TEMPORARY REVISION RJ/236
Vol. 1
Page 1 of 1
TEMPORARY REVISION RJ/236
Oct 08/09
LETTER OF TRANSMITTAL
REASON FOR ISSUE
Vol. 1
Page 1 of 1
Oct 08/09
LETTER OF TRANSMITTAL
REASON FOR ISSUE
Temporary revision to advise the flight crew of the following:
Temporary revision to advise the flight crew of the following:
S Addition of the EMER PWR ONLY condition to the Loss of All AC Power emergency
S Addition of the EMER PWR ONLY condition to the Loss of All AC Power emergency
S Editorial changes to harmonize Flight Controls abnormal procedures across all programs,
S Editorial changes to harmonize Flight Controls abnormal procedures across all programs,
S Editorial changes to the Air-Conditioning and Pressurization Supplement.
S Editorial changes to the Air-Conditioning and Pressurization Supplement.
procedure,
and
INSTRUCTIONS FOR INSERTION OF THIS TEMPORARY REVISION
procedure,
and
INSTRUCTIONS FOR INSERTION OF THIS TEMPORARY REVISION
1.
Insert the Record of Temporary Revisions in the front portion of the Flight Crew
Operating Manual, Vol. 1.
1.
Insert the Record of Temporary Revisions in the front portion of the Flight Crew
Operating Manual, Vol. 1.
2.
Remove and destroy the following pages from the Flight Crew Operating Manual, Vol. 2
and replace them with appropriate (yellow-coloured) pages from this package:
S 03--11--9 <MASTER> and 03--11--10 <MASTER>, and
2.
Remove and destroy the following pages from the Flight Crew Operating Manual, Vol. 2
and replace them with appropriate (yellow-coloured) pages from this package:
S 03--11--9 <MASTER> and 03--11--10 <MASTER>, and
S 07--02--3 <MASTER> and 07--02--4 <MASTER>.
S 07--02--3 <MASTER> and 07--02--4 <MASTER>.
3.
Remove and destroy the following pages of Temporary Revision TR RJ/218 from the
Flight Crew Operating Manual, Vol. 2 and replace them with appropriate
(yellow-coloured) pages from this package:
S 03--04--11 <MASTER> and 03--04--12 <MASTER>.
3.
Remove and destroy the following pages of Temporary Revision TR RJ/218 from the
Flight Crew Operating Manual, Vol. 2 and replace them with appropriate
(yellow-coloured) pages from this package:
S 03--04--11 <MASTER> and 03--04--12 <MASTER>.
4.
Remove and destroy the following pages of Temporary Revision TR RJ/233 from the
Flight Crew Operating Manual, Vol. 2 and replace them with appropriate
(yellow-coloured) pages from this package:
S 05--11--19 <MASTER> and 05--11--20 <MASTER>.
4.
Remove and destroy the following pages of Temporary Revision TR RJ/233 from the
Flight Crew Operating Manual, Vol. 2 and replace them with appropriate
(yellow-coloured) pages from this package:
S 05--11--19 <MASTER> and 05--11--20 <MASTER>.
5.
Record the insertion of this Temporary Revision on the Record of Temporary Revisions
page.
5.
Record the insertion of this Temporary Revision on the Record of Temporary Revisions
page.
6.
Retain this page for record purposes.
6.
Retain this page for record purposes.
LIST OF PAGES AFFECTED BY THIS TEMPORARY REVISION
LIST OF PAGES AFFECTED BY THIS TEMPORARY REVISION
S Volume 2:
S 03--04--11 <MASTER> and 03--04--12 <MASTER>,
S 03--11--9 <MASTER> and 03--11--10 <MASTER>,
S 05--11--19 <MASTER> and 05--11--20 <MASTER>,
S Volume 2:
S 03--04--11 <MASTER> and 03--04--12 <MASTER>,
S 03--11--9 <MASTER> and 03--11--10 <MASTER>,
S 05--11--19 <MASTER> and 05--11--20 <MASTER>,
S 07--02--3 <MASTER> and 07--02--4 <MASTER>.
S 07--02--3 <MASTER> and 07--02--4 <MASTER>.
Flight Crew Operating
Manual
CSP A -- 013
Flight Crew Operating
Manual
CSP A -- 013
EMERGENCY PROCEDURES
Smoke/Fire/Fumes
Vol. 2
EMERGENCY PROCEDURES
Smoke/Fire/Fumes
03--04--11
TR RJ/236, Oct 08/09
D.
SMOKE CARGO
D.
SMOKE CARGO
D.
SMOKE CARGO<0056> <0057>
D.
SMOKE CARGO<0056> <0057>
Indication: SMOKE CARGO warning message on, NORMAL and STANDBY CARGO
SMOKE PUSH switches on and “SMOKE” aural on.
Indication: SMOKE CARGO warning message on, and “SMOKE” aural on.<0056> <0057>
Vol. 2
03--04--11
TR RJ/236, Oct 08/09
Indication: SMOKE CARGO warning message on, NORMAL and STANDBY CARGO
SMOKE PUSH switches on and “SMOKE” aural on.
Indication: SMOKE CARGO warning message on, and “SMOKE” aural on.<0056> <0057>
Bombardier Business Aircraft Division Airplanes <0056> <0057>:
Bombardier Business Aircraft Division Airplanes <0056> <0057>:
(1) Designated crew member
<0056> <0057> . . . . . . . . . . . . . . . . . . . . . . . . . Advise to isolate and extinguish source
of smoke or fire, and to secure
the area.
(1) Designated crew member
<0056> <0057> . . . . . . . . . . . . . . . . . . . . . . . . . Advise to isolate and extinguish source
of smoke or fire, and to secure
the area.
(1) CARGO FIREX, NORMAL
and STANDBY CARGO SMOKE
PUSH switches . . . . . . . . . . . . . . . . . . . . . . . Select to arm both squibs.
S BOTTLE ARMED -- PUSH
TO DISCH lights on.
(1) CARGO FIREX, NORMAL
and STANDBY CARGO SMOKE
PUSH switches . . . . . . . . . . . . . . . . . . . . . . . Select to arm both squibs.
S BOTTLE ARMED -- PUSH
TO DISCH lights on.
(2) CARGO FIREX, NORMAL
and STANDBY BOTTLE ARMED
PUSH TO DISCH switches . . . . . . . . . . . . . Select to discharge both squibs on firex
bottle.
S BOTTLE ARMED -- PUSH
TO DISCH lights out and
CARGO BTL LO caution
message on (may take up to
20 minutes as bottle
gradually discharges).
(2) CARGO FIREX, NORMAL
and STANDBY BOTTLE ARMED
PUSH TO DISCH switches . . . . . . . . . . . . . Select to discharge both squibs on firex
bottle.
S BOTTLE ARMED -- PUSH
TO DISCH lights out and
CARGO BTL LO caution
message on (may take up to
20 minutes as bottle
gradually discharges).
(3) Squib/bottle discharge . . . . . . . . . . . . . . . . Confirm
(3) Squib/bottle discharge . . . . . . . . . . . . . . . . Confirm
(4) Landing elevation . . . . . . . . . . . . Set to 8,000 feet or landing field elevation,
whichever is higher.
(4) Landing elevation . . . . . . . . . . . . Set to 8,000 feet or landing field elevation,
whichever is higher.
(5) Descent . . . . . . . . . . . . Initiate to 10,000 feet MSL or minimum enroute altitude,
whichever is higher.
(5) Descent . . . . . . . . . . . . Initiate to 10,000 feet MSL or minimum enroute altitude,
whichever is higher.
At 10,000 feet or lowest safe altitude, whichever is higher:
At 10,000 feet or lowest safe altitude, whichever is higher:
(6) LDG ELEV . . . . . . . Set to landing field elevation, if not already done.
(6) LDG ELEV . . . . . . . Set to landing field elevation, if not already done.
If source of smoke/fumes/fire not visually confirmed to be extinguished or
fire uncontrollable<0056> <0057>:
If source of smoke/fumes/fire not visually confirmed to be extinguished or
fire uncontrollable<0056> <0057>:
(7) Land immediately at the nearest suitable airport.
(7) Land immediately at the nearest suitable airport.
Flight Crew Operating Manual
CSP A--013
MASTER
Flight Crew Operating Manual
CSP A--013
MASTER
EMERGENCY PROCEDURES
Smoke/Fire/Fumes
Vol. 2
03--04--12
TR RJ/236, Oct 08/09
EMERGENCY PROCEDURES
Smoke/Fire/Fumes
Vol. 2
CAUTION
CAUTION
Expedite the landing. Dependant upon the severity of
the situation, the crew should consider an overweight
landing, tailwind landing, ditching or a forced off-airport
landing.
Expedite the landing. Dependant upon the severity of
the situation, the crew should consider an overweight
landing, tailwind landing, ditching or a forced off-airport
landing.
Flight Crew Operating Manual
CSP A-- 013
MASTER
Flight Crew Operating Manual
CSP A-- 013
03--04--12
TR RJ/236, Oct 08/09
MASTER
EMERGENCY PROCEDURES
Electrical
B.
Vol. 2
Loss of All AC Power
Indication:
(1)
EMERGENCY PROCEDURES
Electrical
03--11--9
TR RJ/236, Oct 08/09
B.
Only BATT BUS and DC ESS BUS powered.
PFD 1, MFD 1 , EICAS primary and status displays are powered.
ADG manual deploy handle . . . . . . . . . . . . . Pull
Indication:
Only BATT BUS and DC ESS BUS powered.
PFD 1, MFD 1 , EICAS primary and status displays are powered.
ADG manual deploy handle . . . . . . . . . . . . . Pull
If on emergency power:
If on emergency power:
(2)
(2)
If battery power only persists:
(2)
03--11--9
TR RJ/236, Oct 08/09
Loss of All AC Power
(1)
EMR PWR ONLY procedure . . . . . . Accomplish Refer to EMERGENCY
PROCEDURES -ELECTRICAL -- EMER PWR
ONLY.
Vol. 2
EMR PWR ONLY procedure . . . . . . Accomplish Refer to EMERGENCY
PROCEDURES -ELECTRICAL -- EMER PWR
ONLY.
If battery power only persists:
Engine instruments . . . . . . . . . Verify N1, N2, ITT
(2)
Engine instruments . . . . . . . . . Verify N1, N2, ITT
If engine instruments indicate that engines are not operating:
If engine instruments indicate that engines are not operating:
(3)
(3)
Double Engine Failure
procedure . . . . . . . . . . . . . . . . . . . . . . Accomplish Refer to EMERGENCY
PROCEDURES -POWERPLANT -- Double
Engine Failure.
Double Engine Failure
procedure . . . . . . . . . . . . . . . . . . . . . . Accomplish Refer to EMERGENCY
PROCEDURES -POWERPLANT -- Double
Engine Failure.
If engine instruments indicate that engines are operating:
(3)
Cabin altitude . . . . . . . . . . . . . . . . . . . . . . Monitor
(4)
Descent . . . . . . . . . . . . . . . . . . . . . . . . As required
If engine instruments indicate that engines are operating:
(3)
Cabin altitude . . . . . . . . . . . . . . . . . . . . . . Monitor
(4)
Descent . . . . . . . . . . . . . . . . . . . . . . . . As required
Airplanes 7002 thru 7304:
(5)
Airspeed . . . . . . . . . . . Not more than 250 KIAS
Airplanes 7002 thru 7304:
(5)
Airspeed . . . . . . . . . . . Not more than 250 KIAS
Airplanes 7305 and subsequent:
Airplanes 7305 and subsequent:
(5)
No airspeed limitation with the ADG deployed.
(5)
No airspeed limitation with the ADG deployed.
(6)
GEN 1 and GEN 2
switches . . . . . . . . . . . . . OFF / RESET then ON S GEN 1 (2) OFF caution
messages out.
(6)
GEN 1 and GEN 2
switches . . . . . . . . . . . . . OFF / RESET then ON S GEN 1 (2) OFF caution
messages out.
(7)
APU (if available, 30,000 feet
and below) . . . . . . . . . . . . . . . . . . . . . . . . . . . Start Refer to LIMITATIONS -POWERPLANT -- AUXILIARY
POWER UNIT.
(7)
APU (if available, 30,000 feet
and below) . . . . . . . . . . . . . . . . . . . . . . . . . . . Start Refer to LIMITATIONS -POWERPLANT -- AUXILIARY
POWER UNIT.
(8)
APU GEN switch (if APU available) . . . . . . . ON S APU GEN OFF caution
message out.
(8)
APU GEN switch (if APU available) . . . . . . . ON S APU GEN OFF caution
message out.
If any generator comes on-line, re-establish normal power:
(9)
ADG manual deploy
handle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Stow if ADG deployed manually
Flight Crew Operating Manual
CSP A-- 013
MASTER
If any generator comes on-line, re-establish normal power:
(9)
ADG manual deploy
handle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Stow if ADG deployed manually
Flight Crew Operating Manual
CSP A-- 013
MASTER
EMERGENCY PROCEDURES
Electrical
(10)
Vol. 2
EMERGENCY PROCEDURES
Electrical
03--11--10
TR RJ/236, Oct 08/09
Vol. 2
03--11--10
TR RJ/236, Oct 08/09
(10)
(11)
ADG PWR TXFR,
OVERRIDE switch . . . . . . . . . . . . . . . . . . . Select S AC ESS BUS now powered
by an operating generator.
CAS messages . . . . . . . . . . . . . . . . . . . . . Review
(11)
ADG PWR TXFR,
OVERRIDE switch . . . . . . . . . . . . . . . . . . . Select S AC ESS BUS now powered
by an operating generator.
CAS messages . . . . . . . . . . . . . . . . . . . . . Review
(12)
Affected systems . . . . . . . . . . . . . . . . . . . Restore
(12)
Affected systems . . . . . . . . . . . . . . . . . . . Restore
Effectivity:
Effectivity:
S Airplanes 7003 thru 7207 not incorporating Canadair Service Bulletin:
S Airplanes 7003 thru 7207 not incorporating Canadair Service Bulletin:
S SB 601R--34--094, Installation of a New ADC (--140) and ARP (--104).
(13)
Flight instruments . . . . . . . . . . . . Check / Reset
barometric altimeter setting,
altitude preselector, V-speeds
and speed bug setting
after generator switching.
S SB 601R--34--094, Installation of a New ADC (--140) and ARP (--104).
(13)
If unable to reset at least one generator, continue flight on battery power only:
Flight instruments . . . . . . . . . . . . Check / Reset
barometric altimeter setting,
altitude preselector, V-speeds
and speed bug setting
after generator switching.
If unable to reset at least one generator, continue flight on battery power only:
NOTE
NOTE
Electrical power may be lost after 30 minutes.
Electrical power may be lost after 30 minutes.
(9)
Descent . . . . . . . . . . . . . . . . . . . . . . . . . . Continue to 10,000 feet MSL or lowest
safe altitude.
(9)
Descent . . . . . . . . . . . . . . . . . . . . . . . . . . Continue to 10,000 feet MSL or lowest
safe altitude.
(10)
ANTI-ICE, WING switch . . . . . STBY if required S N2 gauges change color to
indicate wing anti-ice on.
(addition of amber range,
from 0--77% N2).
(10)
ANTI-ICE, WING switch . . . . . STBY if required S N2 gauges change color to
indicate wing anti-ice on.
(addition of amber range,
from 0--77% N2).
S WING A/I ON advisory
S WING A/I ON advisory
message on. <0039>
(11)
(12)
Leave icing conditions.
message on. <0039>
(11)
Leave icing conditions.
NOTE
NOTE
Icing conditions exist in--flight at a TAT of 10 _C (50 _F)
or below, and visible moisture in any form is
encountered (such as clouds, rain, snow, sleet or ice
crystals), except when the SAT is --40 _C (--40 _F) or
below.
Icing conditions exist in--flight at a TAT of 10 _C (50 _F)
or below, and visible moisture in any form is
encountered (such as clouds, rain, snow, sleet or ice
crystals), except when the SAT is --40 _C (--40 _F) or
below.
Land at the nearest suitable airport.
(12)
Land at the nearest suitable airport.
At 10,000 feet MSL or lowest safe altitude:
At 10,000 feet MSL or lowest safe altitude:
(13)
(13)
RAM AIR switch . . . . . . . . . . . . . . . . . . . . OPEN to open ram air valve and
provide airflow to passengers.
S RAM AIR OPEN status
message on.
Flight Crew Operating Manual
CSP A-- 013
MASTER
RAM AIR switch . . . . . . . . . . . . . . . . . . . . OPEN to open ram air valve and
provide airflow to passengers.
S RAM AIR OPEN status
message on.
Flight Crew Operating Manual
CSP A-- 013
MASTER
ABNORMAL PROCEDURES
Flight Controls
(5)
Vol. 2
ABNORMAL PROCEDURES
Flight Controls
05--11--19
TR RJ/236, Oct 08/09
Maximum landing weight <0090> . . . . . Determine using the table below and
correct for wind:
(5)
Vol. 2
Maximum landing weight <0090> . . . . . Determine using the table below and
correct for wind:
NOTE <0090>
NOTE <0090>
The actual landing weight must not exceed the
corrected maximum landing weight due to tire speed.
The actual landing weight must not exceed the
corrected maximum landing weight due to tire speed.
Flight Crew Operating Manual
CSP A-- 013
MASTER
05--11--19
TR RJ/236, Oct 08/09
Flight Crew Operating Manual
CSP A-- 013
MASTER
ABNORMAL PROCEDURES
Flight Controls
J.
ABNORMAL PROCEDURES
Flight Controls
05--11--20
TR RJ/236, Oct 08/09
SPOILERONS ROLL
J.
Indication: SPOILERONS ROLL caution message on.
On the side with the operative roll control:
On the side with the operative roll control:
PLT ROLL or
CPLT ROLL switch . . . . Select to operative side S PLT ROLL CMD or
CPLT ROLL CMD advisory
messages on.
L (R) SPOILERON
(1)
K.
Vol. 2
05--11--20
TR RJ/236, Oct 08/09
SPOILERONS ROLL
Indication: SPOILERONS ROLL caution message on.
(1)
K.
Vol. 2
PLT ROLL or
CPLT ROLL switch . . . . Select to operative side S PLT ROLL CMD or
CPLT ROLL CMD advisory
messages on.
L (R) SPOILERON
Indication: L or R SPOILERON caution message on.
Indication: L or R SPOILERON caution message on.
Prior to landing:
Prior to landing:
(1)
GPWS/FLAP OVRD switch . . . . . . . . . . . . OVRD to mute flap aural warning.
(1)
(1)
GRND PROX FLAP switch <0040> . . . . . . OVRD to mute flap aural warning.
(1)
GPWS/FLAP OVRD switch . . . . . . . . . . . . OVRD to mute flap aural warning.
GRND PROX FLAP switch <0040> . . . . . . OVRD to mute flap aural warning.
(2)
Landing flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20
(2)
Landing flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20
(3)
Approach speed . . . . . . . . . . . . . . . Not less than
VREF (Flaps 45°)+12 KIAS
(3)
Approach speed . . . . . . . . . . . . . . . Not less than
VREF (Flaps 45°)+12 KIAS
(4)
Actual landing distance . . . . . . . . . . . . . Increase
(4)
Actual landing distance . . . . . . . . . . . . . Increase
WITHOUT THRUST REVERSERS
WITH THRUST REVERSERS
WITHOUT THRUST REVERSERS
WITH THRUST REVERSERS
1.30 (30%)
1.25 (25%)
1.30 (30%)
1.25 (25%)
NOTE
Select the runway available with minimum crosswind.
Flight Crew Operating Manual
CSP A-- 013
NOTE
Select the runway available with minimum crosswind.
MASTER
Flight Crew Operating Manual
CSP A--013
MASTER
SUPPLEMENTARY PROCEDURES
Air-- Conditioning and Pressurization
D.
SUPPLEMENTARY PROCEDURES
Air--Conditioning and Pressurization
07--02--3
Vol. 2
TR RJ/236, Oct 08/09
Air-conditioning From Engine Bleeds During Take-off
D.
If the engine bleed is desired to provide air-conditioning during take-off, transfer
bleeds as follows:
TR RJ/236, Oct 08/09
Air-conditioning From Engine Bleeds During Take-off
If the engine bleed is desired to provide air-conditioning during take-off, transfer
bleeds as follows:
(1)
10TH STAGE, R BLEED AIR valves . . . . . . . . . . . . . . . . . . . . . . . . . . . Open
PLT
(1)
10TH STAGE, R BLEED AIR valves . . . . . . . . . . . . . . . . . . . . . . . . . . . Open
PLT
(2)
10TH STAGE ISOL valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Closed
PLT
(2)
10TH STAGE ISOL valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Closed
PLT
(3)
10TH STAGE, L BLEED AIR valves . . . . . . . . . . . . . . . . . . . . . . . . . . . Open
PLT
(3)
10TH STAGE, L BLEED AIR valves . . . . . . . . . . . . . . . . . . . . . . . . . . . Open
PLT
(4)
APU LCV . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check closed
PLT
(4)
APU LCV . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check closed
PLT
S Press out LCV switch/light to match APU LCV position, i.e. closed.
E.
07--02--3
Vol. 2
Unpressurized Take-off and Landing Procedure
S Press out LCV switch/light to match APU LCV position, i.e. closed.
E.
Unpressurized Take-off and Landing Procedure
The procedures outlined below are recommended when performing a no-engine bleed
(for whatever reason) take-off and landing, with the APU inoperative or selected OFF
for performance reasons.
The procedures outlined below are recommended when performing a no-engine bleed
(for whatever reason) take-off and landing, with the APU inoperative or selected OFF
for performance reasons.
Before Take-off
Before Take-off
When the engine bleeds cannot be used for take-off (due to hot ambient temperature short runway combination, etc.) and the APU is inoperative, the following procedures
are recommended:
When the engine bleeds cannot be used for take-off (due to hot ambient temperature short runway combination, etc.) and the APU is inoperative, the following procedures
are recommended:
(1)
PRESS CONT switch . . . . . . . . . . . . . . . . . . . Auto S Pressed out. MAN light goes
out.
(1)
PRESS CONT switch . . . . . . . . . . . . . . . . . . . Auto S Pressed out. MAN light goes
out.
(2)
EMER DEPRESS switch . . . . . . . . . . . . . . . . . ON S Pressed in. EMER
DEPRESS light on.
(2)
EMER DEPRESS switch . . . . . . . . . . . . . . . . . ON S Pressed in. EMER
DEPRESS light on.
S EMER DEPRESS status
S EMER DEPRESS status
message on.
message on.
(3)
L and R PACKs . . . . . . . . . . . . . . . . . . . . . . . . OFF S Pressed out. OFF lights
come on.
(3)
L and R PACKs . . . . . . . . . . . . . . . . . . . . . . . . OFF S Pressed out. OFF lights
come on.
(4)
10TH STAGE, ISOL valve . . . . . . . . . . . . Closed S OPEN light goes off.
(4)
10TH STAGE, ISOL valve . . . . . . . . . . . . Closed S OPEN light goes off.
(5)
10TH STAGE,
L and R BLEED AIR . . . . . . . . . . . . . . . CLOSED S L and R CLOSED lights
come on.
(5)
10TH STAGE,
L and R BLEED AIR . . . . . . . . . . . . . . . CLOSED S L and R CLOSED lights
come on.
(6)
RAM-AIR switch . . . . . . . . . . . . . . . . . . . . . OPEN S Pressed in. OPEN light
comes on.
(6)
RAM-AIR switch . . . . . . . . . . . . . . . . . . . . . OPEN S Pressed in. OPEN light
comes on.
Flight Crew Operating Manual
CSP A--013
MASTER
Flight Crew Operating Manual
CSP A--013
MASTER
SUPPLEMENTARY PROCEDURES
Air-- Conditioning and Pressurization
Vol. 2
SUPPLEMENTARY PROCEDURES
Air-- Conditioning and Pressurization
07--02--4
TR RJ/236, Oct 08/09
Vol. 2
07--02--4
TR RJ/236, Oct 08/09
After Take-off
After Take-off
At a safe altitude, preferably between 1,500 and 3,000 feet above field elevation:
At a safe altitude, preferably between 1,500 and 3,000 feet above field elevation:
(7)
(7)
RAM-AIR switch . . . . . . . . . . . . . . . . . . . . . . Close S Pressed out. OPEN light
goes off.
(8) 10TH STAGE,
L and R BLEED AIR valves . . . . . . . . . . . . . Open S L and R CLOSED lights go
off.
(9) L and R PACKs . . . . . . . . . . . . . . . . . . . . . . . . . On S Pressed in. OFF lights go
off.
(10) EMER DEPRESS switch . . . . . . . . . . . . . . . . . Off S Pressed out. EMER
DEPRESS light goes off.
RAM-AIR switch . . . . . . . . . . . . . . . . . . . . . . Close S Pressed out. OPEN light
goes off.
(8) 10TH STAGE,
L and R BLEED AIR valves . . . . . . . . . . . . . Open S L and R CLOSED lights go
off.
(9) L and R PACKs . . . . . . . . . . . . . . . . . . . . . . . . . On S Pressed in. OFF lights go
off.
(10) EMER DEPRESS switch . . . . . . . . . . . . . . . . . Off S Pressed out. EMER
DEPRESS light goes off.
S EMER DEPRESS status
S EMER DEPRESS status
message goes out.
message goes out.
NOTE
If an engine failure occurs, delay turning on the
bleeds until after obstacle clearance is assured.
NOTE
If an engine failure occurs, delay turning on the
bleeds until after obstacle clearance is assured.
Landing
Landing
The procedures outlined below are recommended if engine bleeds are not to be used
during landing, with the APU inoperative or selected OFF for performance reasons.
The procedures outlined below are recommended if engine bleeds are not to be used
during landing, with the APU inoperative or selected OFF for performance reasons.
When below 10,000 feet AGL:
When below 10,000 feet AGL:
(1)
PRESS CONT switch . . . . . . . . . . . . . . . . . . . Auto S Pressed out. MAN light goes
out.
At the turn to final approach:
(1)
(2)
(2)
(3)
(4)
(5)
L and R PACKs . . . . . . . . . . . . . . . . . . . . . . . . OFF S Pressed out. OFF lights
come on.
10TH STAGE,
L and R BLEED AIR valves . . . . . . . . . CLOSED S L and R CLOSED lights
come on.
S L and R 10TH SOV CLSD
status messages come on.
RAM-AIR switch . . . . . . . . . . . . . . . . . . . . . OPEN S Pressed in. OPEN light
comes on.
LDG ELEV . . . . . . . . . . . . . . . . . Set to 3,000 feet
above landing field elevation
PRESS CONT switch . . . . . . . . . . . . . . . . . . . Auto S Pressed out. MAN light goes
out.
At the turn to final approach:
(3)
(4)
(5)
L and R PACKs . . . . . . . . . . . . . . . . . . . . . . . . OFF S Pressed out. OFF lights
come on.
10TH STAGE,
L and R BLEED AIR valves . . . . . . . . . CLOSED S L and R CLOSED lights
come on.
S L and R 10TH SOV CLSD
status messages come on.
RAM-AIR switch . . . . . . . . . . . . . . . . . . . . . OPEN S Pressed in. OPEN light
comes on.
LDG ELEV . . . . . . . . . . . . . . . . . Set to 3,000 feet
above landing field elevation
NOTE
1. Avoid high rates of descent for passenger comfort.
NOTE
1. Avoid high rates of descent for passenger comfort.
2. After landing, ensure that the airplane is
completely depressurized prior to opening any
airplane doors.
2. After landing, ensure that the airplane is
completely depressurized prior to opening any
airplane doors.
Flight Crew Operating Manual
CSP A-- 013
MASTER
Flight Crew Operating Manual
CSP A-- 013
MASTER