Download - System Schematics.pdf
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Dornier 328 - 300
Training Manual
Indicating/Recording
Effectivity:328-300
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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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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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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
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Effectivity:328-300
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
96 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
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)
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Dornier 328 - 300
Training Manual
Electrical Power
Effectivity:328-300
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Issue: Mar. 99 ETM
/XPage: 24 - 71
Honeywell
SYSTEM 2/3APUICE
PROTECTECSELECTR NEXT
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
NONESS1 1 2 NONESS2ESSENTIAL
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)
-
Dornier 328 - 300Training ManualElectrical Power
Issue: Mar. 99 ETM/XPage: 24 - 72
- FOR TRAINING PURPOSES ONLY - Effectivity:328-300
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
-
Dornier 328 - 300Training ManualElectrical Power
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
PROTECTECSELECTR NEXT
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
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Dornier 328 - 300
Training Manual
Electrical Power
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/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
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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
- FOR TRAINING PURPOSES ONLY - Issue: Mar. 99 ETM/XPage: 36 - 33
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
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Issue
: Mar.
99 ETM
/XP
age: 36
- 35
REC FAN FAIL
REC FAN FAIL
FAIL
HX FAN FAILPACK OVHT
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
(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
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
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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
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
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-
Effectivity:328-300
4 SYSTEM
IND
ICATIONS
FAIL
HX FAN FAILPACK OVHT
COCKPIT ENGINEATS
CABIN24 C
ECONOMY
BAGGAGE 23 C
PSI 45
LH PACK X-BLEED RH PACK
BLEEDHP
LHLPHP
RHAPU
SYSTEM 2/3ICE
PROTECTECSELECTR NEXTAPU
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
HX FAN FAILPACK OVHT
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
-
Dornier 328 - 300Training ManualCPCS
Issue: Mar. 99 ETM/XPage: 21 - 34
- FOR TRAINING PURPOSES ONLY - Effectivity:328-300
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
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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
Issue: Mar. 99 ETM/XPage: 30 - 56
- FOR TRAINING PURPOSES ONLY - Effectivity:328-300
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
APUOVERSPEEDOVERTEMP EGTOVERCURRENT ECUOIL PRESS LOWOIL TEMP HIGH
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
- FOR TRAINING PURPOSES ONLY - Issue: Mar. 99 ETM/XPage: 28 - 51
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
Issue: Mar. 99 ETM/XPage: 27 - 128
- FOR TRAINING PURPOSES ONLY - Effectivity:328-300
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
-
Dornier 328 - 300Training Manual Flight Controls
Issue: Mar. 99 ETM/XPage: 27 - 132
- FOR TRAINING PURPOSES ONLY - Effectivity:328-300
8.2 SYSTEM 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 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
-
Dornier 328 - 300Training Manual Flight Controls
Issue: Mar. 99 ETM/XPage: 27 - 36
- FOR TRAINING PURPOSES ONLY - Effectivity:328-300
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
- FOR TRAINING PURPOSES ONLY - Issue: Mar. 99 ETM/XPage: 27 - 133
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
-
Dornier 328 - 300Training Manual Flight Controls
Issue: Mar. 99 ETM/XPage: 27 - 134
- FOR TRAINING PURPOSES ONLY - Effectivity:328-300
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
APUOVERSPEEDOVERTEMP EGTOVERCURRENT ECUOIL PRESS LOWOIL TEMP HIGH
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
-
Dornier 328 - 300Training Manual Flight Controls
Issue: Mar. 99 ETM/XPage: 27 - 136
- FOR TRAINING PURPOSES ONLY - Effectivity:328-300
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
Issue: Mar. 99 ETM/XPage: 32 - 32
- FOR TRAINING PURPOSES ONLY - Effectivity:328-300
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
De-ice BleedShut off Valve
De-ice BleedShut off Valve
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
HX FAN FAILPACK OVHT
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
(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
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
Issue: Mar. 99 ETM/XPage: 49 - 68
- FOR TRAINING PURPOSES ONLY - Effectivity:328-300
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
PROTECTECSELECTR NEXT
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
-
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 - 300Training ManualNavigation
Effectivity:328-300
- FOR TRAINING PURPOSES ONLY - Issue: Oct. 99 ETM/XPage: 34 - 113
-
Issue: Oct. 99 ETM/XPage: 34 - 138
- FOR TRAINING PURPOSES ONLY - Effectivity:328-300
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
TMM-Indicating & Recording
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
TMM-Indicating & Recording
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