TEMPORARY REVISION RJ/266
Vol. 1
Page 1 of 1
TEMPORARY REVISION RJ/266
Jan 14/11
LETTER OF TRANSMITTAL
REASON FOR ISSUE
Vol. 1
Page 1 of 1
Jan 14/11
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 Revisions to the windshield wiper and side-slip maneuvers limitations,
S Revisions to the windshield wiper and side-slip maneuvers limitations,
S Corrections to the fuel feed check valve test in the After Landing Check, and
S Corrections to the fuel feed check valve test in the After Landing Check, and
S Revisions to the target cabin altitude table in the Manual Pressurization Control procedure.
S Revisions to the target cabin altitude table in the Manual Pressurization Control procedure.
INSTRUCTIONS FOR INSERTION OF THIS TEMPORARY REVISION
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 page of Temporary Revision TR RJ/225 from the
Flight Crew Operating Manual, Vol. 2 and replace it with the appropriate
(yellow-coloured) page from this package:
S 02--06--5 <MASTER>.
2.
Remove and destroy the following page of Temporary Revision TR RJ/225 from the
Flight Crew Operating Manual, Vol. 2 and replace it with the appropriate
(yellow-coloured) page from this package:
S 02--06--5 <MASTER>.
3.
Remove and destroy the following pages of Temporary Revision TR RJ/235 from the
Flight Crew Operating Manual, Vol. 2 and replace them with appropriate
(yellow-coloured) pages from this package:
S 04--12--7 <MASTER> and 04--12--8 <MASTER>.
3.
Remove and destroy the following pages of Temporary Revision TR RJ/235 from the
Flight Crew Operating Manual, Vol. 2 and replace them with appropriate
(yellow-coloured) pages from this package:
S 04--12--7 <MASTER> and 04--12--8 <MASTER>.
4.
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 02--07--1 <MASTER>, and
S 05--05--6 <MASTER>.
4.
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 02--07--1 <MASTER>, and
S 05--05--6 <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
S Volume 2:
S 02--06--5 <MASTER>,
S 02--07--1 <MASTER>,
S 04--12--7 <MASTER> and 04--12--8 <MASTER>, and
S 05--05--6 <MASTER>.
LIST OF PAGES AFFECTED BY THIS TEMPORARY REVISION
S Volume 2:
S 02--06--5 <MASTER>,
S 02--07--1 <MASTER>,
S 04--12--7 <MASTER> and 04--12--8 <MASTER>, and
S 05--05--6 <MASTER>.
Flight Crew Operating
Manual
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Flight Crew Operating
Manual
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LIMITATIONS
Operating Speeds
7.
Vol. 2
LIMITATIONS
Operating Speeds
02--06--5
TR RJ/266, Jan 14/11
TIRE LIMIT SPEED
7.
The tire limit speed is182 knots ground speed.
8.
02--06--5
TR RJ/266, Jan 14/11
TIRE LIMIT SPEED
The tire limit speed is182 knots ground speed.
MAXIMUM AIRSPEED FOR ADG OPERATION
8.
MAXIMUM AIRSPEED FOR ADG OPERATION
For airplanes 7002 thru 7304 -- The maximum airspeeds for continuous operation of the
air-driven generator are as follows:
For airplanes 7002 thru 7304 -- The maximum airspeeds for continuous operation of the
air-driven generator are as follows:
S Following automatic or manual deployment, speeds up to 250 KIAS are permitted for
S Following automatic or manual deployment, speeds up to 250 KIAS are permitted for
S When operationally necessary (e.g. windmill airstarts), speeds up to 330 KIAS are
S When operationally necessary (e.g. windmill airstarts), speeds up to 330 KIAS are
S For flight test or pilot training deployment, the maximum airspeed is 215 KIAS.
S For flight test or pilot training deployment, the maximum airspeed is 215 KIAS.
For airplanes 7305 and subsequent -- There are no airspeed limitations with the ADG
deployed during flight.
For airplanes 7305 and subsequent -- There are no airspeed limitations with the ADG
deployed during flight.
the remainder of the flight.
the remainder of the flight.
permitted for a period of twelve (12) minutes, and speeds between 331 and 335 KIAS
are permitted for a period of four (4) minutes.
9.
Vol. 2
TURBULENCE PENETRATION SPEED
permitted for a period of twelve (12) minutes, and speeds between 331 and 335 KIAS
are permitted for a period of four (4) minutes.
9.
Maximum air speed for turbulence penetration is 280 KIAS or 0.75 Mach, whichever is lower.
10. MINIMUM OPERATING LIMIT SPEED
TURBULENCE PENETRATION SPEED
Maximum air speed for turbulence penetration is 280 KIAS or 0.75 Mach, whichever is lower.
10. MINIMUM OPERATING LIMIT SPEED
Intentional speed reduction below the onset of stall warning, as defined by stick shaker
operation, is prohibited unless a lower speed is specifically authorized for flight test or
training operations.
11. WINDSHIELD WIPER (IF INSTALLED)
Intentional speed reduction below the onset of stall warning, as defined by stick shaker
operation, is prohibited unless a lower speed is specifically authorized for flight test or
training operations.
11. WINDSHIELD WIPER (IF INSTALLED)
The windshield wiper must not be operated above 220 KIAS.
The windshield wiper must not be operated above 220 KIAS.
If the windshield wiper has failed in a non-parked position, the airplane speed must not
exceed 220 KIAS.
If the windshield wiper has failed in a non-parked position, the airplane speed must not
exceed 220 KIAS.
Flight Crew Operating Manual
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Flight Crew Operating Manual
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MASTER
LIMITATIONS
Operating Speeds
Vol. 2
02--06--6
REV 57, Apr 05/04
THIS PAGE INTENTIONALLY LEFT BLANK
Flight Crew Operating Manual
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LIMITATIONS
Operating Speeds
Vol. 2
02--06--6
REV 57, Apr 05/04
THIS PAGE INTENTIONALLY LEFT BLANK
MASTER
Flight Crew Operating Manual
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LIMITATIONS
Maneuvering Loads
1.
Vol. 2
LIMITATIONS
Maneuvering Loads
02--07--1
TR RJ/266, Jan 14/11
MANEUVERING LIMIT LOAD FACTORS
1.
These load factors limit the permissible angles of bank in turns and the severity of pull-up and
push-over maneuvers:
02--07--1
TR RJ/266, Jan 14/11
MANEUVERING LIMIT LOAD FACTORS
These load factors limit the permissible angles of bank in turns and the severity of pull-up and
push-over maneuvers:
Flaps up:
--1.0 G to 2.5 G
Flaps down: 0.0 G to 2.0 G
2.
Vol. 2
Flaps up:
--1.0 G to 2.5 G
Flaps down: 0.0 G to 2.0 G
SIDE-SLIP MANEUVERS
2.
SIDE-SLIP MANEUVERS
Avoid unnecessary and large side-slip maneuvers during low-speed, high-altitude cruise.
Avoid unnecessary and large side-slip maneuvers during low-speed, high-altitude cruise.
Flight Crew Operating Manual
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Flight Crew Operating Manual
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MASTER
LIMITATIONS
Maneuvering Loads
Vol. 2
02--07--2
REV 56, Jan 31/03
THIS PAGE INTENTIONALLY LEFT BLANK
Flight Crew Operating Manual
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LIMITATIONS
Maneuvering Loads
Vol. 2
02--07--2
REV 56, Jan 31/03
THIS PAGE INTENTIONALLY LEFT BLANK
MASTER
Flight Crew Operating Manual
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NORMAL PROCEDURES
After Landing
Vol. 2
04--12--7
TR RJ/266, Jan 14/11
On the first shutdown of the day:
NORMAL PROCEDURES
After Landing
Vol. 2
04--12--7
TR RJ/266, Jan 14/11
On the first shutdown of the day:
(5) Fuel feed check valve test . . . . . . . . . . . Complete ¡
(5) Fuel feed check valve test . . . . . . . . . . . Complete ¡
(a) Engine that was started first . . . . . . Shutdown S L and R FUEL PUMP ON
advisory messages come on
S L and R BOOST PUMP ON
lights come on
(a) Engine that was started first . . . . . . Shutdown S L and R FUEL PUMP ON
advisory messages come on
S L and R BOOST PUMP ON
lights come on
(b) L and R BOOST PUMP
switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off S FUEL LO PRESS caution
message comes on for the
shutdown engine
(b) L and R BOOST PUMP
switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off S FUEL LO PRESS caution
message comes on for the
shutdown engine
S L and R BOOST PUMP
S L and R BOOST PUMP
INOP lights come on
INOP lights come on
If after two (2) minutes and the FUEL LO PRESS caution message is still not
displayed for the shutdown engine:
If after two (2) minutes and the FUEL LO PRESS caution message is still not
displayed for the shutdown engine:
(c) Shutdown
engine . . . . . . . . Dry motor (30 seconds max.) Applicable FUEL LO PRESS
caution message should be
displayed during motoring as
the residual fuel pressure is
reduced
(c) Shutdown
engine . . . . . . . . Dry motor (30 seconds max.) Applicable FUEL LO PRESS
caution message should be
displayed during motoring as
the residual fuel pressure is
reduced
NOTE
NOTE
Absence of the FUEL LO PRESS caution message on
the EICAS is an indication that the fuel feed check valve
has failed in the open position.
Absence of the FUEL LO PRESS caution message on
the EICAS is an indication that the fuel feed check valve
has failed in the open position.
(d) Other engine . . . . . . . . . . . . . . . . . . . Shutdown
(d) Other engine . . . . . . . . . . . . . . . . . . . Shutdown
(6) Thrust levers . . . . . . . . . . . . . . . . . . . . . SHUT OFF
(6) Thrust levers . . . . . . . . . . . . . . . . . . . . . SHUT OFF
(7) ANTI-ICE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
(7) ANTI-ICE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
(a) WING switch . . . . . . . . . . . . . . . . . . . . . . . . OFF
(a) WING switch . . . . . . . . . . . . . . . . . . . . . . . . OFF
(b) LH and RH COWL switches . . . . . . . . . . . OFF
(b) LH and RH COWL switches . . . . . . . . . . . OFF
(8) Fuel pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off S L and R FUEL LO PRESS
caution message on
S L and R BOOST PUMP
INOP lights come on
Flight Crew Operating Manual
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(8) Fuel pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off S L and R FUEL LO PRESS
caution message on
S L and R BOOST PUMP
INOP lights come on
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NORMAL PROCEDURES
After Landing
Vol. 2
(9) HYDRAULIC 3A pump . . . . . . . . . . . . As required If not required, after the parking
brake is selected on, turn off
hydraulic pump 3A
Effectivity: ¡
S Airplanes 7003 thru 7134 not incorporating Canadair Service Bulletin:
S
S
Vol. 2
04--12--8
TR RJ/266, Jan 14/11
(9) HYDRAULIC 3A pump . . . . . . . . . . . . As required If not required, after the parking
brake is selected on, turn off
hydraulic pump 3A
Effectivity: ¡
S Airplanes 7003 thru 7134 not incorporating Canadair Service Bulletin:
SB 601R ---27 ---065, Flight Controls - Aileron - Installation of the Aileron Flutter Damper,
Pivot and Shear Link Assembly.
Airplanes 7003 thru 7067, 7069 thru 7357 not incorporating Canadair Service Bulletin:
S
NORMAL PROCEDURES
After Landing
04--12--8
TR RJ/266, Jan 14/11
S
S
SB 601R ---27 ---100, Flight Controls - Elevator - Flutter Damper Shear Pins Replacement, and
Airplanes 7003 thru 7067, 7069 thru 7357 not incorporating Canadair Service Bulletin:
S
NOTE
The following aileron and elevator checks can be
accomplished either before engine start or after engine
shutdown on the first flight of the day.
SB 601R ---27 ---065, Flight Controls - Aileron - Installation of the Aileron Flutter Damper,
Pivot and Shear Link Assembly.
SB 601R ---27 ---100, Flight Controls - Elevator - Flutter Damper Shear Pins Replacement, and
NOTE
The following aileron and elevator checks can be
accomplished either before engine start or after engine
shutdown on the first flight of the day.
(a) Pump 3A switch . . . . . . . . . . . . . . . . . . . . . . ON
(a) Pump 3A switch . . . . . . . . . . . . . . . . . . . . . . ON
(b) Pump 1 and 2 switches . . . . . . . . . . . . . . OFF Deplete #1 and #2 hydraulic
system pressure, confirm <400
psi.
Check aileron and elevator
travel range (to approx ½
travel), in both directions.
(b) Pump 1 and 2 switches . . . . . . . . . . . . . . OFF Deplete #1 and #2 hydraulic
system pressure, confirm <400
psi.
Check aileron and elevator
travel range (to approx ½
travel), in both directions.
(c) Pump 1 switch . . . . . . . . . . . . . . . . . . . . . . . ON
(c) Pump 1 switch . . . . . . . . . . . . . . . . . . . . . . . ON
(d) Pump 3A switch . . . . . . . . . . . . . . . . . . . . . OFF Deplete #3 hydraulic system
pressure; confirm <400 psi.
Check elevator travel range (to
approx ½ travel), in both
directions.
(d) Pump 3A switch . . . . . . . . . . . . . . . . . . . . . OFF Deplete #3 hydraulic system
pressure; confirm <400 psi.
Check elevator travel range (to
approx ½ travel), in both
directions.
(e) Pump 2 switch . . . . . . . . . . . . . . . . . . . . . . . ON
(e) Pump 2 switch . . . . . . . . . . . . . . . . . . . . . . . ON
(f)
(f)
Pump 1 switch . . . . . . . . . . . . . . . . . . . . . AUTO Deplete #1 hydraulic system
pressure; confirm <400 psi.
Check elevator travel range (to
approx ½ travel), in both
directions.
Pump 1 switch . . . . . . . . . . . . . . . . . . . . . AUTO Deplete #1 hydraulic system
pressure; confirm <400 psi.
Check elevator travel range (to
approx ½ travel), in both
directions.
(g) Pump 2 switch . . . . . . . . . . . . . . . . . . . . . AUTO
(g) Pump 2 switch . . . . . . . . . . . . . . . . . . . . . AUTO
(h) Pump 3A switch . . . . . . . . . . . . . . . As required
(h) Pump 3A switch . . . . . . . . . . . . . . . As required
Flight Crew Operating Manual
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Flight Crew Operating Manual
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ABNORMAL PROCEDURES
Air--Conditioning, Bleed and
Pressurization
C.
ABNORMAL PROCEDURES
Air--Conditioning, Bleed and
Pressurization
05--05--5
Vol. 2
REV 58, Oct 31/05
Unpressurized Flight Procedure (PACKs ON)
C.
(1)
Airplane altitude . . . . . . . . . . . . . 10,000 feet MSL
maximum or lowest safe altitude.
(2)
EMER DEPRESS switch . . . . . . . . . . . . . . . . . ON S EMER DEPR ON light on
(1)
Airplane altitude . . . . . . . . . . . . . 10,000 feet MSL
maximum or lowest safe altitude.
(2)
EMER DEPRESS switch . . . . . . . . . . . . . . . . . ON S EMER DEPR ON light on
S EMER DEPRESS caution
message on
Unpressurized Flight Procedure (PACKs OFF)
message on
D.
Unpressurized Flight Procedure (PACKs OFF)
(1)
Airplane altitude . . . . . . . . . . . . . 10,000 feet MSL
maximum or lowest safe altitude.
(1)
Airplane altitude . . . . . . . . . . . . . 10,000 feet MSL
maximum or lowest safe altitude.
(2)
Airspeed . . . . . . . . . . . . . Not less than 250 KIAS
(2)
Airspeed . . . . . . . . . . . . . Not less than 250 KIAS
NOTE
250 KIAS airspeed recommended during cruise to
provide sufficient airflow to passengers within cabin.
(3)
NOTE
250 KIAS airspeed recommended during cruise to
provide sufficient airflow to passengers within cabin.
L and R PACK switches . . . . . . . . . . . . . . . . . OFF S L and R PACK OFF light on
(3)
L and R PACK switches . . . . . . . . . . . . . . . . . OFF S L and R PACK OFF light on
S L and R PACK OFF status
S L and R PACK OFF status
message on
message on
(4)
AIR-CONDITIONING CARGO
switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
(4)
AIR-CONDITIONING CARGO
switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
(5)
DSPLY FAN switch . . . . . . . . . . . . . . . . . . . STDBY
(5)
DSPLY FAN switch . . . . . . . . . . . . . . . . . . . STDBY
(6)
RAM-AIR switch . . . . . . . . . . . . . . . . . . . . . . OPEN S RAM AIR OPEN status
message on
(6)
RAM-AIR switch . . . . . . . . . . . . . . . . . . . . . . OPEN S RAM AIR OPEN status
message on
(7)
EMER DEPRESS switch . . . . . . . . . . . . . . . . . ON S EMER DEPRESS light on
(7)
EMER DEPRESS switch . . . . . . . . . . . . . . . . . ON S EMER DEPRESS light on
S EMER DEPRESS status
S EMER DEPRESS status
message on
E.
REV 58, Oct 31/05
Unpressurized Flight Procedure (PACKs ON)
S EMER DEPRESS caution
D.
05--05--5
Vol. 2
Manual Pressurization Control Procedure
message on
E.
Manual Pressurization Control Procedure
(1)
MAN ALT switch . . . . . . . . . . Mid position / centre
(1)
MAN ALT switch . . . . . . . . . . Mid position / centre
(2)
PRESS CONT switch . . . . . . . . . . . . . . . . . . MAN S MAN light on
S CABIN PRESS MAN status
message on
(2)
PRESS CONT switch . . . . . . . . . . . . . . . . . . MAN S MAN light on
S CABIN PRESS MAN status
message on
To increase cabin altitude:
To increase cabin altitude:
(3)
MAN ALT switch . . . . . . . . . . . . . . . . . . . . . . . . . UP
(3)
MAN ALT switch . . . . . . . . . . . . . . . . . . . . . . . . . UP
(4)
MAN RATE switch . . . . . . . . . . . . . . . . As required
(4)
MAN RATE switch . . . . . . . . . . . . . . . . As required
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ABNORMAL PROCEDURES
Air--Conditioning, Bleed and
Pressurization
Vol. 2
To decrease cabin altitude:
(3)
(4)
MAN ALT switch . . . . . . . . . . . . . . . . . . . . . . . . . DN
MAN RATE switch . . . . . . . . . . . . . . . . As required
(3)
(4)
180
200
220
240
260
Target
Cabin Altitude
1700
2000
2400
2800
3200
Cruise
Flight Level
310
330
350
370
390
Target
Cabin Altitude
4600
MAN ALT switch . . . . . . . . . . . . . . . . . . . . . . . . . DN
MAN RATE switch . . . . . . . . . . . . . . . . As required
5300
6000
6700
7400
(5)
MAN ALT
switch . . . . . . . . . . . . Set to mid position / center when reaching target cabin
altitude (see table below)
290
Cruise
Flight Level
180
200
220
240
260
280
290
3700
4100
Target
Cabin Altitude
1700
2000
2400
2800
3200
3700
4100
410
---
Cruise
Flight Level
310
330
350
370
390
410
---
---
Target
Cabin Altitude
4600
5300
6000
6700
7400
8000
---
280
8000
Descent: <0090>
Descent: <0090>
At the top of descent:
At the top of descent:
(1)
Cabin altitude . . . . . . . . . . . . . Adjust to 8000 feet
(1)
At 21,000 feet airplane altitude:
(1)
Cabin altitude . . . . . . . . . . . . . Adjust to 8000 feet
At 21,000 feet airplane altitude:
Cabin altitude . . . . . . . . . . . . Adjust to LDG ELEV
(1)
NOTE
When in manual pressurization control mode:
S The CABIN ALT cation message will be posted when
the cabin altitude is between 8500 feet and 10000
feet.
S The CABIN ALT warning message will be posted
when the cabin altitude is greater than 10000 feet.
Cabin altitude . . . . . . . . . . . . Adjust to LDG ELEV
NOTE
When in manual pressurization control mode:
S The CABIN ALT cation message will be posted when
the cabin altitude is between 8500 feet and 10000
feet.
S The CABIN ALT warning message will be posted
when the cabin altitude is greater than 10000 feet.
Before landing:
(1)
05--05--6
TR RJ/266, Jan 14/11
To maintain cabin altitude:
MAN ALT
switch . . . . . . . . . . . . Set to mid position / center when reaching target cabin
altitude (see table below)
Cruise
Flight Level
Vol. 2
To decrease cabin altitude:
To maintain cabin altitude:
(5)
ABNORMAL PROCEDURES
Air--Conditioning, Bleed and
Pressurization
05--05--6
TR RJ/266, Jan 14/11
Before landing:
Cabin altitude . . . . . . . . . . . . Adjust to LDG ELEV.
(1)
NOTE
Do not set cabin altitude below landing field
elevation.
Cabin altitude . . . . . . . . . . . . Adjust to LDG ELEV.
NOTE
Do not set cabin altitude below landing field
elevation.
If differential pressure is not zero upon landing:
If differential pressure is not zero upon landing:
(2)
MAN ALT switch . . . . . . . . . . . . . . . . . . . . . . . . . UP
(2)
MAN ALT switch . . . . . . . . . . . . . . . . . . . . . . . . . UP
(3)
MAN RATE switch . . . . . . . . . . . . Maximum INCR
(3)
MAN RATE switch . . . . . . . . . . . . Maximum INCR
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