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5.0
RUDDER
AIL
LWD RWD
NL NR
FF (PPH)
OIL PRESS
OIL TEMP
FAN VIB
0 4050
8100
0.0
33
0
0
0
- FUEL (LBS) - TOTAL
0
0
33
0.0
4050
DN DN DN
- GEAR - - FLAPS - 20
R ENG OIL PRESS
L ENG OIL PRESS
L WSHLD HEAT
L WINDOW HEAT
INBD BRAKE PRESS
R WSHLD HEAT
R WINDOW HEAT
OUTBD BRAKE PRESS
R PROBE HEAT OFF
L PROBE HEAT OFF
HYD 3 LO PRESS
BRT
CABIN TEMP
BLEED PRESS
FUEL TEMP
ENGINE
BULK
OXY
C ALT
RATE
P
47
23
0
36 35
1820
100
0
0.0
APU
100 323
RPM EGT
R FUEL PUMP ON
L FUEL PUMP ON
DOOR CLOSED
PARKING BRAKE ON
PROX SYS FAULT
FDR FAIL
SPOILERS
15
2 000
2
3
4
ALT
0
7 3
2
1
4
9
6 2992
5
1014
400
350
300 250
200
150
100
60
KTS
IAS
FEET
X 1000
CABIN
ALTITUDE
0
4
2
6
8
10
20
30
45
BRT
BRT
80
60
20
00
20
10
10
20
300
200
100
100
000
8000
4
RA2
IRS2
ADC2
DCP2
TERM
VOR1
TRU
NO FLIGHT PLAN
TCAS
OFF
29.92 IN
2400M
GS
RA
TO
LOC 1
DR TO
ALTS
FMS1
12
DTK 333
.7
YUL
NM
4
4
2
2
1
1
2500M
200
N
33
15
12
E
6
3
0
3000
40
VT 150
V2 133
VR 121
V1 113
ADF2
0FT
2
1
CYUL
TOC
ALEXS
3
059
N
E
12
25
WX+TRB
UTC 11:01 TAS 0 GS 0 SAT 15 C TAT 15 C
VOR 1 FMS MAP ADF 2
CYUL
LONNA
ALEXS
CYUL
1NM
12NM
20NM
111NM
0:03
0:04
0:23
11:02
11:05
11:07
11:25 7137LB 35.6GM
12.5
DME 1
YUL
12.7
DME 2
– – – –
LONNA
VFE (45 FLAPS)
VFE (30 FLAPS)
VFE (20 FLAPS)
VA (MANEUVERING)
(AT SEA LEVEL 48,200LB)
(AT 20,000FT 26,000LB)
VNO (BELOW 8,000FT)
VNO (8,000 TO 22,150 FT)
AIRSPEED LIMITS - (INDICATED SPEEDS)
MMO (22,150FT TO 26,570FT)
VMO (26,570FT TO 30,990FT)
MMO (30,990FT TO 41,000FT)
VLO (EXT) (L/G EXTENSION)
VLO (RET) (L/G RETRACTION)
VLE (L/G EXTENDED)
189
197
231
248
187
300
348
0.78
318
0.85
197
197
250
80
60
20
00
20
10
10
20
300
200
100
100
000
8000
4
RA2
IRS2
ADC2
DCP2
VOR1
TRU
TCAS
OFF
29.92 IN
2400M
GS
RA
TO
LOC 1
DR TO
ALTS
4
4
2
2
1
1
2500M
200
0
3000
40
VT 150
V2 133
VR 121
V1 113
ADF2
0FT
2
1
FMS2
12
DTK 056
.2
LONNA
NM
TERM
N
33
15
12
E
6
3
PFD EICAS
NORM
L MFD
EICAS PFD
NORM
R MFD
ED
1
ED
NORM
EICAS
D EIC
2
AS PF
Display Reversionary
Selector must be selected
to display EICAS on MFD
AURAL/VISUAL WARNING
3-20 For Training Purposes Only
May 03
P I LOT T R A I N I N G GU I D E
Maintenance Diagnostic Computer
Description
The maintenance diagnostic computer (MDC) is an onboard computer that is used to
record aircraft mechanical and avionics system data. Maintenance personnel can
retrieve the information for use in engine trend analysis, significant event recording
and for avionics/aircraft system failure detection.
Operation
The MDC continuously records data for fault analysis and engine trend monitoring.
The MDC data is downloadable to a maintenance facility computer.
MDC data is available on the flight deck by means of a red guarded switch on circuit
breaker panel number one (CBP 1). Data can be displayed on MFD 1 or MFD 2, as
determined by switch selection. Instructions on MDC data presentation are displayed
on the selected MFD.
　
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