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CABIN CLIMB RATE
ACCORDING TO
CLIMB SCHEDULE
TIME
7850 ft MAX
CABIN ALTITUDE
AIRCRAFT ALTITUDE
MAX 45,000 ft
TAKEOFF
ELEVATION
7850 ft
LANDING
ELEVATION
7850 ft >-
<-
AIR CONDITIONING/PRESSURIZATION
Volume 2 Flight Crew Operating Manual Sep 13/2004
02-04-08 CSP 100-6 REV 1
CONTROLS AND INDICATIONS (Cont)
TAKEOFF AND RETURN TO BASE
TAKEOFF FROM AIRFIELD ABOVE 7850 FT AND LANDING FIELD ELEVATION LESS THAN 7850 FT
During climb and cruise mode, the target for the cabin altitude will be the normal cabin pressure schedule which is below
the maximum normal limit of 7850 ft for aircraft altitudes below 45 000 ft. The warning and caution thresholds will decrease
until the caution threshold reaches 8500 ft and the warning threshold reaches 9400 ft
CFO0204002_006
10 Min TIME
T/O FIELD
ELEVATION
CABIN ON DESCENT
SCHEDULE TOWARD
STORED TAKEOFF
FIELD ELEVATION
THROTTLES
ADVANCED
AIRCRAFT CLIMB
+6000
DESCENT
DETECTED
CABIN DESCENDS TO
T/O FIELD ELEVATION
CABIN CLIMBS ON
CLIMB SCHEDULE
WITHIN 10 Min OF LIFTOFF
AIRCRAFT ALTITUDE 6000 ft
ABOVE T/O FIELD ELEVATION
-
ALTITUDE
<
DESCENT 500 ft/MIN
FOR > 10 SEC
>-
CFO0204002_008
>-
TIME
LANDING
ELEVATION
7000 ft
7850 ft MAX
CABIN ALTITUDE
DESCENT RATE
300 fpm
TAKEOFF
ELEVATION
10 000 ft ALTITUDE
THROTTLES
ADVANCED
AIRCRAFT CLIMB
AIRCRAFT ALTITUDE
45,000 MAX
DESCENT 500 ft MIN
FOR > 10 SEC
AIR CONDITIONING/PRESSURIZATION
Sep 13/2004 Flight Crew Operating Manual Volume 2
REV 1 CSP 100-6 02-04-09
CONTROLS AND INDICATIONS (Cont)
ECS SYNOPTIC PAGE
CFO0305002_010
CAS
CKLST SKIP
FRMT TFC ENTER
ELEC FLT HYD
L R
FUEL
TR/WX SUMRY
COM1 NAV1 ATC1/TCAS ADF1 HF1 COM3 COM2
118.000 108.00 7777 1799.5 118.000 118.000
118.000 108.00 STBY 190.0 2.0000 118.000 118.000
ABV
TX 2.0000 AM
DN
UP
CAB ALT
CAB RATE
APU RPM
APU EGT
FUEL QTY LBS
TOTAL
N2
OIL PRESS
OIL TEMP
FF PPH
I T T
N1 NU
ND
STAB AIL
TRIM
LWD RWD
RUD
FLAPS GEAR
SPOILERS
7300
1000
0
61.0
600
84.7
46
115
7300
300
250
12000
6000 6000
93.0
84.7
46
115
7300
ST
A
RT
ST
A
RT
600
IGN IGN
85.0 MCT
MACH
HOLD
VIB VIB
85.0 MCT
REV
L R
6.6
MSGS
A/ICE
LEFT ENGINE FIRE
PARKING BRAKE
BRAKE OVERHEAT
GEAR DISAGREE
FUEL IMBALANCE
DISPLAY COOL
ECS
MFD CONTROL
RAM AIR
COCKPIT
22°
24°
16°
24°
28°
25°
CABIN
MANUAL
PACK TRIM AIR
XBLEED
APU
PSI PSI
OXY QTY
CAB ALT
CAB RATE
CAB AP
LNDG ALT
1200
6200
1500
9.1
14000
45 60
C
C
C
C
C
C
ECS
AUTO PLAN
SHLDR SIDE
AIR CONDITIONING/PRESSURIZATION
Volume 2 Flight Crew Operating Manual Sep 13/2004
02-04-10 CSP 100-6 REV 1
EICAS MESSAGES
The air conditioning/pressurization system CAS messages and voice aurals are listed below. A brief explanation of each
message is provided.
MESSAGE INHIBITS MEANING
AURAL
WARNING
CABIN ALTITUDE TO/LAND
The normal cabin altitude warning is at 9400 ft
When a takeoff or landing is conducted above
7850 ft, the warning is at the field elevation +
1550 ft, but limited to no higher than 14 300 ft
“Cabin
Altitude”
CABIN DELTA P TO/LAND
The cabin differential pressure is greater than
9.2 psid or less than -0.5 psid
L (R) BLEED LEAK
TO/LAND
A leak has been detected in the bleed air ducting
downstream of the bleed valve
PACK LEAK TO/LAND A leak has been detected in the pack ducting
TRIM AIR LEAK TO/LAND
A leak has been detected in the bleed air ducting
downstream of the right flow control valve, up to
the precooler crossover and up to the trim air
check valve
L (R) PYLON BLEED
LEAK TO/LAND
A leak has been detected in the engine pylon or
tail cone (before shutoff valve)
AIR COND TEMP FAIL TO/LAND
The automatic temperature control system has
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Bombardier AIR CONDITIONING/PRESSURIZATION(13)
