470pC4*

1206

10k0P1

top*

330ER10

axi al

*

470pC1

radial

AngleC N2Se r v o 2

1

2

3

1M00

R7

1 2 0 6

*

1M00

R4

axial

*

1 0k0P4

bot

C N4lamp*

Flatca bleC N 5

1 2

3 4

5 6

7 8

9 10

11

13

12

14

4 k70R 11

1 2 0 6

M MHFC N6

1

2

3

4

5

6

1M00R1

axial

*

470pC2

radial

AngleC N1Se r v o 1

1

2

3

1 0k0P2

bot

1M00

R8

1 2 0 6

330ER9

1206

1M00R5

1 2 0 61M00R2

axial

*

4 k 7 0R 12

axial

*

470pC3*

1206

10k0P3

top

*

AngleC N 3D ig iPo t

1

2

3

1M00R6

1 2 0 6

1M00

R3

axial

*


24/41

+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 of c

Rev. Board Remarks

O

0 241003 PC----

TRC circ. breakers

BS/Ontwerp

11Date Page of c

Rev. Board Remarks

O

0 241003 PC----

TRC circ. breakers

BS/Ontwerp

11Date Page of 2003 TRC Development b.v. - The Netherlandsc

Rev. Board Remarks

O

0 241003 PC----

TRC circ. breakers

BS/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


Vee

8

Vcc

9


2 15

IC2IC2

RY4RY4

R30R30

6 11

IC2IC2

RY4RY4

RY14RY14

R25R25

R42R42

RY12RY12

1 2

3 4

5 6

7 8

9 10


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


3 14

IC3IC3

1 2

3 4

5 6

7 8

9 10

11

13

12

14

15 16

17 18

19 20


RY7RY7

RY1RY1

2 15

IC3IC3

R39R39

Vee

8

Vcc

9


RY11RY11

R6R6

R34R34

2 15

IC4IC4

4 13

IC2IC2

RY2RY2

A02

Q210

OE23

A13

LE1

Vcc

24

Q38

Vss

12

Q65

A221

Q56

Q47

Q19

Q74

Q011

A322

Q917

Q1416

Q1313

Q1119

Q1214

Q1020

Q818

Q1515

74HC4514IC174HC4514IC1

R18R18

1 16

IC4IC4

RY15RY15

R24R24

5 12

IC4IC4

RY2RY2

RY5RY5R13R13


25/41

+5V

+5V

+5V

+5V

+5V

+5V

+5V

+5V

DCS3

DCS5

DCS1

DCS2

DCS4

DCS6

DCS4

DCS5

DCS6

DCS1

DCS2

DCS3

Date Page of

2003 TRC Development b.v., HollandcRev. Board Remarks

O

0 291002 PC02321.1 280303 PC0305 Digital Clock 1

BS/DesignBS/proc,knob,backl,p57

11* option

39k0

R1

0603

SKHHCRSW2

IC2

3

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

*

12k0

R6

0603

1u00

C3

25V

10k0

R13

0603

10k0

R4

0603

10n0

C4

D20291A0LCD1

S15

S26

S37

S48

S59

S610

S711

S812

S913

S1014

S1115

S1216

S1317

S1418

S16 20

S1519

S1721

C11

C22

C33

C44

A23

K22

1E00R17

1206

SKHHCRSW1

FCX789AT1

12k0

R2

0603

12k0R7

0603

100E

R9

0805

10k0

R11

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

SEG1868SEG19

69

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

SEG7929SEG80

30

COM150

COM249

COM348

COM447

COM546

NC31

LOAD33

CLOCK34

DATA35

BLANK36

DSEL237

DSEL138

OSC-R39

OSC-C40

OSC-IN41

VLC145

VLC244

VLC343

12k0R8

0603

*

12k0R5

0603

1E00R15

1206

1n00

C1

0805


26/41

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 CN16of CCU

via Ribbon cable



Dual SmallGauge1.0 230603 CR/Design


27/41

+5X

+5X

Date Page of


O

0 2 80 50 2 P C0 21 3

Gen. Instr.BS/Design

11* option

CN3lamp*

Servo Connector (Black wire = pin 3)

1

2

3

via 10 wire ribbon cableConnected to CN21, CN 22 or CN23 of CCU

1 2

3 4

5 6

7 8

9 10


28/41

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 CCUvia Ribbon cable



Turn & Bank

Indicator1.0 230603 CR/Design

Yellow

Black

Red

Yellow

Black

Red


29/41

+5V

+5V

+5V

+5X

+5X

+5X

+5X +5V+5V

+5V +5V

Date Page of


O

0 1 30 50 2 P C0 21 0

VOR 1+2BS/Ontwerp

11* option

10k0P1

top

1M00R1

axial

AngleCN2Servo 2

1

2

3

1M00R2

axial10k0P2

bot

1M00R3

1206

*AngleCN3

Servo 3

1

2

3

FlatcableCN5

1 2

3 4

5 6

7 8

9 10

1M00R4

1206

*

AngleCN1Servo 1

1

2

3

CN4lamp*


30/41

+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 of


O

0 1 30 50 2 P C0 21 3

WarningBS/Design

11* option

SW1

redLD20

-TEST-

redLD19

Volts

120ER9

0805

IC1

611

orangeLD4

Low Fuel

IC2

1 16

IC2

5 12

120ER15

0805

IC1

1 16

120E

R16

0805

redLD12

Oil P.

120ER17

0805

IC1

710

redLD21

-TEST-

120ER25

0805

120ER18

0805

120ER14

0805

orangeLD5

Low Fuel

120ER22

0805

120ER19

0805

120ER7

0805

IC2

215

120ER3

0805

IC1

2 15

orangeLD1

L LF

IC2

6 11

120ER4

0805

120ER24

0805

120ER13

0805

IC1 ULN2003A

Vcc

9

Vee

8

120ER10

0805

redLD8

Oil P.

orangeLD16

R VAC

120ER2

0805

redLD22

-TEST-

orangeLD15

VAC

IC1

3 14

orangeLD6

Low Fuel

120ER20

0805

orangeLD14

VAC

orangeLD2

Low Fuel

IC2

3 14

120ER5

0805

redLD11

Oil P.

IC2

7 10

redLD9

Oil P.

120ER12

0805120ER8

0805

IC1

413

redLD23

-TEST-

FlatcableCN1

1 2

3 4

5 6

7 8

9 10

11

13

12

14

120ER1

0805

orangeLD13

L VAC

orangeLD7

R LF

IC2 ULN2003A

Vcc

9

Vee

8

orangeLD3

Low Fuel

redLD18

VoltsIC2

413

120ER23

0805

IC1

5 12

redLD10

Oil P.

120ER21

0805

120ER6

0805

redLD24

-TEST-

redLD17

Volts

redLD25

-TEST-

120ER11

0805


31/41

+5V

+5V

+5V

+5V +5V

+5V+5V

+5X

+5X

Date Page of


O

0 2 80 50 2 P C0 21 3

CompassBS/Design

11* option

10k0P1

top

CN3lamp*

StraightCN1Servo

1

2

3

1M00R1

axial

10k0P2

bot

1M00R4

1206

*

1M00R2

axial

FlatcableCN2

1 2

3 4

5 6

7 8

9 10

1M00R3

1206

*


32/41

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


33/41


(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


1.1 22-03-2004 Key Lock Cable + PCB

(Starter Switch)



34/41

Starter Switch for Flight Simulators

Bottom View - connections 1(for general use)

Contact specificationsContact configuration 1 CO (SPDT)

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 the4th 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 viaconnector CN17 on the CCU or from any existing electronics.

Mounting InstructionsThe Starter Switch comes assembled. To mount the switch into a panel, loosen the smallscrews on the copper bushing to release the key.

Now loosen the nut from the Threaded Bush, and mount it in a panel, together with themetal parts as shown in the picture below. Do not forget to use the Round MountingRing.The panel hole must be 10 mm. (0,3937). When the Starter Switch is mounted into theTRC472 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 smallscrews 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

i ii i

12

3

4

5

678

9

10

1112

Common

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 Simulationuse, only pins 1 to 5

(positions 6-12 aremechanically locked).

67

Bottom View - connections 2(for use on the CCU1 or CCU2)


35/41


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


1.2 01-10-2003 Cable Yoke

1.3 29-04-2004



36/41


1

Trim Wheel connecting cable

2

1 3

4 wires cut off

3 wires cut off

To CN16


1.1 01-09-2003 Cable Trim Wheel

1.2 01-10-2003



37/41


1

Flaps/Throttle/Mixture/Prop

To CN15


1.0 29-04-2004 Cable Throttle/Mix/Prop


Throttle 1

Mixture 1

Prop 1

Throttle2

Mixture2

Prop2

Flappotentiometer

Flap Indicator


38/41

14

3

2


1

6 wires cut off

To CN13

Tank Switch / Fuel cut-off connecting cable


1.1 01-09-2003 Cable Tank Switch /

1.2 01-10-2003 Fuel Cut-off


Tank Switch seen from the back

Tank Sw. FSS1 FSS2Left 0 1

Both 1 0Right 0 0

Fuel Switch FSS3On 1Off 0

Fuel Switch seen from the back

Total length 75 cm.

Switches connecting cable


39/41

1

4 3

2

Gear Switch

seen from the back

1

20

Some wires cut off (5, 6, 14)


To CN 11

Handbrake

AV Switch

(Switches seen from the back)

Top ViewPotentiometer

10 Kohm

4 cm.

ALT

(Switches seen from the back)

BATT

Master SwitchGear Lights Light Regulation


1.0 01-03-2004 CN12 Cable Assembly

forCCU v. 2



40/41


1

3 wires cut off

To CN18

Rudder Pedals connecting cable


1.1 01-09-2003 Cable Tank Switch /

1.2 01-10-2003 Fuel Cut-off


7-pole DIN Connector seen from the back

Total length 60 cm.


41/41

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.


1.1 01-09-2003 Cable Throttle/Mix/Prop

1.2 01-10-2003


Ccu 2 Connections March 2005

Documents

Transcript of Ccu 2 Connections March 2005