system schematics.pdf

Dornier 328 - 300

Training Manual

Indicating/Recording

Effectivity:328-300

- FO

R TRAINING PURPO

SES ONLY -

Issue: Jul. 99 ETM

/XPage: 31 - 9

1.2 IN

TERFACE TO

OTHER SYSTEM

S

WU

FMSCDU

RAD. ALT.

CLRDEL

A BWX/EFIS/FWC

I/O

FMS AP

AC

A BWX/EFIS/FWC

AC

I/O

FROMR IACDATALOADER

TO FLT REC

FROM R DAU

TO R RMU

AP11

4

5

3

2 2

2

5 5 5 5

PFD MFD EICAS MFD PFDARINC 429WRAP-AROUND

AHRS

ADRU

DAU

COMM

NAV

MLS

RMU

FLIGHT GUIDANCE AND DISPLAY CONTROL PANEL

AHRS

ADRU

DAU

COMM

NAV

MLS

RMU

RAD. ALT.

ASCB

ASCB

RSB

TO FLT RECTO L RMU

FROM L DAU

TO WU

ASCB ASCB

TRIM

AILERON

ELEVATOR

RU

DD

ER

Fig. 1 Avionic System - Circuit Diagram

Do

rnier 328 - 300Training M

anualHydraulic Power

Effectivity:328-300

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R TRAINING PURPO

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Issue

: Mar. 99 ETM

/XPage:

29 - 31

28VDC BUS

DCMPCRTL

Relay10DA

PROX

Main ReservoirRelief/Vacuum

Break Valve

A

PSEU

M

AC MAINPUMP

ACMPCRTL

R-IN

R-OUTCaseDrainLine

P-INMain

Main Filter Package

P-out MAIN

Pressure Filter

ReturnFilterwithBypass

Main System Relief Valve

TemperatureTransducer

PressureTransducer

Outboard Return

GroundSpoiler

OutboardAlternate

Brake

RestrictorAssy

PROX

Main ReservoirRelief/Vacuum

Break Valve

A

PSEU

M M

AC MAINPUMP

ACMPCRTL

R-IN

R-OUTP-INSTBY

CaseDrainLine

P-INMain

Main Filter Package

P-out MAIN

Pressure Filter

ReturnFilterwithBypass

Main System Relief Valve

TemperatureTransducer

PressureTransducer

Outb.Conn.

GroundSpoilerInboard

RollSpoilerFlapsNormal

BrakeLdg.Ext.Emerg.

NoseWheel

Steering

Emerg./ParkBrake

STBYControl

PressureSwitch

DCMP Crtl

ReliefRestrictorValve

Change OverValve

PressureSwitch

ThermalRelief Valve

LandingGear

A

C

B

U

S

1

1

X

P

A

C

B

U

S

2

2

X

P

A

C

B

U

S

2

2

X

P

A

C

B

U

S

1

1

X

P

Dornier 328 - 300Training ManualElectrical Power

Issue: Mar. 99 ETM/XPage: 24 - 68

- FOR TRAINING PURPOSES ONLY - Effectivity:328-300

12.2! PRIMARY EICAS PAGE

Honeywell

MAINAHRSREF

DATA

MSGCOPY

2870450 FF LBS / HR

FQ LBS 2870450

50018000 CABIN

XXFTFPM

NU

NDOIL

TEMPOIL

PRSS

20 !20 !

24 !CV/S

XX90.5

N2

910 ITT

80.3

N1

115.0

912

108.3 TOGA

NO SYNC

IGN

VIB VIB

IGNSTART START

CAS FIELD MESSAGES:The following messages can be displayed:DC BUS 1 FAILDC BUS 2 FAILNON-ESS BUS 1 FAILNON-ESS BUS 2 FAILESS BUS FAILAPU GEN FAILL DC GEN FAILR DC GEN FAILL GEN OVHTR GEN OVHTBATT 1 FAILBATT 2 FAILL ALT FAILR ALT FAILL AC VOLT FAILR AC VOLT FAILINV 1 FAILINV 2 FAILINV BUS 1 FAILINV BUS 2 FAILTRU FAIL

Fig. 36 Primary EICAS Page - Indications

Dornier 328 - 300

Training Manual

Electrical Power

Effectivity:328-300

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R TRAINING PURPO

SES ONLY -

Issue: Mar. 99 ETM

/XPage: 24 - 69

12.3!ELECTRIC PAG

E

Honeywell

SYSTEM 2/3APUICE

PROTECTECSELECTR NEXT

INV 1

115 V 26 V 26 V 115 V

INV 2

ESSDC

BUS 1 BUS 2ACPOWER

102 A

GEN LH BATT 1 EXT

423 A

APU BATT 2

0 A

GEN RH

NONESS1 1 2 NONESS2ESSENTIAL

28.1 V 28.1 V

DCPOWER

ALT LH ALT RHTRUEXT

OFF

OVHTFAIL

115 V 115 V

FAIL

FAIL

OFF

DC NON-ESS 1 / DC NON-ESS 2Synoptic (green)- > 18.0 to 32.0 VDC

DC ESSENTIAL BUS(Synoptic)

DC BUS 1 / DC BUS 2(Synoptic)DC MAIN BUS 1 / 2Digital readout (white)- > 18.0 to < 32.0 VDCDigital readout (amber)- < 18.0 or > 32.0 VDC

DC GENERATOR L / R, APUFAIL (amber)- Generator has failed.OVHT (amber)- Generator overheated.Digital readout (white)- 400 A load max.Digital readout (amber)- Above 400 A load.

BATTERY 1 / BATTERY 2FAIL (amber)- Battery 1 or 2 has failed.OVHT (red)- Battery 1 or 2 is overheated.

DC BUS TIEVertical flowbar (green)- DC bus tie open (Off).Horizontal flowbar (white)- DC bue tie closed (On).

DC EXTERNAL POWERON (blue)- DC external power is switched on.OFF (blue)- DC external power is switched off.When airborne, whole synoptic is removed.

OVHTFAIL

28.1 V

DC ESSENTIAL BUSDigital readout (white)- > 18 to > 32 VDCDigital readout (amber)- < 18 or > 32 VDC

Fig. 37 Electric Page - DC Indications

Dornier 328 - 300

Training Manual

Electrical Power

Issue: Mar. 99 ETM

/XPage: 24 - 70

- FO

R TRAINING PURPO

SES ONLY -

Effectivity:328-300

Honeywell

SYSTEM 2/3APUICE


INV 1

115 V 26 V 26 V 115 V

INV 2

ESSDC

BUS 1 BUS 2ACPOWER

102 A

GEN LH BATT 1 EXT

96 A

APU BATT 2

0 A

GEN RH


28.1 V 28.1 V

DCPOWER

ALT LH ALT RHTRUEXT

OFF

OVHTFAIL

115 V 115 V

FAIL

FAIL

OFF

AC BUS 1 / AC BUS 2Synoptic (green)- >98 to >132 VAC.Synoptic (amber)- < 98 or > 132 VAC.

ALTERNATOR LH / RHFAIL (amber)- Alternator LH or RH failed.

TRUFAIL (amber)- Transformer rectifier unit failed.

AC BUS TIEVertical flowbar (green)- AC bus tie open (Off).Horizontal flowbar (white)- AC bus tie closed (On).

AC EXTERNAL POWERON (blue)- AC external is switched on.OFF (blue)- AC external power is switched off.When airborne, whole synoptic is removed.

FAIL

TRUSynoptic (green)- Transformer rectifier unit operating.Synoptic (white)- Transformer rectifier unit off.Synoptic (amber)- Transformer rectifier unit faled.

28.1 V

Fig. 38 Electric Page - AC Indications (Sheet 1 of 2)

Dornier 328 - 300

Training Manual

Electrical Power

Effectivity:328-300

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SES ONLY -

Issue: Mar. 99 ETM

/XPage: 24 - 71

Honeywell

SYSTEM 2/3APUICE


INV 1

115 V 13 26 V 115 V

INV 2

ESSDC

BUS 1 BUS 2ACPOWER

102 A

GEN LH BATT 1 EXT

96 A

APU BATT 2

0 A

GEN RH


28.1 V 28.1 V

DCPOWER

ALT LH ALT RHTRUEXT

OFF

OVHTFAIL

115 V 115 V

FAIL

FAIL

OFF

AC PHASES LH / RHDigital readout of phase 1 (white)- All AC phases are available.Digital readout of phases 1 to 3 (amber)- Respective AC phase has failed.

INVERTER BUS 1 / 2 (26V)Digital readout (white)- > 16 VAC to < 30 VAC.Digital readout (amber)- < 16 VAC or > 30 VAC.Synoptic (green)- > 16 VAC to < 30 VAC.Synoptic (amber)- < 16 VAC or > 30 VAC.

INVERTER BUS 1 / 2 (115 V)Digital readout (white)- > 98 VAC to < 132 VAC.Digital readout (amber)- < 98 VAC or > 132 VAC.Synoptic (green)- > 98 VAC to < 132 VAC.Synoptic (amber)- < 98 VAC or > 132 VAC.FAIL (amber)- Inverter 1/2 failed.

115 V0 V

V

28.1 V

Fig. 39 Electric Page - AC Indications (Sheet 2 of 2)




12.4! SYSTEM MAINTENANCE PAGE

Honeywell

SYSTEM 3/3CPCS/

OXYGENDOORS SYS

MAINTSENSOR

DATANEXT

FUELL TRANSFER MON 020498R TRANSFER MON 020498L TRANSFER LOWR TRANSFER LOWL LP FILTERR LP FILTER

CPCSBACKUP INSTRUMENTSAUTO CTRL MAINT

OXYGENQTY ACCURACY

ICE PROTECTL SWDW TEMPR SWDW TEMPL FWDW TEMPR FWDW TEMP

HYDRAULICSPROXI MAINT

MAX BRAKE TEMPERATURESL INB 123 !CL OUT 345 !CR INB 234 !CR OUT 456 !C

FLIGHT CONTROLSELEV TRIM MOTOR FAILRUDDER LIMIT FAIL

ELECTRTRU FAIL

APUOVERSPEEDOVERTEMP EGTOVERCURRENT ECUOIL PRESS LOWOIL TEMP HIGH

ENGINEL MAIN OIL FILTR MAIN OIL FILTL SCAV OIL FILTR SCAV OIL FILTL RGB CHIPS DETECTR RGB CHIPS DETECTL ENG CHIPS DETECTR ENG CHIPS DETECT

ELECTRTRU FAIL (amber)- Transformer Rectifier Unit has failed

Fig. 40 System Maintenance Page - Electric Indication


Effectivity:328-300

- FOR TRAINING PURPOSES ONLY - Issue: Mar. 99 ETM/XPage: 24 - 73

12.5! APU SYSTEM PAGE

ELECTRIC

200 AGEN OVHTGEN FAIL

READY TO LOADFUEL SOV CLOSED

OVERSPEEDOVERTEMP EGT

OVERCURRENT ECUOIL PRESS LOWOIL TEMP HIGH

LEAK

FAIL

ECS

EXT

ENG START

BLEEDELECTRIC PWR

APU

SYSTEM 2/3APUICE


90 650

EGTN

PT 0068

Honeywell

DC GENERATOR APUDigital Readout (white)- 400 A load max.Digital Readout (amber)- When 400 A load is exceeded.GEN OVHT (amber)- APU generator overheated (automatic APU shutdown)GEN FAIL (amber)- APU generator has failed (automatic APU shutdown)

Fig. 41 System Page APU

Dornier 328 - 300

Training Manual

Electrical Power

Effectivity:328-300

- FO

R TRAINING PURPO

SES ONLY -

Issue: Mar. 99 ETM

/XPage: 24 - 75

12.7!ELECTRIC CO

NTROL PANEL

GEN-LH BAT 1 EXT GEN-APU BAT 2 GEN-RH

V

TIE

ESSENTIAL

NON-ESS 1 BUS 1 BUS 2 NON-ESS 2

DC ELECTRIC AC

BUS 1 BUS 2

ALT-LH TRU ALT-RH

TIE

EXT

115V 26V 26V 115V

INV 1 INV 2

FAILOFF

FAILOFF

AVAIL

ON

FAILOFF

FAILOFF

AVAIL

ONFAIL FAILFAIL

ON OFF OFF

FAILOFF

FAILOFF

OFF

OFF

L / R DC VOLTAGE INDICATORDigital readout (green)- Shows the output of the LH/RH batteries or LH/RH DC generators (voltage on MAIN BUS 1 and 2).

NON-ESS1/NON-ESS2 BUTTONVertical bar (white)- Indicates that NON ESS BUS is switched to DC MAIN BUS.OFF (white)- Indicates that NON ESS BUS is switched off.

ESSENTIAL BUS LEDSLEDs (green)- Indicates that ESSENTIAL BUS is supplied by either DC BUS 1, DC BUS 2, or by the TRU.LEDs (dark)- Extinguishes when ESSENTIAL BUS has failed or not powered.

GENERATOR LH / RH BUTTONNomal operation (dark)- Gererator is operating.FAIL (amber)- Generator has failed.OFF (white)- Generator is switched off.

BATTERY 1 / 2 BUTTONNormal operation (dark)- Battery is operating.FAIL (amber)- Battery has failed.OFF (white)- Battery is switched off.

DC BUS TIE BUTTONHorizontal bar (white)- Indicates that bus tie is closed (On).Vertical bar (white)- Indicates that bus tie is open (Off).

GENERATOR APU BUTTONON (white)- Generator is switched on.FAIL (amber)- Generator has failed.

DC EXTERNAL POWER BUTTONAVAIL (green)- Indicates that external power is plugged in and available.ON (white)- Indicates that external power is switched on.

Fig. 43 Electric Control Panel - DC Controls

Dornier 328 - 300

Training Manual

Electrical Power

Issue: Mar. 99 ETM

/XPage: 24 - 76

- FO

R TRAINING PURPO

SES ONLY -

Effectivity:328-300

GEN-LH BAT 1 EXT GEN-APU BAT 2 GEN-RH

V

TIE

ESSENTIAL

NON-ESS 1 BUS 1 BUS 2 NON-ESS 2

DC ELECTRIC AC

BUS 1 BUS 2

ALT-LH TRU ALT-RH

TIE

EXT

115V 26V 26V 115V

INV 1 INV 2

FAILOFF

FAILOFF

AVAIL

ON

FAILOFF

FAILOFF

AVAIL

ONFAIL FAILFAIL

ON OFF OFF

FAILOFF

FAILOFF

OFF

OFF

TRU SWITCHNormal position (safety latched)LH or RH position- Safety latch has to be lifted when switching to the LH or RH alternator.

AC BUS TIE BUTTONHorizontal bar (white)- Indicates that bus tie is closed (On).Vertical bar (white)- Indicates that bus tie is open (Off).

INVERTER 1 / 2 BUTTONNormal operation (dark)- Inverter is operating.FAIL (amber)- Inverter has failed.OFF (white)- Inverter is switched off.

AC EXTERNAL BUTTONAvail (green)- Indicates that AC external power is plugged in and available.ON (white)- Indicates that AC external power is switched on.

AC ALTERNATOR LH / RH BUTTONNormal operation (dark)- Alternator is operating.FAIL (amber)- Alternator has failed.OFF (white)- Alternator is switched off.

Fig. 44 Electric Control Panel - AC Controls

Dornier 328 - 300Training ManualPneumatic

Effectivity:328-300


3 CONTROLS ANDINDICATIONS

3.1 ECS PANEL

LHPACK

RHPACK

X-BLEED

LH RH

COLD HOT COLD HOT

TEMP SEL

CABIN

EFIS AVIONICRECIRC

FLOWMODE

COCKPIT

ECSFANS

OFF

OFF

OFF

OFF

APU

AVAILON

EXT

MAN HIGH MAN

OFFFAILOFF

FAILOFF

APU BLEED BUTTONAVAIL (green)- Bleed air supply to left ECS PACK availableON (white)- Bleed air supply to left ECS PACK selected open

X-BLEED BUTTONHorizontal flow bar (white)- Cross bleed air supply to LH/RH ECS PACK selected openVertical flow bar (white) - Cross bleed air supply to LH/RH ECS PACK selected close

LH/RH BLEED BUTTONVertical flow bar (white)- Bleed air supply to LH/RH ECS PACK selected openOFF (white) - Bleed air supply to LH/RH ECS PACK selected close

EXT sign IndicatorEXT(white)- is an indication that the external supply door is open

Fig. 20 Controls and Indicators - ECS PanelThe selected position (not the actual position) of the various bleed air control valves isindicated on the related switch/light. With the exception of the X-BLEED and APUBLEED switch/lights, all indications are in the form of a bar symbolising an open valveand an OFF caption for a closed valve. The X-BLEED switch/light has a horizontal barto symbolise when the valve is open and a vertical bar for a closed valve. The APUBLEED switch/light has an ON and an AVAIL caption. The ON caption indicates thatthe switch/light is pressed in (APU bleed air selected on). The AVAIL caption iscontrolled by the APU available relay 125HB and indicates that APU bleed air isavailable. It does not indicate that the APU is delivering bleed air. The ECS panel isequipped with an EXT light indicating that the APU Access door is open whenilluminated and Ground air power source is attached.

Dornier 328

- 300

Training Manual

Pneumatic

Effectivity:328-300

- FO

R TRAINING PURPO

SES ONLY -

Issue

: Mar.

99 ETM

/XP

age: 36

- 35

REC FAN FAIL

REC FAN FAIL

FAIL

HX FAN FAILPACK OVHT


Honeywell

COCKPIT ENGINEATSENGINE

ATS

CABIN24 C

ECONOMY

BAGGAGE 23 C

PSI 45

LH PACK X-BLEED RH PACK

BLEEDLP HP

LHLPHP

RHAPU

SYSTEM 2/3ICE

PROTECTECSELECTR NEXTAPU

24 C

OVPRSSOVHTLEAK

FAILFAIL

OVPRSSOVHTLEAKLEAK

FAIL

FAIL

APU Bleed SOV

(green)- Shut-off valve selected close or automatically closed(white)- Shut-off valve open and selected openFAIL (amber)- Shut-off valve not in selected position

FAIL (amber)- Shut-off valve not in selected position

ATS-VALVE



LEAK APU (amber)- Bleed air leak in APU air duct (more 205C (400F))

LH/RH MAIN DUCT PRSOV

(green)- LH/RH low pressure reducing and shut-off valve open and selected open(white)- LH/RH low pressure reducing and shut-off valve close and selected closeFAIL (amber)- LH/RH low pressure reducing and shut-off valve not in selected positionFAIL (amber)- LH/RH low pressure reducing and shut-off valve not in selected position

LH/RH HP PRSOV

(green)- LH/RH high pressure reducing and shut-off valve automatically close or selected(white)- LH/RH high pressure reducing and shut-off valve open and selected openFAIL (amber)- LH/RH high pressure reducing and shut-off valve not closed but selected closed

LEAK

EXT

X - Bleed Valve

(green)- X-Bleed valve close and selected close

(white)- X-Bleed valve open and selected openFAIL (amber)- X-Bleed valve not in selected position

FAIL (amber)- X-Bleed valve not in selected position

OVPRSS LH/RH (amber)- Overpressure condition in LH/RH main bleed air duct (more than 37 psi)OVHT LH/RH (amber)- Overheat condition in LH/RH main bleed air duct (more 26510C (50918F))LEAK LH/RH and APU (amber)- Bleed air leak in LH/RH bleed air duct (more 205C (400F))

Fig. 21 ECS Page -

System Indications Sheet 1

Dornier 328 - 300Training ManualCPCS

Effectivity:328-300

- FOR TRAINING PURPOSES ONLY - Issue: Mar. 99ETM/XPage: 21 - 33

1.4.1 CAS Field Indications

Honeywell

MAINAHRSREF

DATA

MSG

FWC MESSAGE LINE 1FWC MESSAGE LINE 2FWC MESSAGE LINE 3FWC MESSAGE LINE 4FWC MESSAGE LINE 5FWC MESSAGE LINE 6FWC MESSAGE LINE 7FWC MESSAGE LINE 8FWC MESSAGE LINE 9FWC MESSAGE LINE 10FWC MESSAGE LINE 11FWC MESSAGE LINE 12FWC MESSAGE LINE 13FWC MESSAGE LINE 14FWC MESSAGE LINE 15

COPY

2870450 FF LBS / HR

FQ LBS 2870450

50018000 CABIN

XXFTFPM

NU

NDOIL

TEMPOIL

PRSS

20 20

24 CV/S

XX90.5

N2

910 ITT

80.3

N1

115.0

912

108.3 TOGA

NO SYNC

IGN

VIB VIB

IGNSTART START

CAS FIELD MESSAGESThe following messages can be displayed- CAB DIFF PRSS (amber)- CPCS AUTO FAIL (amber)- CPCS MISCOMPARE (amber)- CPCS CTRL MODE MAN (blue)- NO VALID LAND ELEV (blue)

CABIN ALTITUDEIndicates cabin altitude in auto/manualmode.CABIN ALTITUDE RATE OF CHANGEIndicates cabin altitude rate of change in auto/manual mode. increasing rate of change decreasing rate of change

Fig. 15 Messages and Indications on the CAS Field

Dornier 328

- 300

Training Manual

Pneumatic

Issue: Mar. 99

ETM/X

Page

: 36 - 18

- FO

R TRAINING PURPO

SES ONLY -

Effectivity:328-300

COWL PICCOLOTUBE (LIP ANTI-ICING)

INSTALLATION WITHINENGINE NACELLE

PRSOV

M

D

P

R

S

O

V

T

E

M

P

.

C

O

N

T

R

O

L

V

A

L

V

E

AIR TURBINESTARTER

TEMPERATURESENSOR

OVERTEMP.-SWITCH (OVHT1/2)

PRE-COOLERECS-BLEED.

OVERPRESSURESWITCH

CROSSFEEDVALVE

FLOW CONTROLSHUTOFF VALVE

ECSPACKLH

ECSPACKRH

T

E

M

P

E

R

A

T

U

R

E

S

W

I

T

C

H

(

O

V

H

T

3

)

2,5 in. NON RETURN

VALVE

OUTBOARDCONNECTOR

COOLER-DEICING-SYSTEM

ATS-VALVE

PRESSURESWITCH

(LP)

(HP)

28 V DC ESS BUSPre-Cooler

Pressure Regulatorand Relief Valve

see Detail A

see Detail B

TCVTCV

L

C

V

APU

HP PRSOV

THERMOSTAT

JETPUMPOPCSEICAS EICAS

WaterSeparator Pressure

Switch

De-ice BleedShut off Valve


AirfoilDeicing

RH EngineIdentical

to LH Side

Fig. 12 Bleed Air

Distribution - Functional Schem

atic

Dornier 328

- 300

Training Manual

Air C

onditio

ning

Issue: Mar. 99

ETM/X

Page

: 21 - 48

- FO

R TRAINING PURPO

SES ONLY

-

Effectivity:328-300

4 SYSTEM

IND

ICATIONS

FAIL


COCKPIT ENGINEATS

CABIN24 C

ECONOMY

BAGGAGE 23 C

PSI 45


BLEEDHP

LHLPHP

RHAPU

SYSTEM 2/3ICE


24 C

OVPRSS

FAIL

OVPRSSOVHTLEAKLEAK

FAIL

FAIL

LEAK

EXT

LH/RH PACK (FCSOV)

REC FAN FAIL (amber)- Fwd/aft recirculation fan failed

ECONOMY (blue)- Airflow is selected to normal

High (blue)

Honeywell

ENGINEATS

LP

OVHTLEAK

FAIL


REC FAN FAIL

REC FAN FAIL

LH/RH PACK OVHT (amber)- LH/RH ECS PACK overheat

LH/RH HX FAN FAIL (amber)- LH/RH ground cooling fan failed

COCKPIT / CABIN (SYNOPTIC)Digital readout (white)- Digital readout of temperature in C (provide the respective TEMP CRTL mode button is in auto)

(green)- LH/RH flow control and shut-off valve is selected open(white)- LH/RH flow control and shut-off valve is selected closed

- Airflow is selected to high mode operation




1.4.2 CPCS / Oxygen Page and Red Warning Panel

OXYGEN

APU FIRE

LH ENGFIRE

L OIL PRS

BAT1 OVHT

CAB ALT T/O CONF

LAV FIRE

PFD DOORS R OIL PRS

BAT2 OVHT

RH ENGFIRE

CARG FIRE

18 %FAIL CREW PRSS LOWPAX PRSS LOW

Honeywell

PAX AUTO

OXY QTY 1

FT00 0.00 PSI 0 FPM

0 0DN

0

UP

CABIN RATEDIFF PRSSCABINALTITUDE

LAND ELEV14000 FT

CTRL MODEAUTO

SYSTEM 3/3NEXTDOORSCPCS/

OXYGENSYS

MAINTSENSOR

DATA

CABIN RATEDigital readout (white) -2500 to +2500FPMAnalog range- normal in white 0 to 1000 FPM- amber 1000 to 2500FPM

CABIN ALT (red)- cabin altitude above 9500200 ft annunciated by a TRIPLE CHIME (chime inhibited during take-off phase

CTRL MODEMAN- indicates that cabin pressurization is manually controlled by the MANCAB ALT selectorAUTO - indicates that pressurization control is in auto mode

LAND ELEVAUTO MODE (green)-digital read is manually selectedMANUAL MODE (white)-digital readout show dashes

AUTO CTRL FAIL (amber)-cabin pressurization AUTOCONTROL MODE failed

MISCOMPARE (amber)-cabin pressurization rate of change signal (main and backup) differ by more than 600 ft/min for more than20sOR- cabin altitude signals (main and backup) differ by more than 600 ft for more than 20s

CABIN ALTITUDE Digital readout (white) -1500 to +9500 ft Digital readout (red) +9500 to +20000 ft Analog range white -1500 to +9500 ft red +9500 to +15000ft

DIFFERENTIAL PRESS Digital readout (amber) -0,5 to -0,2 psi Digital readout (white) -0,2 to +6,9 psi Digital readout (amber) +6,9 to +7,5 psi Analog range is identical to digital readout

MISCOMPAREAUTO CTRL FAIL

Fig. 16 Messages and Indications on CPCS/Oxygen Page and Red Warning Panel

Dornier 328

- 300

Training Manual

Ice and R

ain

Effectivity:328-300

- FO

R TRAINING PURPO

SES ONLY -

Issue

: Mar.

99ETM

/XPage: 30-

55

Honeywell

SYSTEM 2 / 3ICE

PROTECTELECTR ECS APU NEXT

BLEED BLEED

ON

WSHLD

ENGINE ANTI- ICE

AIRFOIL DEICERSINGLE FAIL

LH RHICE DETECTEDFAIL

FAIL

FAIL

FAIL

FAIL

PRSS FAILTEMP FAIL

PRSS FAILTEMP FAIL

INTAKE OVERHEAT

TTO HEAT FAILANTI-ICE HEAT FAIL

INTAKE OVERHEAT

TTO HEAT FAILANTI-ICE HEAT FAIL

FAIL (amber) Indicates either front windshield heater failed

FAIL (amber) Indicates either side windshield heater failed

LH/RH Synoptic ISW, MSW, OSW bootsSynoptic (dark, green outline) Indicates respective boot deflatedSynoptic (full green) Indicates respective boot inflatedSynoptic (amber) Indicates respective boot failed

LH/RH Synoptic OSS, ISS bootsSynoptic (dark, green outline) Indicates respective boot deflatedSynoptic (full green) Indicates respective boot inflatedSynoptic (amber) Indicates respective boot failed

PRSS LOW (amber) Indicates insufficient de-ice bleed air pressureSENS FAIL (amber) Indicates de-ice bleed air switch failed

ICE DETECTED (blue) Indicates ice detectedICE DETECTOR FAILED Indicates ice detector self test failed

ANTI-ICE HEAT FAIL (amber) inlet anti-icing engine anti-icing SOV has failed in open or closed position

INTAKE OVER HEAT (amber) Intake/Cowl anti-icing switched ON and OAT 10C

TTO HEAT FAILamber) engine inlet Total Temoerature Sensor failure

Isolation Valve positionCLOSED (white)

OPEN (green)

Engine Anti-IceOFF (blue) Indicates LH/RH engine intake button OFFON (blue) Indicates LH/RH engine intake button ONFAIL (amber) Low Pressure High Temperature Isolation Valve failed

OFF (blue) Indicates airfoil selector set to OFFSLOW (blue) Indicates airfoil selector set to SFAST (blue) Indicates airfoil selector set to FFAST FAIL (amber) Indicates FAST MODE cycle failedSINGLE (blue) Indicates airfoil SINGLE button has been pushedSINGLE FAIL (amber) Indicates FAST MODE cycle failed

Fig. 37

Ice

Protection

Page Indications

Dornier 328 - 300Training ManualIce and Rain



Honeywell

FUELL RLRLRLR

TRANSFER MON 102390TRANSFER MON 102390TRANSFER LOWTRANSFER LOWFILTER BYPASSFILTER BYPASSMOTFLOW NRV FAILMOTFLOW NRV FAIL

CPCSBACKUP INSTRUMENTSAUTO CTRL MAINTOXYGENQTY ACCURACY

HYDRAULICSANTISKID MAINTPROXI MAINT

MAIN OIL FILTMAIN OIL FILTENG CHIPS DETECTENG CHIPS DETECT

MAX BRAKE TEMPERATURESLOUT 345 CLINB 123 CRINB 234 CROUT 456 C

FLIGHT CONTROLSELEV TRIM MOT FAILRUDDER LIMIT FAILGND SPOILER FAIL

ELECTRTRU FAIL


SYSTEM 3/3CPCS/

OXYGENDOORS SYS

MAINTSENSOR

DATANEXT

ICE PROTECTLRLRLRLRLRLRLR

SWDW TEMPSWDW TEMPFWDW TEMPFWDW TEMPINTAKE ICE PRSSINTAKE ICE PRSSCONE ICE POS SWCONE ICE POS SWTTO PROBE 1 FAILTTO PROBE 1 FAILTTO PROBE 2 FAILTTO PROBE 2 FAILBLEED OVTEMPBLEED OVTEMP

ENGINELRLR

ICE PROTECTL-R SWDW SideWindow Sensor failureL-R FWDW Windshied Sensor failureL-R INTAKE ICE PRSS Low pressure behind the cowl inlet SOVL-R CONE ICE POS SW SOV failkure for Plenum and inlet cone anti-icingL-R TTO1/1FAILTotal Temperature sensor heatingin the engine inlet failedL-R BLEED OVERTEMP airfoil de-cing system temperatue exceeds the limit (165C)

Fig. 38 System Maintenance Page Indications

Dornier 328 - 300Training ManualIce and Rain

Effectivity:328-300

- FOR TRAINING PURPOSES ONLY - Issue: Mar. 99ETM/XPage: 30- 15

2.2 OPERATION

CYCLE

28 V DC ESS BUS

EjectorPumpCPCSEICAS

EICAS

HP

C C C C C C C C

Air Condition

Pre-Cooler

LowPressure Switch

OvertempSwitch

Isolation Valve

Ejector FlowControl Valvessee Detail C

TimerManual

TimerAutom.

Wing De-Icer Boots LH Wing De-Icer Boots RH

Vertical Stabilizer Boots

Horizontal Stabilizer Boots

SINGLE

WaterSeparator

PressureSwitch

Pressure Regulator and Relief Valve

EICAS

HPAir Condition

Pre-Cooler

LowPressure Switch

OvertempSwitch

Isolation Valve

WaterSeparator

Pressure Reg and Relief Va

Fig. 10 Airfoil De-icing System - Functional Schematic

Dornier 328 - 300

Training Manual

Oxygen

Effectivity:328-300

- FO

R TRAINING PURPO

SES ONLY -

Issue: Mar. 99

ETM/X

Page: 35 - 25

SeperationValve

LP SwitchLP Switch

P

B

E

H

o

o

d

F

i

r

s

t

A

i

d

O

u

t

l

e

t

Altitude Switch

ShuttleValve

Seal Valve, Passenger

Seal Valve,Crew

First AidOutlet

PBE Hood (Option)

Seal Valve, Passenger

First AidOutlet

Solenoid Valve

Solenoid Valve

ContentsGage

Pressure/Temp

Sensor

Filler Valve DischargeIndicator

Crew System

Passenger System

Seal Valve,Crew

E

I

C

A

S

O

x

y

.

P

a

n

e

l

Electrical Circuit

Crew Mask

Passenger Drop-out Unit

First AidOutlet

Regulator/Altitude Compensator

Shuttle Valve Pax

Fig. 16 O

xygen System - System

Schematic

Dornier 328 - 300

Training Manual

Oxygen

Effectivity:328-300

- FO

R TRAINING PURPO

SES ONLY -

Issue: Mar. 99

ETM/X

Page: 35 - 31

MISCOMPAREAUTO CTRL FAIL

Honeywell

OXY QTY 1

FT00 0.00 PSI 0 FPM

0 0DN

0

UP

CABIN RATEDIFF PRSSCABINALTITUDE

LAND ELEV14000 FT

CTRL MODEAUTO

SYSTEM 3/3NEXTDOORSCPCS/

OXYGENSYS

MAINTSENSOR

DATA

PAX AUTOCREW PRSS LOWPAX PRSS LOW

PAX AUTO- Pax-Supply switch in ON position- Drop-out switch in AUTO position- Altitude switch open (13800700ft) or- Pax-Supply switch in ON position- Drop-out switch in MAN positionPAX OFF- Pax-Supply switch in OFF position

CREW PRESS LOW- Pressure crew oxygen

Dornier 328

- 300

Training Manual

Fuel

Effectivity:328-300

- FO

R TRAINING PURPO

SES ONLY

-

Issue

: Mar.

99 ETM

/XP

age: 28

- 21

2.3 FUEL SYSTEM

CONTRO

LS2.3.1

Fuel Panel

RHENGINE

SOV

AUTO

ELPMPJETPMPJETPMPELPMP

SOV

AUTO

X-FEED

LHENGINE FUEL

FAILON

FAILOFF

FAILOFF

FAILON

FAILOFF

FAILOFF

Engine Shut-off (SOV) LightVertical flow bar (green) Engine SOV openHorizontal flow bar (green) Engine SOV closed

ELPMP AUTO ButtonNormal (dark) Electrical booster pump in AUTO modeFAIL (amber) Electrical booster pump has failedOFF (white) AUTO mode swiched OFF

ELPMP ButtonNormal (dark) Electrical booster pump switched OFFFAIL (amber) Electrical booster pump has failedON (white) Electrical booster pump manually switched ON independent from ELPMP AUTO mode

JETPMP ButtonNormal (dark) Motive flow valve open Jet pump in operationFAIL (amber) Jet pump has failedOFF (white) Motive flow valve OFF Jet pump manually switched OFF

X-FEED SelectorMid position No crossfeedLeft position LH engine is crossfed from RH TankgroupRight position RH engine is crossfed from LH Tankgroup

X-FEED LightVertical flow bar (green) Crossfeed valve closedHorizontal flow bar (green) Crossfeed valve open (active in direction of the X-FEED selector)

Fig. 21 Fuel Control P

anel

Dornier 328

- 300

Training Manual

Fuel

Effectivity:328-300

- FO

R TRAINING PURPO

SES ONLY

-

Issue

: Mar.

99 ETM

/XP

age: 28

- 23

2.3.3 Refu

el/Defuel P

an

el

Master SwitchON Refuel/defuel control panel activated. FUEL CONECT OPEN message is displayed from valve positionOFF Refuel/defuel control panel deactivated. FUEL CONECT OPEN message is displayed only if access panel is not closed.

Left/Right High Level Warning Lights Indicates a refueling shut-off valve failure when blinking

Data Entry Switch For entering calibration data and resetting error memory

Fuel Quantity Remaining Display Shows the remaining amount of fuel in the LH / RH wing tank groups

Preselect Qty Display Shows the preselected amount of fuel or Communication modes with the processors.

Preselector SwitchINC/DEC In/decreases the preselected amount of fuel on the PRESELECT QTY display

Left/Right Refueling Valves LightsCLOSED Refueling valves are closed (OPEN lights extinguished)OPEN Refueling valves are opened (CLOSED lights extinguished)Left/Right Refueling/Defuel SwitchesRefuel OPEN light illuminates when the system is under pressure to indicate refueling valve is opened (CLOSED light extinguished) FUEL QTY REMAINING display is continuously ascending.Defuel OPEN light illuminates when the system is under negative pressure to indicate refueling valve is opened (CLOSED light extinguished) FUEL QTY REMAINING display is continuously decending.Middel position Refuel/Defuel sequence is de-activated.

INTERTANK XFER SwitchTO LH Fuel is transfered to the LH wing tank group when the RH ELPMP is switched on (fuel connect valve is open).TO RH Fuel is transfered to the RH wing tank group when the LH ELPMP is switched on (fuel connect valve and x-feed valve is open).OFF Intertank transfer is de-activated.

DEC

DATAENTRY

LEFT RIGHTLEFT RIGHT

REFUELING VALVESCLSD

OPEN

HI LEVELWARNING

REFUELAUTO

DEFUELINCINTERTANK XFER

TOLH

TORH

OFFAUTOMATIC MANUAL

FUEL QUANTITY REMANING

PRESELECTED QTY

125 130

3416LBS KGS

Fig. 23 Refuel/Defuel Control Panel

Dornier 328

- 300

Training Manual

Fuel

Effectivity:328-300

- FO

R TRAINING PURPO

SES ONLY

-

Issue

: Mar.

99 ETM

/XP

age: 28

- 35

RHENGINE

SOV

AUTO

ELPMPJETPMPJETPMPELPMP

SOV

AUTO

X-FEED

LHENGINE

FUEL

FAILON

FAILOFF

FAILOFF

FAILON

FAILOFF

FAILOFF

DEC

DATAENTRY

LEFT RIGHTLEFT RIGHT

REFUELING VALVESCLSD

OPEN

HI LEVELWARNING

REFUELAUTO

DEFUELINCINTERTANK XFER

TOLH

TORH

OFFAUTOMATIC MANUAL

FUEL QUANTITY REMANING

PRESELECTED QTY

1708 1708

0LBS KGS

Before this procedure can be carried out, the aircraft must be suction defueled and/or the fuel level in the inner tank must be 80kg (170lbs)or below to make sure the refuel valves are closed.

CAUTION: DO NOT LET THE LEVEL OF FUEL IN THE LH AND/OR RH WING FEEDER TANK GO BELOW 9 kg. DRY OPERATION OF THE PUMP CAN CAUSE AN EXPLOSION.

For further information refer to Job Instruction CardDEFUEL THROUGH THE PRESSURE REFUEL/DEFUEL COUPLING - DEFUELING

Jet Booster Pump

Fuel Shut-off

Valve

APU Shut-offValve

Motive FuelCheckValve

Motive FuelCheck ValveValve

CrossfeedValve

ConnectValve Fuel

Shut-offValve

RefuelingAdapter

Jet Transfer Pump

Electrical Booster Pump Flapper Valve

Relief Valve

Temperature TransducerPressure Switch

Pressure RefuelingMotive Fuel FlowEngine FeedFuel Transfer

Inner Tank

Feeder TankOuter Tank

M

MM

M

MM

Fig. 31 Pu

mp

defuel th

rough the pressure refuel/defuel

coupling

Dornier 328 - 300Training ManualFuel

Effectivity:328-300


5.4 EICAS MESSAGES AND INDICATIONS

5.4.1 Primary EICAS Page

Honeywell

MAINAHRSREF

DATA

MSGCOPY

2870450 FF LBS / HR

FQ LBS 2870

450

50018000 CABIN

XXFTFPM

NU

NDOIL

TEMPOIL

PRSS

20 20

24 CV/S

XX90.5

N2

910 ITT

80.3

N1

115.0

912

108.3 TOGA

NO SYNC

IGN

VIB VIB

IGNSTART START

CAS FIELD MESSAGESThe following messages can be displayed: L-R FUEL SOV CLSD L-R FUEL SOV FAIL FUEL ELPMP FAIL FUEL ELPMP ON FUEL JETPMP FAIL FUEL JETPMP ON FUEL XFEED FAIL FUEL CONN VLV OPEN L-R FUEL LOW/VMO FUEL TANK TEMP FUEL FILT BYPASS L-R FUE PRSS LOW FUEL ASYM MISCOMP - FUEL L-R FUEL TRANS FAIL L-R FUEL LOW FAIL L-R FUEL QTY FAIL L-R FUEL CONTAMIN L-R FEED TANK LOW FUEL FEED TEMP FUEL XFEED PMP FUEL FEED ACTIVE L-R FUEL QTY ACCUR FUEL BALANCE

FUEL FLOWDigital readout for fuel flowin kg or lbs per hour

WING FUEL QTY INDICATOR Digital readout in kg or lbs per hour forfuel quantity in LH/RH wing tank group.Digital readout changes to amber withan amber C in front when calculated

Fig. 39 Primary EICAS Display Messages and Indications

Do

rnier 328 - 300Training M

anualHydraulic Power

Effectivity:328-300

- FO

R TRAINING PURPO

SES ONLY -

Issue

: Mar. 99 ETM

/XPage:

29 - 43

4.3 EICAS IN

DICATIO

NS

PRSS TEMP

FLIGHTCONTROL

HYDR ENGINE FUEL NEXT

SYST 1 / 3

3000 6060

OFF

CPSI

3000PSI

NWS INOP

LH RH

NWS BYPASS FAIL

PROXI SSA FAILPROXI SSB FAIL

PROXI MLG WOW FAILPROXI NLG WOW FAIL

PROXI LOCK FAILPROXI BYPASS FAIL

NORM ANTI SKID FAILALT ANTISKID DEGR

50 C25 C98 C23 C

Main HydraulicSystem Temperature (A&B)Normal (white) -60C and 100CHigh (amber) >102C to 135CHigh (red) >135C to 150C

Main HydraulicSystem Pressure (A&B)Normal (white) >1813 and

Dornier 328

- 300

Training Manual

Fuel

Issue: Mar. 99

ETM/X

Page

: 28 - 52

- FO

R TRAINING PURPO

SES ONLY

-

Effectivity:328-300

5.4.2 M

FD Fuel System

Page

Honeywell

FLIGHTCONTROL

HYDR ENGINE FUEL NEXTSYSTEM 1/3

1935LBS 3960200010

PRESEL QTYTANK TEMP. C

LBS2025 LBS

780

X-FEED

LHENG

JETPMP ONELPMP OFF

RHENG

770 775FF LBS/HRUSED LBS

31 C30 C

185 850 185990

614 617

HP FILTER

PRSS LOW

FAILFAIL

FAIL

HP FILTER

PRSS LOW

APU

TOTAL QTY

970

JETPMP ONELPMP OFF

FUEL TANK TEMPERATUREDigital readout range (white) Fuel tank temperature above -36C or below+53CDigital readout range (amber) Fuel tank temperature below -38C or above +55C

FEEDER TANK FUEL QTYOUTER TANK FUEL QTY

INNER TANK FUEL QTY

TOTAL FUEL QTY and WING TANK GROUPDigital readout in kg or lbs per hour for fuel quantity in LH/RH wing tank group. Digital readout changes to amber with an amber"C" in front when calculated.

LH /RH ENINGE and APU FUEL SOVSYNOPTIC and FAIL light (green) Fuel shut-off valve selected open and valve opened. (amberAPU SOV white) Fuel shut-off valve selected close and valve closed. FAIL (amber) Fuel shut-off valve selected open but valve closed. FAIL (amber) Fuel shut-off valve selected close but valve opened

X-FEED SOV SYNOPTIC and FAIL light (green) Crossfeed valve selected close a. valve closed. (green) Crossfeed valve seleted selected RH tank to LH side and valve opened. (green) Crossfeed valve seleted selected LH tank to RH side and valve opened. FAIL (amber) Crossfeed valve seleted selected to LH or RH side but valve closed FAIL (amber) Crossfeed valve seleted selected close but valve opened.

FUEL FLOWDigital readout for fuel flowin kg or lbs per hour

FUEL USEDDigital readout for fuelused in kg or lbs per hour

FUEL TEMPERATURE(downstream fuel heater)Digital readout range (white) from 4C to 67CDigital readout range (amber) below 3C and above 68C

ELPMP FAIL (amber) Electrical booster pump has failedELPMP ON (amber) Electrical booster pump manually switched ON and feed to side during crossfeed Electrical booster pump switched OFF and the speed switch in the pump motor is indicating an active pumpELPMP ON (blue) Electrical booster pump manually switched ON Electrical booster pump automatically switched ONELPMP OFF (blue) Electrical booster pump manually switched OFF

JETPMP FAIL (amber) Jet booster pump has failedJETPMP ON (amber) Jet booster pump outlet pressure above 8,5 psi at the at the feed to side during crossfeedJETPMP ON (blue) Jet booster pump manually switched ONJETPMP OFF (blue) Jet booster pump manually switched OFF

HP FILTER (amber) High pressure fuel filter impending bypass indication

PRESELECTED FUEL QTYDigital readout in kg or lbs for preselected fuel quantity, shows dashes if no fuel quantity isselected for refueling.

PRSS LOW (amber) fuel pressure below 5psi

Fig. 40 Fuel System

Page Messages and Indications

Dornier 328 - 300Training Manual Flight Controls



8 CONTROLS AND INDICATIONS

8.1 SYSTEM CONTROLS

ELEV

STBY

TRIM

UP

RH

RUD

LH

AILSTBY

OFF

PRESSTO

RESET

STBYELEV

UP

RHLH AILRHLH AIL

DN

AILERON MAINTrim SwitchesOperates the normal aileron trim circuit

AILERON STBYTrim SwitchesOperates the standby aileron trim circuit andlocks out main trim

STBY AIL Reset Switch/LightNormal (dark) Main trim cicuit is activeSTBY AIL (withe) Standby trim circuit is activePushbutton when P/B is pressed the normal trim circuit is reactivated

STBY ELEV Reset Switch/LightNormal (dark) Main trim cicuit is activeSTBY AIL (withe) Standby trim circuit is activePushbutton when P/B is pressed the normal trim circuit is reactivated

ELEVATOR STBYTrim SwitchesOperates the standby elevator trim circuit andlocks out main trim

RUDDER MAINTrim SwitchesOperates the normal rudder trim circuit

Fig. 64 Trim Control Panel

Dornier 328

- 300

Training Manual

Flight Controls

Effectivity:328-300

- FO

R TRAINING PURPO

SES ONLY -

Issue

: Mar.

99 ETM

/XP

age: 27

- 131

GROUND SPOILER SWITCH/LIGHTNormal operation (dark) Ground spoiler switched on but is not armedOFF (white) Ground spoiler is switched offARM (white) Ground spoiler is armed if - gear is down and locked - condition lever are above 85% HMU - Mod.10 and 20, power lever is in or above FI (24) Mod.30, power lever is in or above 28

+

-

TRENDREFUEL QTY

QTY

EXCEED IMT/FDR

UN-LIMIT

ARM

OFF

RUD

LIMIT

GND

SPOIL

ON

ARM

ELTBAT T/O CONFIG

TESTLH RHSTALL WARN

PUSHER

EMGOFF

BACK UP

PUSHER DISARM SWITCH/LIGHTNormal operation (dark) Stick pusher is armedOFF (white) Stick pusher is disarmed (can only be reset on ground)

RUDDER LIMITER SWITCH/LIGHTNormal operation (dark) Rudder limiter is controlled from ADC1 and ADC1UNLIMIT (white) Activated if limiter fails in LIMITED position (below 160kts), limiter STBY motor manually unlimits the rudder

STALL WARNING TESTBUTTONSLH Captains shaker is activatedRH F/O shaker is activatedBoth buttons Stick pusher is activatedNote: Can only be carried out with AOA sensors heated

Fig. 67 LH and RH M

iscellaneous Panel




8.2 SYSTEM INDICATIONS

Honeywell

MAINAHRSREF

DATA

MSG


COPY

2870450 FF LBS / HR

FQ LBS 2870

450

50018000 CABIN

XXFTFPM

NU

NDOIL

TEMPOIL

PRSS

20 20

24 CV/S

XX90.5

N2

910 ITT

80.3

N1

115.0

912

108.3 TOGA

NO SYNC

IGN

VIB VIB

IGNSTART START

Fig. 68 Primary EICAS Page




Spring Tab Locking Lever

A

A

Torsion Bar Spring

Torsion Bar Connection to Rudder

Torsion Bar Connection to Rudder

Spring Tab Lock Actuator

Spring TabConnection

Spring Tab Drive Rods

Rudder Drive Rod (Input)

Actuator Connection to Rudder

Fig. 18 Spring Tab Lever Assembly

Dornier 328 - 300Training ManualFlight Controls

Effectivity:328-300


Honeywell

SYSTEM 1 / 3HYDR ENGINE FUEL NEXTFLIGHT

CONTROL

ROLLGND GND

ROLL

14 14

NU

ND

AIL

RUD

ELEV

TRIMTRIM SPEED FAST

PITCH TRIM ASYM

RUDDERAILERON

ELEVATORLH RH

FLAPS

1220

RUDDER LIMITEDAIL DISCONNECT

ELEV DISCONNECT

GND SPOILER OFFFLAP ASYM

FLAP CTRL FAIL

32

Fig. 69 Flight Control Page




Honeywell

FUELL RLRLRLR

TRANSFER MON 102390TRANSFER MON 102390TRANSFER LOWTRANSFER LOWFILTER BYPASSFILTER BYPASSMOTFLOW NRV FAILMOTFLOW NRV FAIL

CPCSBACKUP INSTRUMENTSAUTO CTRL MAINTOXYGENQTY ACCURACY

HYDRAULICSANTISKID MAINTPROXI MAINT

MAIN OIL FILTMAIN OIL FILTENG CHIPS DETECTENG CHIPS DETECT

MAX BRAKE TEMPERATURESLOUT 345 CLINB 123 CRINB 234 CROUT 456 C

FLIGHT CONTROLSELEV TRIM MOT FAILRUDDER LIMIT FAILGND SPOILER FAIL

ELECTRTRU FAIL


SYSTEM 3/3CPCS/

OXYGENDOORS SYS

MAINTSENSOR

DATANEXT

ICE PROTECTLRLRLRLRLRLRLR

SWDW TEMPSWDW TEMPFWDW TEMPFWDW TEMPINTAKE ICE PRSSINTAKE ICE PRSSCONE ICE POS SWCONE ICE POS SWTTO PROBE 1 FAILTTO PROBE 1 FAILTTO PROBE 2 FAILTTO PROBE 2 FAILBLEED OVTEMPBLEED OVTEMP

ENGINELRLR

Fig. 70 System Maintenance Page




RMU Backup Page 1 RMU Backup Page 2

XXXXXXX.X

XXXXXXXXX

XXXXXXX.X

XXXXXX.X

ITTN2VIBFQ

ALT DPMSGMORE

TUNESQ DIM 1/2 STO

ID PGE TST DME

85.2 N1 84.7IGN IGN

CPCS AUTO FAILPITOT S HEAT FAILL AOA FAILR AOA FAILBATT 1 FAILBATT 2 FAIL

XXXX XXXXFFXXX XXXOIL TEMPXXX XXXOIL PRS

RUDDER LIMITEDRETURN

TUNESQ DIM 1/2 STO

ID PGE TST DME

Fig. 72 RMU - Engine Page 2

Dornier 328 - 300Training ManualLanding Gear



4.2.1! Normal System

4.2.1.1! Landing Gear Control Lever 2GA

LDG GEAR

UP DN

DN LCKREL

TEST

+

UNLK

UNLK

UNLK

UP

DN

Gear Unlock LightUNLK (red) Illuminated if respective Gear is not UP and locked or DN and locked (transit or unsafe) or illuminate if landing failed to extend or retract

Gear Warning Lightred in combination with a not mutable aural warning (HI-LO chime) triggered if both PL are

Dornier 328 - 300

Training Manual

Doors

Issue: Mar. 99

ETM/X

Page: 52 - 30- FO

R TRAINING PURPO

SES ONLY -

Effectivity:328-300

Honeywell

SYSTEM 3 / 3DOORSCPCS/

OXYGEN

PAX

EMERG

CABIN

BAGGAGE

HATCH

SWITCH FAIL

COCKPIT

EMERG

SERVICE

GNDAIR

NEXTSYSMAINT

SENSORDATA

OPEN

OPEN

PAX Door synoptic Synoptic CLOSED (green) Service door closed and lockedSynoptic OPEN (red) Service door not locked discrepancy between both sensors detectedSynoptic CLOSED (amber) Single sensor or interface failureCross (amber) Double sensor or interface failure

BAGGAGE Door synoptic Synoptic CLOSED (green) Baggage door closed and lockedOPEN (red) Baggage door not lockeded discrepancy between both sensors detectedSynoptic CLOSED (amber) Single sensor or interface failureCross (amber) Double sensor or interface failure

EMERG LH/RH Exit synoptic Synoptic CLOSED (green) Emergency exit closed and lockedSynoptic OPEN (red) Emergency exit not lockedCross (amber) Sensor or interface failure

SWITCH FAIL (amber)Indicates a sensor failureor discrepancy of twocorresponding sensors

HATCH synoptic Synoptic CLOSED (green) Hatch door closed and lockedSynoptic OPEN (red) Hatch door not lockedCross (amber) Sensor or interface failure

SERVICE Door synoptic Synoptic CLOSED (green) Service door closed and lockedOPEN (red) Service door not locked discrepancy between both sensors detectedSynoptic CLOSED (amber) Single sensor or interface failureCross (amber) Double sensor or interface failure

GND AIR synoptic (optional)Synoptic CLOSED (green) Ground air door closed and lockedOPEN (red) Ground air door not locked

EXT AIR

Fig. 16 Door System

Page

Dornier 328 - 300

Training Manual

Starting

Issue: Mar. 99

ETM/X

Page: 80 12- FO

R TRAINING PURPO

SES ONLY -

Effectivity:328-300

COWL PICCOLOTUBE (LIP ANTI-ICING)

INSTALLATION WITHINENGINE NACELLE

PRSOV

M

D

P

R

S

O

V

T

E

M

P

.

C

O

N

T

R

O

L

V

A

L

V

E

AIR TURBINESTARTER

TEMPERATURESENSOR

OVERTEMP.-SWITCH (OVHT1/2)

PRE-COOLERECS-BLEED.

OVERPRESSURESWITCH

CROSSFEEDVALVE

FLOW CONTROLSHUTOFF VALVE

ECSPACKLH

ECSPACKRH

T

E

M

P

E

R

A

T

U

R

E

S

W

I

T

C

H

(

O

V

H

T

3

)

2,5 in. NON RETURN

VALVE

OUTBOARDCONNECTOR

COOLER-DEICING-SYSTEM

ATS-VALVE

PRESSURESWITCH

(LP)

(HP)

28 V DC ESS BUSPre-Cooler

Pressure Regulatorand Relief Valve

see Detail A

see Detail B

TCVTCV

L

C

V

APU

HP PRSOV

THERMOSTAT

C

JETPUMPOPCSEICAS EICAS

WaterSeparator Pressure

Switch



AirfoilDeicing

C

RH EngineIdentical

to LH Side

Fig. 6 Pneumatic Diagram

Dornier 328 - 300Training ManualStarting

Effectivity:328-300

- FOR TRAINING PURPOSES ONLY - Issue: Mar. 99 ETM/XPage: 80 19

5! CONTROLS AND INDICATION

5.1! STARTING PANEL

IGNCONT

IGNCONT

RUNOFF

VENT

LH ENGINESTART

VENTOFF

RUN

RH

STARTSTART

Fig. 8 Starting Panel

LHPACK

RHPACK

X-BLEED

LH RH

COLD HOT COLD HOT

TEMP SEL

CABIN

EFIS AVIONICRECIRC

FLOWMODE

COCKPIT

ECSFANS

OFF

OFF

OFF

OFF

APU

AVAILON

EXT

MAN HIGH MAN

OFFFAILOFF

FAILOFF

APU BLEED BUTTONAVAIL (green)- Bleed air supply to left ECS PACK availableON (white)- Bleed air supply to left ECS PACK selected open

X-BLEED BUTTONHorizontal flow bar (white)- Cross bleed air supply to LH/RH ECS PACK selected openVertical flow bar (white) - Cross bleed air supply to LH/RH ECS PACK selected close

LH/RH BLEED BUTTONVertical flow bar (white)- Bleed air supply to LH/RH ECS PACK selected openOFF (white) - Bleed air supply to LH/RH ECS PACK selected close

EXT sign IndicatorEXT(white)- is an indication that the external supply door is open

Fig. 9 ECS Panel

Dornier 328 - 300

Training Manual

Starting

Issue: Mar. 99

ETM/X

Page: 80 20- FO

R TRAINING PURPO

SES ONLY -

Effectivity:328-300

5.2!SYSTEM

INDICATIONS

REC FAN FAIL

REC FAN FAIL

FAIL



Honeywell

COCKPIT ENGINEATSENGINE

ATS

CABIN24 !C

ECONOMY

BAGGAGE 23 !C

PSI 45


BLEEDLP HP

LHLPHP

RHAPU

SYSTEM 2/3ICE


24 !C

OVPRSSOVHTLEAK

FAILFAIL

OVPRSSOVHTLEAKLEAK

FAIL

FAIL

APU Bleed SOV



ATS-VALVE



LEAK APU (amber)- Bleed air leak in APU air duct (more 205!C (400!F))

LH/RH MAIN DUCT PRSOV

(green)- LH/RH low pressure reducing and shut-off valve open and selected open(white)- LH/RH low pressure reducing and shut-off valve close and selected closeFAIL (amber)- LH/RH low pressure reducing and shut-off valve not in selected positionFAIL (amber)- LH/RH low pressure reducing and shut-off valve not in selected position

LH/RH HP PRSOV

(green)- LH/RH high pressure reducing and shut-off valve automatically close or selected(white)- LH/RH high pressure reducing and shut-off valve open and selected openFAIL (amber)- LH/RH high pressure reducing and shut-off valve not closed but selected closed

LEAK

EXT

X - Bleed Valve

(green)- X-Bleed valve close and selected close

(white)- X-Bleed valve open and selected openFAIL (amber)- X-Bleed valve not in selected position

FAIL (amber)- X-Bleed valve not in selected position

OVPRSS LH/RH (amber)- Overpressure condition in LH/RH main bleed air duct (more than 37 psi)OVHT LH/RH (amber)- Overheat condition in LH/RH main bleed air duct (more 265"10!C (509"18!F))LEAK LH/RH and APU (amber)- Bleed air leak in LH/RH bleed air duct (more 205!C (400!F))

Fig. 10 ECS Page

Dornier 328 - 300Training ManualStarting

Effectivity:328-300

- FOR TRAINING PURPOSES ONLY - Issue: Mar. 99 ETM/XPage: 80 21

Honeywell

FLIGHTCONTROL

HYDR ENGINE FUEL NEXTSYSTEM 1/3

FUEL

OILPRSS

OILTEMP

VIB

60.3 %

680 !C % N1

N2

ITT

60.3 %

680 !C108.3 %

FF LBS/HR

LR

FADEC MINORFADEC FAULT

LLLLLLL

EXCEEDANCES

ENGINE N1ENG ITT ZONE BENG ITT ZONE CENGINE N2ENGINE OIL TEMPENGINE OIL PRESSENGINE N1

RRRRR

ENG ITT ZONE BENG ITT ZONE CENGINE N2ENGINE OIL TEMPENGINE OIL PRESS

108.3

450

FAIL FAIL

PRSS LOW

IGN START

FUEL

450

PRSS LOW

IGN

57

0.4

PSI

in/sec 0.4 in/sec

57 PSI

56 !C 57 !C

Fig. 11 Engine Page

Dornier 328 - 300Training ManualAPU



8 49-70 ENGINE INDICATION

8.1 GENERAL

8.1.1 APU Systempage

ELECTRIC

200 AGEN OVHTGEN FAIL

READY TO LOADFUEL SOV CLOSED

OVERSPEEDOVERTEMP EGT

OVERCURRENT ECUOIL PRESS LOWOIL TEMP HIGH

LEAK

FAIL

ECS

EXT

ENGINEATS

BLEEDELECTRIC PWR

APU

SYSTEM 2/3APUICE


90 650

EGTN

PT 0068

Honeywell

Fig. 51 APU Systempage

Dornier 328 - 300Training ManualPowerplant

Effectivity:328-300

- FOR TRAINING PURPOSES ONLY - Issue: Mar. 99 ETM/XPage: 70-80 - 35

Fig. 39 HMU Schematic


Effectivity:328-300

- FOR TRAINING PURPOSES ONLY - Issue: Mar. 99ETM/XPage: 21 - 33

1.4.1 CAS Field Indications

Honeywell

MAINAHRSREF

DATA

MSG


COPY

2870450 FF LBS / HR

FQ LBS 2870450

50018000 CABIN

XXFTFPM

NU

NDOIL

TEMPOIL

PRSS

20 20

24 CV/S

XX90.5

N2

910 ITT

80.3

N1

115.0

912

108.3 TOGA

NO SYNC

IGN

VIB VIB

IGNSTART START

CAS FIELD MESSAGESThe following messages can be displayed- CAB DIFF PRSS (amber)- CPCS AUTO FAIL (amber)- CPCS MISCOMPARE (amber)- CPCS CTRL MODE MAN (blue)- NO VALID LAND ELEV (blue)

CABIN ALTITUDEIndicates cabin altitude in auto/manualmode.CABIN ALTITUDE RATE OF CHANGEIndicates cabin altitude rate of change in auto/manual mode. increasing rate of change decreasing rate of change

Fig. 15 Messages and Indications on the CAS Field

Dornier 328 - 300Training ManualNavigation

Effectivity:328-300

- FOR TRAINING PURPOSES ONLY - Issue: Oct. 99 ETM/XPage: 34 - 113

Issue: Oct. 99 ETM/XPage: 34 - 138


Fig. 75 Terrain Threat on WX Display

Dornier 328DORNIER LUFTFAHRT TRAINING MANUAL

LINE /BASE MAINTENANCE

TMM-Indicating & Recording

SYSTEM INDICATIONS

PFD Displays

Honeywell

LNAV VALT

20

10

10

20

20

10

10

20

APN

33

30W24

21S

15 3

2200014500

13500

256

260

280

220

240246

7140

200080

0.47M

HDG012

VOR

GPWS

T

200DH 29.924267M52.5NM

TRA

DTK269

0

321

123

TX

VOR1ADF2

Dornier 328TRAINING MANUAL DORNIER LUFTFAHRTLINE /BASE MAINTENANCE


Honeywell

14000

LNAV VALT

20

10

10

20

20

10

10

20

0.47M

HDG012

FMS

GPWS

AP

1850MDA 29.924267M52.5NM

TRA

DTK269

0

321

123

2200014500

13500

256

260

280

220

240246

7

TX

50

140200080

21

50 N

30W24

T

VOR1ADF2

PFD ARC Format with Weather

Dornier 328DORNIER LUFTFAHRT TRAINING MANUAL

LINE /BASE MAINTENANCE


MFD Displays

Honeywell

W30

33

2421

29

HDG012

FMS263

14000

MAIN 1/2DISPLAY RADAR FMS MFD

FORMAT

RNG

WX

T 2.0

52.5NMTRA

ETE 11

TCAS

0.0

TRA FL200 FL250

SAT -13

TAS 288

GS 283

RALIXTOC

DTK269

T

5050

TRARALIXTOC

TGO LBU

KPT

MFD Display

Radio Management Unit - System Pages

COM/NAV Main Page DIRECT Tuning Mode FMS Tuned Radio Mode Display Dimming

RADIO PAGE

123.20 110.40109.35

1471 429.5

TEMP-1

ADF1ATC

1 ON ALT ADF

COM1 NAV1

RANGE: 12MLS1TCAS DSPY 1

RANGE:

127.25119.55

112.40114.00

360.0

TEMP-6 TEMP-1

ADF2ATC

ADF

MLS2TCAS DSPY 2

COM2 NAV2NB

RANGE: 12

BELOW

123.20131.27

110.40109.35

1471 429.5

MEMORY-3 TEMP-1

ADF1ATC

1 ATC ALT ADF

MLS1TCAS DSPY 1

COM1 NAV1NB

TCAS NOTINSTALLED

DME PASS

ADF1ATC

MLS1TCAS DSPY 1

COM1 NAV1NB

VOR PASS

TEST 127.25119.55

112.40114.00

TEMP-6 TEMP-1

ADF2ATC

MLS2TCAS DSPY 2

COM2 NAV2NB

COM TEST

TEST

TUNE TO DIM DISPLAY

ANY KEY TO RETURN

SQ

Pilots Cross-Side Mode Pilots ActivatedSelf-Test Mode

RANGE: 12

BELOW

CH:

GP:AZ:

512000 M3.0

123.20131.27

110.40109.35

1471 429.5

MEMORY-3 TEMP-1

ADF1ATC

1 ATC ALT ADF

MLS1TCAS DSPY 1

COM1 NAV1NB

CH:

GP:AZ:

512000 M3.0

NB

CH:

GP:AZ:

512000 M3.0

30201 ADF ALT

CH:

GP:AZ:

512000 M3.0

AUTO

1471 429.51 ATC ALT ADFATC PASS

TESTADF PASS

TEST

MLS PASS

TESTMMLS

TUNE

Honeywell

SQ DIM 1/2 STO

ID PGE TST DME

TUNE

Honeywell

SQ DIM 1/2 STO

ID PGE TST DME

TUNE

Honeywell

SQ DIM 1/2 STO

ID PGE TST DME

TUNE

Honeywell

SQ DIM 1/2 STO

ID PGE TST DME

TUNE

Honeywell

SQ DIM 1/2 STO

ID PGE TST DME

TUNE

Honeywell

SQ DIM 1/2 STO

ID PGE TST DME

RMU Page Menu COM Memory Page 1 NAV Memory Page 1 COM Memory Page 2 System Test Page Radio Test Result Page

PROGRAM PAGES START-UP SELF TEST PAGES

SYSTEM 1 PAGE MENU 123.20 BRANDWIDTHSELECT

MEMORIES

COM1 NARROW

RADIO PAGE

COM MEMORY

NAV MEMORY

ATC/TCAS

MLS

RETURN

NAVIGATION

ENGINE PG1

ENGINE PG2

MAINTENANCE

NB

1

2

3

MORERETURN

121.70

119.75

123.55

4

5

6

118.00

INSERTDELETE

123.20 FMSENABLEDMEMORIES

1

2

3

MORERETURN

112.50

112.35

108.00

4

5

6

112.50

INSERTDELETE

110.50

115.20

123.20MEMORIES

NAV1

7

8

9

MORERADIOS

113.50

113.35

109.00

10

11

12

111.50

INSERTDELETE

114.50

114.20

123.10135.55

110.80108.50

TEMP-4 TEMP-4

COM NAVNB

PRI BUS

NAV BUS1PRESS TST TO CONTINUE

RMU/SYSTEM TEST RESULTS

123.10135.55

110.80108.50

TEMP-4 TEMP-4

COM NAVNB

NAV1 UNIT

ADF1PRESS TST TO CONTINUE

RADIO TEST RESULTS

DME1NAV1MLS1ATC1

ERRERRERRERRERR

COM1 NBNBBRANDWIDTH

SELECT

NARROW

TUNE

Honeywell

SQ DIM 1/2 STO

ID PGE TST DME

TUNE

Honeywell

SQ DIM 1/2 STO

ID PGE TST DME

TUNE

Honeywell

SQ DIM 1/2 STO

ID PGE TST DME

TUNE

Honeywell

SQ DIM 1/2 STO

ID PGE TST DME

TUNE

Honeywell

SQ DIM 1/2 STO

ID PGE TST DME

TUNE

Honeywell

SQ DIM 1/2 STO

ID PGE TST DME

90 Degree Intercept HDG Information N/A

BACKUP NAVIGATION DISPLAY PAGES

TO360

ADF

VOR300

005

110.40 429.5360

33N

3

CRS

NAV ADF

50,0DME

FROM015

ADF

VOR160

185

112.70 429.5360

33N

3

CRS

NAV ADF

17,5DME

MM360

ADF330

109.90 429.5360

33N

3

CRS

NAV ADF

7,2DME

090

ADF000

110.40 429.5360

33N

3

CRS

NAV ADF

25,2DME

VOR360

MM

ADF

109.90 429.5

33N

3

CRS

NAV ADF

3.1DME

HDGFAIL

Typical FROM Format Typical ILS FormatTypical TO Format

TUNE

Honeywell

SQ DIM 1/2 STO

ID PGE TST DME

TUNE

Honeywell

SQ DIM 1/2 STO

ID PGE TST DME

TUNE

Honeywell

SQ DIM 1/2 STO

ID PGE TST DME

TUNE

Honeywell

SQ DIM 1/2 STO

ID PGE TST DME

TUNE

Honeywell

SQ DIM 1/2 STO

ID PGE TST DME

VOR Information N/A ILS Information N/A ADF Information N/A RSB Information N/A

TO360

ADF300

110.40 429.5360

33N

3

CRS

NAV ADF

MM360

ADF330

109.90 429.5360

33N

3

CRS

NAV ADF

DMEOM360

ADF

109.90 429.5360

33N

3

CRS

NAV ADF

5,2DME

MM360

ADF

109.90 360

33N

3

CRS

NAV ADF

DME

429.5

DME

RMU PROGRAM PAGES

TUNE

Honeywell

SQ DIM 1/2 STO

ID PGE TST DME

TUNE

Honeywell

SQ DIM 1/2 STO

ID PGE TST DME

TUNE

Honeywell

SQ DIM 1/2 STO

ID PGE TST DME

TUNE

Honeywell

SQ DIM 1/2 STO

ID PGE TST DME

CONTROL DISPLAY PAGES

Engine Page No. 1 Engine Page No. 2 RMU SETUP Page ATC/TCAS Control Page MLS Control Page Maintenance Page

BACKUP ENGINE DISPLAY PAGES

85.2 TQ 84.7

99.874598.014505000IGN

99.874097.814400.80IGN

NPITTNHFQ

ALT DPMSG

PAGE 2

CPCS AUTO FAILPITOT S HEAT FAILL AOA FAILR AOA FAILBATT 1 FAILBATT 2 FAIL

600 600FF85 84OIL TEMP61 61OIL PRS

RUDDER LIMITED

RMU SETUP SYSTEM 1 MLS DISPLAY - ENABLED

RETURN TORADIOS

MAINTMENU

TCAS DISPLAY - ENABLED

AUTO BRIGHT- ENABLED

ATC/TCAS CONTROLINTRUDER ALTITUDE:

RETURN TORADIOS

ATC ALTITUDE 1 DATA INVALID

TA DISPLAY: CH: 512

MLS CONTROL - SYSTEM 1

RETURN TORADIOS

AZ: 000BAZ: 000

GP: 3.0

AUTO:MAN MAN

INDENT

AZ BAZ:AZ

MAINTENANCE DATA SYSTEM 1STRAPS

RETURN TORADIOS

SOFTWARE VERSIONS

MAINTENANCE LOG

RMU SETUP

PAGE 1

TUNE

Honeywell

SQ DIM 1/2 STO

ID PGE TST DME

TUNE

Honeywell

SQ DIM 1/2 STO

ID PGE TST DME

TUNE

Honeywell

SQ DIM 1/2 STO

ID PGE TST DME

TUNE

Honeywell

SQ DIM 1/2 STO

ID PGE TST DME

TUNE

Honeywell

SQ DIM 1/2 STO

ID PGE TST DME

TUNE

Honeywell

SQ DIM 1/2 STO

ID PGE TST DME

system schematics.pdf

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