WT9 Dynamic LSA. AIRCRAFT MAINTENANCE MANUAL (AS-AMM-01-000, 22. 05. 2017) - page 29

Effectivity:

ALL

12 06. 2020

NAVIGATION

– Transponder antenna

– Coaxial cable

– Antenna nut

For information:

– Serrated locking washer

– Fuselage bottom part

Fig. 34-13 XPDR Antenna Removal / Installation

DEPENDENT POSITION DETERMINING

NAVIGATION

SV-GPS-250 antenna

Type of maintenance:

Line

Personnel qualification:

Independent certifying staff qualified in accordance

with Part-66 or higher.

Recommended tools, materials, persons and documentation:

ITEM

QUANTITY

Philips screwdriver

1 pc

Cable ties 2.6

Persons

Tab. 34-11 Recommended tools, materials, persons and documentation

(1) SV-GPS-250 antenna removal:

Set

MASTER SWITCH

OFF

position.

Remove the instrument panel cover (Chapter 39-10).

Disconnect the connector of cable (2, Fig. 34-14) from the display.

Remove all cable ties on length of cable (2).

Unscrew the bolts (3), remove washers (6), nuts (7) and remove
the antenna (1).

(2) SV-GPS-250 antenna installation:

Put the antenna (1, Fig. 34-14) to the bracket (8) and fasten it
by means of the bolts (3), washers (6) and nuts (7).

Attach cable (2) by using cable ties.

Connect the connector of cable (2) to the display.

Install the instrument panel cover (Chapter 39-10).

Set

MASTER SWITCH

position and carry out an operational

test.

Effectivity:

ALL

12. 06 2020

NAVIGATION

– SV-GPS-250 antenna

– Washer 6 x 12 x 0.5

– Cable

– Nut M4

– Bolt M4 x 25 (4 pcs)

For information:

– TRX / AT-1 GPS antenna

– Bracket

– Cable

– Bracket

Fig. 34-14 SV-GPS-250 and TRX / AT-1 GPS Antennas Removal / Installation

DEPENDENT POSITION DETERMINING

NAVIGATION

TRX / AT-1 GPS antenna

Type of maintenance:

Line

Personnel qualification:

Independent certifying staff qualified in accordance

with Part-66 or higher.

Recommended tools, materials, persons and documentation:

ITEM

QUANTITY

Knife

1 pc

Double side tape

Cable ties 2.6

Persons

Tab. 34-12 Recommended tools, materials, persons and documentation

(1) TRX / AT-1 GPS antenna removal:

Set

MASTER SWITCH

OFF

position.

Remove the instrument panel cover (Chapter 39-10).

Disconnect the connector of cable (5, Fig. 34-14) from the TRX unit.

Remove all cable ties on length of cable (5).

Using knife, carefully remove the antenna (4).

(2) TRX / AT-1 GPS antenna installation:

Remove all remains of tape from antenna (4, Fig. 34-14) and bracket
(7).

Glue new tape on the antenna (4) and put it on the bracket (7).

Attach cable (5) by using cable ties.

Connect the connector (5) to the TRX unit.

Install the instrument panel cover (Chapter 39-10).

Set

MASTER SWITCH

position and carry out an operational

test.

Effectivity:

ALL

12. 06. 2020

NAVIGATION

GA 35 GPS antenna

Type of maintenance:

Line

Personnel qualification:

Independent certifying staff qualified in accordance

with Part-66 or higher.

Recommended tools, materials, persons and documentation:

ITEM

QUANTITY

Philips screwdriver

1 pc

Wrench 7

1 pc

Knife

1 pc

Persons

Tab. 34-13 Recommended tools, materials, persons and documentation

(1) GA 35 GPS antenna removal:

Set

MASTER SWITCH

OFF

position.

Remove the instrument panel cover (Chapter 39-10).

Remove the EPS cover (Chapter 06-00).

Disconnect the connector (5, Fig. 34-15) from the GPS antenna.

Unscrew the nuts (4), remove washers (7, 8), remove the ground
wire (2) and remove the screws (3).

Pull out the metal plate (6) and carefully pull out GPS antenna (1)
from the fuselage using a knife.

Install the protective cover on the antenna connector.

(2) GA 35 GPS antenna installation:

Put the antenna (1, Fig. 34-15) to correct position on top of fuselage.

Attach the antenna using the screws (3), metal plate (6), washers
(7, 8), ground wire (2) and nuts (4).

Connect the connector (5) to the GPS antenna.

Apply the white silicone around the antenna to seal it.

Install the EPS cover (Chapter 06-00).

Install the instrument panel cover (Chapter 39-10).

Set

MASTER SWITCH

position and carry out an operational

test.

DEPENDENT POSITION DETERMINING

NAVIGATION

– GPS GA 35 antenna

– Connector

– Ground wire

– Metal plate

– Bolt M4 x 30

– Washer 4 x 12 x 1

– Nut M4

– Washer 4 x 9 x 0.7

Fig. 34-15 GPS GA 35 Antenna Removal / Installation

CONTENTS

INSTRUMENT AND

CONTROL PANELS

39 INSTRUMENT AND

CONTROL PANELS

CONTENTS

GENERAL ......................................................................... 3

INTRODUCTION ....................................................................... 3

39-10

INSTRUMENT AND CONTROL PANELS......................... 5

DESCRIPTION .......................................................................... 5

WT9 Dynamic LSA / Club Instrument panel ...................... 6

WT9 Dynamic LSA / Club Instrument panel (towing version)
.......................................................................................... 9

MAINTENANCE PRACTICES ................................................. 13

Instrument panel cover .................................................... 13

Instrument panel .............................................................. 15

12 V socket ...................................................................... 17

Circuit breakers KLIXON ................................................. 19

Circuit breakers ETA 106-P10 ......................................... 21

Switches .......................................................................... 23

Control / warning lamp .................................................... 25

Test button ...................................................................... 27

Airspeed indicator, altimeter ............................................ 28

Vertical speed indicator ................................................... 31

Standby RPM indicator .................................................... 33

Propeller regulator PR1-P ............................................... 35

Flight hours counter ......................................................... 37

Standby bank indicator .................................................... 39

SV-D1000 display ............................................................ 41

PM3000 intercom ............................................................ 45

Radio Garmin GNC 255A NAV/COMM ........................... 47

GENERAL

INSTRUMENT AND

CONTROL PANELS

39-00 GENERAL

1. INTRODUCTION

The instrument panel is arranged primarily for use by the pilot in the left seat; however,
it can be viewed from the co-pilot in the right seat. Primary flight display and warning
and control lamps are located on the left side of the panel and engine monitoring
system is located on the right side of the instrument panel.

INSTRUMENT AND CONTROL PANELS

INSTRUMENT AND

CONTROL PANELS

39-10 INSTRUMENT AND CONTROL PANELS

1. DESCRIPTION

Instrument panel is made of glass/carbon fabric laminate and is attached to the central
tunnel and  both  sides of  fuselage.  In the middle  of  top  edge  is  the panel  supported
with composite stiffener. The instrument panel is covered with glass laminate cover.
The  cover  overlaps  the  instrument  panel  to  limits  undesirable  reflections
on instruments displays. The panel is divided into three sections: left, centre and right.
Under the instrument panels, on both left and right side, are located remote controls
for position adjustment of rudder pedals.

Depending on the installed equipment, there are available two layouts of instrument
panel. For basic instrument panel layouts see 1.A. (Fig. 39-1), for instrument panel
layout with installed towing equipment see 1.B (Fig. 39-2).

Effectivity:

ALL

12. 06. 2020

INSTRUMENT AND
CONTROL PANELS

WT9 Dynamic LSA / Club Instrument panel

Layout valid from S/N 17001 to 20005 inclusive

Layout valid from S/N 21001

Fig. 39-1 Instrument Panel Layout (page 1 of 2)

INSTRUMENT AND CONTROL PANELS

INSTRUMENT AND

CONTROL PANELS

– PFD Dynon SkyView SV-D1000

– USB Connector (RH-D1000)

– MFD Dynon SkyView SV-D1000

– Standby fuel pressure indicator

– Standby altimeter

– Flying hours counter

– Standby airspeed indicator

– Pedal’s adjustment remote control handle

– USB Connector (LH-D1000)

– 12V/10A Power socket

–

FUEL PUMP

control lamp

– Standby bank indicator

–

STALL

warning lamp

–

AVIONICS

switch

–

LH FUEL RES.

warning lamp

–

NAV / ACL

switch

–

RH FUEL RES.

warning lamp

–

LAND

switch

–

EMS

warning lamp

–

FUEL PUMP

switch

–

OIL PRESS.

warning lamp

–

IGNITION

switches

–

TEST

button

–

THROTTLE

control

–

CHARGE

warning lamp

–

CARBUR. PREHEATING

handle

– Intercom

– Fuel selector valve

– Magnetic compass

–

MASTER SWITCH

– Standby variometer

– Keyed ignition switch

– Standby RPM indicator

–

RESCUE SYSTEM

activating

handle

– NAV / COMM radio

–

CABIN HEATING

control

– Transponder

–

CABIN VENTILATION

control

– ELT remote control

–

CHOKE

control

– Engine Hours Counter

– Circuit breakers

Fig. 39-1 Model Instrument Panel Layout (page 2 of 2)

Effectivity:

ALL

12. 06. 2020

INSTRUMENT AND
CONTROL PANELS

Left section of instrument panel:

Installed are: standby airspeed indicator Winter 7FMS511 (or 7FMS513), altimeter
Winter 4FGH40 and bank indicator Winter QMII.

Primary Flight Display (PFD) Dynon SkyView SV-D1000 is installed in the middle
of left section. This instrument also can display data of Engine Monitoring System
(EMS) and MAP data.

Under the PFD, in the lower right corner of the left section are located the following
switches:

AVIONICS

NAV / ACL

(navigation and anti-collision lights),

LAND

(landing

lights) and

FUEL PUMP

Above the PFD is located a row of control and warning lamps as follows (with their
meaning):

FUEL PUMP

activation of the auxiliary electric fuel pump

STALL

activation of the stall warning system

LH FUEL RES.

fuel quantity in the left tank is less than 16 liters

RH FUEL RES.

fuel quantity in the right tank is less than 16 liters

EMS

exceeding of the engine limit parameters

OIL PRESS.

oil pressure is less than 2 bar / 29 psi

CHARGE

voltage is less than approximately 12.5 volts

Control and warning lamps function can be verified by pressing of the

TEST

button.

In the left lower corner is located 12 V / 10 A power socket.

Central section of instrument panel:

In bottom section are installed:

IGNITION

switches, starter key and

MASTER

SWITCH

. There are also installed transponder Garmin GTX 328 or GTX 335, radio

Garmin GNC 255A, intercom PM3000, standby variometer 5StVM 10 and standby
RPM indicator ROAD IF61.2B35.2301.

Sticker with registration marks is also placed in this section.

At the top of centre section there is installed magnetic compass Airpath C-2400P
on the glare shield.

Right section of instrument panel:

Multifunction Flight Display (MFD) Dynon Skyview SV-D1000 is installed in the middle
of right section. This instrument displays data of Engine Monitoring System (EMS).

On the right part are installed: standby fuel pressure indicator Skydrive FP-912/10 and
flying hours counter Winter FSMZ.

Circuit breakers are placed in a row at the lower edge of right section and on the right
side of right section (list of circuit breakers with values is in Chapter 24-60). In the right
lower corner is 12 V / 10 A power socket.

Remote control of the Emergency Locator Transmitter (ELT) and Engine Hours
Counter Hobbs are placed in the left upper area of right section.

INSTRUMENT AND CONTROL PANELS

INSTRUMENT AND

CONTROL PANELS

Central console:

Vertical section contains throttle control, rescue system actuator, carburetor preheating
control, cockpit heating and ventilation control handles, fuel selector valve and choke
control.

Pedestal panel between pilot and co-pilot is equipped with flaps control, pitch and roll
trim switches and brake lever (see Chapter 27-50).

Instrument Panel Cover:

Instrument  panel  cover  (1,  Fig.  39-3)  is  made  of  glass  laminate.  It  is  attached
to the fuselage with screws. On the top of  the cover is attached magnetic compass
(Chapter  39-10,  see  2.S.),  on  the  bottom  part  are  attached  ADS-B  and  FLARM
antennas (Chapter 34-40).

WT9 Dynamic LSA / Club Instrument panel (towing version)

Fig. 39-2 Instrument Panel Layout (Towing Version) (page 1 of 2)

Effectivity:

ALL

12. 06. 2020

INSTRUMENT AND
CONTROL PANELS

– PFD Dynon SkyView SV-D1000

– Standby fuel pressure indicator

– MFD Dynon SkyView SV-D1000

– Flying hours counter

– Standby altimeter

– Pedal’s adjustment remote control handle

– Standby airspeed indicator

– 12V/10A Power socket

– USB Connector (LH-D1000)

– Standby bank indicator

–

FUEL PUMP

control lamp

–

AVIONICS

switch

–

STALL

warning lamp

–

NAV / ACL

switch

–

LH FUEL RES.

warning lamp

–

LAND

switch

–

RH FUEL RES.

warning lamp

–

FUEL PUMP

switch

–

EMS

warning lamp

–

IGNITION

switches

–

OIL PRESS.

warning lamp

–

THROTTLE

control

–

TEST

button

–

CARBUR. PREHEATING

handle

–

CHARGE

warning lamp

– Fuel selector valve

– Intercom

–

MASTER SWITCH

– Magnetic compass

– Keyed ignition switch

– Standby variometer

–

RESCUE SYSTEM

activating

handle

– Propeller regulator

–

CABIN HEATING

control

– NAV / COMM radio

–

CABIN VENTILATION

control

– Transponder

–

CHOKE

control

– ELT remote control

– Circuit breakers

– Engine Hours Counter

–

CAMERA

switch

– USB Connector (RH-D1000)

–

TOW RELEASE

handle

Fig. 39-2 Instrument Panel Layout (Towing Version) (page 2 of 2)

INSTRUMENT AND CONTROL PANELS

INSTRUMENT AND

CONTROL PANELS

Left section of instrument panel:

Installed are: standby airspeed indicator Winter 7FMS511 (or 7FMS513), altimeter
Winter 4FGH40 and bank indicator Winter QMII.

Primary Flight Display (PFD) Dynon SkyView SV-D1000 is installed in the middle
of left section. This instrument also can displays data of Engine Monitoring System
(EMS) and MAP data.

Under the PFD, in the lower right corner of the left section are located the following
switches:

AVIONICS

NAV / ACL

(navigation and anti-collision lights),

LAND

(landing

lights),

FUEL PUMP

and

CAMERA

Above the PFD is located a row of control and warning lamps as follows (with their
meaning):

FUEL PUMP

activation of the auxiliary electric fuel pump

STALL

activation of the stall warning system

LH FUEL RES.

fuel quantity in the left tank is less than 16 liters

RH FUEL RES.

fuel quantity in the right tank is less than 16 liters

EMS

exceeding of the engine limit parameters

OIL PRESS.

oil pressure is less than 2 bar / 29 psi

CHARGE

voltage is less than approximately 12.5 volts

Control and warning lamps function can be verified by pressing of the

TEST

button.

In the left lower corner is located 12 V / 10 A power socket.

Central section of instrument panel:

In bottom section are installed:

IGNITION

switches, starter key and

MASTER

SWITCH

. There are also installed transponder Garmin GTX 328 or GTX 335, radio

Garmin GNC 255A, intercom PM3000, standby variometer 5StVM 10 and Flybox
Propeller regulator PR1-P. Sticker with registration marks is also placed in this section.

At the top of centre section there is installed magnetic compass Airpath C-2400P
on the glare shield.

Right section of instrument panel:

Multifunction Flight Display (MFD) Dynon Skyview SV-D1000 is installed in the middle
of right section. This instrument displays data of Engine Monitoring System (EMS).

On the right part are installed: standby fuel pressure indicator Skydrive FP-912/10 and
flying hours counter Winter FSMZ.

Remote control of the Emergency Locator Transmitter (ELT) and Engine Hours
Counter Hobbs are placed in the left upper area of right section.

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