TEMPORARY REVISION RJ/186--2

Jul 07/11

LETTER OF TRANSMITTAL

REASON FOR ISSUE

Temporary revision to advise the flight crew of the following:

S Incorporation of Service Bulletin, SB 601R-29-031 --- Hydraulic Power --- Hydraulic

System 3 --- Deactivation and Removal of the Accumulator Assembly, to ensure that the

hydraulic 3B pump is selected ON instead of AUTO for all phases of flight,

S Incorporation of Service Bulletin, SB 601R-29-034 -- Hydraulic Power -- Hydraulic

System No. 3 -- Installation in a New Location of the New Accumulator and the Nitrogen

Pressure Gauge of Hydraulic System No. 3,

S Incorporate Temporary Revision TR RJ/170--2,

S Revisions to the HYD 3 HI TEMP abnormal procedure, and

S Remove the requirement to check the operation of the gravity crossflow system

whenever operations are beyond 30 minutes of an alternate airport.

INSTRUCTIONS FOR INSERTION OF THIS TEMPORARY REVISION

(1) Insert the Record of Temporary Revisions in the front portion of the Airplane

Flight Manual.

(2) Remove and destroy the pages and the Letter of Transmittal of Temporary

Revision No. TR RJ/186 ---1.

(3) Insert the pages of this Temporary Revision in the Airplane Flight Manual as

instructed at the top of each page.

(4) Record the insertion of this Temporary Revision on the Record of Temporary

Revisions page.

(5) Retain this page for record purposes.

LIST OF PAGES AFFECTED BY THIS TEMPORARY REVISION

S 02 ---00 ---4 <MST>,

S 02 ---08 ---8 <MST>,

S 04 ---02 ---4 <MST>,

S 04 ---02 ---5 <MST>,

S 04 ---02 ---6 <MST>,

S 04 ---02 ---11 <MST>,

S 04 ---02 ---12 <MST>,

S 05 ---09 ---3, and

S 05 ---13 ---8.

Page 1 of 12

Airplane Flight Manual

CSP A-012 DOT Approved
TEMPORARY REVISION RJ/186--2

Jul 07/11

INSERT IN LIMITATIONS -- TABLE OF CONTENTS

FACING PAGE 02--00--4 <MST>

ACTION

Replace the list under “SYSTEMS LIMITATIONS (CONT’D)” to read as follows:

SYSTEMS LIMITATIONS (CONT’D)

Enhanced Ground Proximity Warning System (EGPWS) 02 ---08 ---7

General <0040> 02 ---08 ---7

Systems Limitations <0040> 02 ---08 ---7

Terrain Avoidance Maneuvering <0040> 02 ---08 ---7

QFE Operations <0040 without 0027, 0047> 02 ---08 ---7

GPS Inoperative <0040 & 0047> / Both GPS Inoperative <0027 & 0040> 02 ---08 ---7

Flight Deck Door <FAA, 0093> 02 ---08 ---8

Flight Deck Door <JCAB, 0093> 02 ---08 ---8

Integrated Standby Instrument (ISI) 02 ---08 ---8

Hydraulic 3B Pump 02 ---08 ---8

Page 2 of 12

Airplane Flight Manual

CSP A-012 DOT Approved MST
TEMPORARY REVISION RJ/186--2

Jul 07/11

INSERT IN LIMITATIONS -- SYSTEMS LIMITATIONS

FACING PAGE 02--08--8 <MST>

ACTION

Add the following:

Effectivity:

S Airplanes incorporating Bombardier Aerospace Service Bulletin SB 601R-29-031,

Hydraulic Power --- Hydraulic System No. 3 --- Deactivation and Removal of the Accumulator

Assembly, and

S Airplanes not incorporating Bombardier Aerospace Service Bulletin SB 601R-29-034,

Hydraulic Power --- Hydraulic System No. 3 --- Installation in a New Location of the New

Accumulator and the Nitrogen Pressure Gauge of Hydraulic System No. 3.

18. HYDRAULIC 3B PUMP

S The Hydraulic 3B pump switch must be selected ON instead of AUTO for all phases of

flight.

Page 3 of 12

Airplane Flight Manual

CSP A-012 DOT Approved MST
TEMPORARY REVISION RJ/186--2

Jul 07/11

INSERT IN NORMAL PROCEDURES -- CONSOLIDATED PROCEDURES

FACING PAGE 04--02--4 <MST>

ACTION

Change paragraph “F. Cleared to Start Check” to read as follows:

F. Cleared to Start Check

(1) Personal Electronic Devices ............... Off

(2) APU / AC electrics ............... On / Checked

(3) Papers ............................. On board

(4) Take-off data ............................ Set

(5) Doors ........................ Closed / Locked

Page 4 of 12

Airplane Flight Manual

CSP A-012 DOT Approved MST
TEMPORARY REVISION RJ/186--2

Jul 07/11

INSERT IN NORMAL PROCEDURES -- CONSOLIDATED PROCEDURES

FACING PAGE 04--02--5 <MST>

ACTION 1

Replace the steps under “F. Cleared to Start Check (Cont’d)” to read as follows:

F. Cleared to Start Check (Cont’d)

(6) BEACON <0021> ......................... ON

Effectivity:

S Airplanes 7003 thru 8104 incorporating SB 601R--34--146 -- Navigation -- Transponder

System -- Wire Strapping Changes for Operation of Transponder when the Aircraft is on

the Ground, or:

S Airplanes 8105 and subsequent.

NOTE

At airports where transponder operation on ground

is required, the flight crew should select the assigned

Mode A (squawk) and activate the transponder when

required by ATC.

(7) Transponder ..................... As required

(8) Fuel pumps and quantity On, (quantity) ........

Effectivity:

S Airplanes incorporating Bombardier Aerospace Service Bulletin SB 601R-29-031,

Hydraulic Power -- Hydraulic System No. 3 -- Deactivation and Removal of the Accumulator

Assembly.

(9) HYDRAULIC pumps .............. AUTO / ON Hydraulic pumps 1 and 2 are

selected to AUTO and hydraulic

pumps 3A and 3B are selected

to ON.

Effectivity:

S Airplanes incorporating Bombardier Aerospace Service Bulletin SB 601R-29-034,

Hydraulic Power -- Hydraulic System No. 3 -- Installation in a New Location of the New

Accumulator and the Nitrogen Pressure Gauge of Hydraulic System No. 3

(9) HYDRAULIC pumps .............. AUTO / ON Hydraulic pumps 1, 3B and 2 are

selected to AUTO and hydraulic

pump 3A is selected to ON.

Page 5 of 12

Airplane Flight Manual

CSP A-012 DOT Approved MST
TEMPORARY REVISION RJ/186--2

Jul 07/11

INSERT IN NORMAL PROCEDURES -- CONSOLIDATED PROCEDURES

FACING PAGE 04--02--5 <MST> (CONT’D)

F. Cleared to Start Check (Cont’d)

(10) PARKING BRAKE As required ................

NOTE

Release parking brake and turn off nosewheel

steering if push-back is required. Audio or visual

communications with the ground crew must be

maintained at all times during push-back.

(11) IGNITION A or B ....................... ARM

(12) Engines ............................... Start

(13) Fuel Feed Check Valve test ......... Complete First flight of the day <TC><FAA> .

(13) Fuel Feed Check Valve test .......... Complete First flight of the day <JAA>.

Refer to SUPPLEMENTS ---

FUEL FEED CHECK VALVE

TEST.

ACTION 2

Change the steps in paragraph “A. After Start Check” to read as follows:

A. After Start Check

NOTE

1. A high vortex noise may occur during stationary

engine run-up to high power in high crosswind or

tailwind conditions. This phenomenon is not harmful

to the engines and may be ignored.

2. Do not accelerate engine until oil pressure has

stabilized below 116 psi.

(1) GEN 1 and GEN 2 ....................... ON

(2) Bleeds / PACKs ..................... Set / ON

(3) IGNITION ............................... Off

(4) APU ............................. As required

(5) ANTI-ICE ............... Checked / As required Check --- First flight of the day.

Page 6 of 12

Airplane Flight Manual

CSP A-012 DOT Approved MST
TEMPORARY REVISION RJ/186--2

Jul 07/11

INSERT IN NORMAL PROCEDURES -- CONSOLIDATED PROCEDURES

FACING PAGE 04--02--6 <MST>

ACTION 1

Change the steps in paragraph “A. After Start Check (Cont’d)” to read as follows:

A. After Start Check (Cont’d)

(6) PROBES ................................ ON

(7) APR ........................... Tested / ARM Test --- First flight of the day.

(8) Electrics ............................ Checked

(9) Rudder ............................ Checked

(10) N/W STRG ......................... ARMED

Effectivity:

S Airplanes 7003 thru 8104 incorporating SB 601R--34--146 -- Navigation -- Transponder

System -- Wire Strapping Changes for Operation of Transponder when the Aircraft is on

the Ground, or

S Airplanes 8105 and subsequent.

(11) Transponder ..................... As required

NOTE

At airports where runway structural repair or debris is

known to exist, use thrust reversers with extreme

caution to preclude the possibility of foreign object

damage (FOD) from occurring.

ACTION 2

Delete the NOTE immediately after paragraph “B. Taxi Check”

Page 7 of 12

Airplane Flight Manual

CSP A-012 DOT Approved MST
TEMPORARY REVISION RJ/186--2

Jul 07/11

INSERT IN NORMAL PROCEDURES -- CONSOLIDATED PROCEDURES

FACING PAGE 04--02--11 <MST>

ACTION

Change paragraph “A. After Landing Check” to read as follows:

A. After Landing Check

(1) APU ............................ As required

Effectivity:

S Airplanes 7003 thru 8104 incorporating SB 601R--34--146 -- Navigation --

Transponder System -- Wire Strapping Changes for Operation of Transponder

when the Aircraft is on the Ground, or:

S Airplanes 8105 and subsequent.

NOTE

At airports where required, after landing, the flight

crew must maintain the transponder on continuously

until the airplane is fully parked on stand. The

transponder shall be switched to STBY after parking.

(2) Transponder ..................... As required

Effectivity:

S Airplanes 7003 thru 8104 not incorporating SB 601R--34--146 -- Navigation --

Transponder System -- Wire Strapping Changes for Operation of Transponder

when the Aircraft is on the Ground.

(2) Transponder .......................... STBY

(3) Radar .................................. OFF

(4) Flaps ................................... Up

(5) Lights and strobes ................ As required

(6) PROBES ............................... OFF

(7) Bleeds .................................. Set

Page 8 of 12

Airplane Flight Manual

CSP A-012 DOT Approved MST
TEMPORARY REVISION RJ/186--2

Jul 07/11

INSERT IN NORMAL PROCEDURES -- CONSOLIDATED PROCEDURES

FACING PAGE 04--02--12 <MST>

ACTION

Replace paragraph “B. Shutdown Check” to read as follows:

B. Shutdown Check

NOTE

An engine must not be shut down until after the

following have been confirmed:

1. The thrust reverse lever is at the stowed position,

2. The REV icon at N1 gauge goes out, and

3. The REV UNLOCKED caution message is not

displayed.

CAUTION

Inform ground crew of ‘Hot’ brakes condition as

soon as possible.

(1) Chocks and Brakes ................ As required

Effectivity:

S Airplanes 7003 thru 8104 incorporating SB 601R--34--146 -- Navigation --

Transponder System -- Wire Strapping Changes for Operation of Transponder

when the Aircraft is on the Ground, or:

S Airplanes 8105 and subsequent.

(2) Transponder ........................... STBY

CAUTION

If the aircraft is to be moved again under its own

power or otherwise, before all the passengers have

deplaned, then the SEAT BELTS signs must be

turned back on and all the passengers confirmed

seated with their seat belts fastened before any

further aircraft movement.

(3) SEAT BLTS ............................ OFF

Page 9 of 12

Airplane Flight Manual

CSP A-012 DOT Approved MST
TEMPORARY REVISION RJ/186--2

Jul 07/11

INSERT IN NORMAL PROCEDURES -- CONSOLIDATED PROCEDURES

FACING PAGE 04--02--12 <MST> (CONT’D)

(4) Electrics / GEN 1 and GEN 2 Set / OFF ........

(5) Fuel Feed Check Valve test Complete .......... First flight of the day <TC><FAA> .

(5) Fuel Feed Check Valve test ......... Complete First flight of the day <JAA>.

Refer to SUPPLEMENTS ---

FUEL FEED CHECK VALVE

TEST.

(6) Thrust Levers SHUT OFF .....................

(7) ANTI-ICE OFF ...............................

(8) Fuel pumps Off ..............................

(9) HYDRAULIC 3A and 3B pumps As required .....

(10) BEACON <0021> ........................ OFF

(11) N/W STRG switch OFF .......................

Page 10 of 12

Airplane Flight Manual

CSP A-012 DOT Approved MST
TEMPORARY REVISION RJ/186--2

Jul 07/11

INSERT IN ABNORMAL PROCEDURES -- ELECTRICAL

FACING PAGE 05--09--3

ACTION

Change paragraph “K. ADG Inadvertent Deployment” to read as follows:

K. ADG Inadvertent Deployment

Airplanes 7002 to 7304:

(1) Airspeed Not more than 250 KIAS .........................................

Airplanes 7305 and subsequent:

(1) No airspeed limitation with the ADG deployed.

To re-establish normal operations:

(2) ADG manual release handle Stow ..........................................

(3) ADG PWR TXFR OVERRIDE switch Select ...................................

Effectivity:

S Airplanes incorporating Bombardier Aerospace Service Bulletin SB 601R-29-031,

Hydraulic Power -- Hydraulic System No. 3 -- Deactivation and Removal of the

Accumulator Assembly.

(4) HYDRAULIC 3B pump switch .......................................... ON

Effectivity:

S Airplanes incorporating Bombardier Aerospace Service Bulletin SB 601R-29-034,

Hydraulic Power -- Hydraulic System No. 3 -- Installation in a New Location of the New

Accumulator and the Nitrogen Pressure Gauge of Hydraulic System No. 3.

(4) HYDRAULIC 3B pump switch ................................... As required

Page 11 of 12

Airplane Flight Manual

CSP A-012 DOT Approved
TEMPORARY REVISION RJ/186--2

Jul 07/11

INSERT IN ABNORMAL PROCEDURES -- HYDRAULIC POWER

FACING PAGE 05--13--8

ACTION

Change paragraph “F. HYD 3 HI TEMP” to read as follows:

F. HYD 3 HI TEMP

NOTE

If the HYDRAULIC 3A and 3B pumps were running at

the time the HYD 3 HI TEMP caution message

appeared, attempt to isolate the malfunctioning

pump by switching each pump to OFF, in turn.

(1) HYDRAULIC 3B pump switch .......................................... ON

(2) HYDRAULIC 3A pump switch ......................................... OFF

(3) System 3 temperature ............................................. Monitor

If temperature can be controlled:

(4) Affected HYDRAULIC pump switch .............................. Leave OFF

If temperature cannot be controlled:

(4) HYDRAULIC 3A and 3B pump switches ................................ OFF

(5) System 3 temperature ............................................. Monitor

NOTE

No action is required for the HYD 3 LO PRESS

caution message, continue HYD 3 HI TEMP

procedure until landing.

If temperature is less than 107°C:

Prior to landing:

(6) HYDRAULIC 3A and 3B pump switches ................................. ON

If temperature is 107°C or higher:

(6) Land at the nearest suitable airport.

Prior to landing:

(7) HYDRAULIC 3A and 3B pump switches ................................. ON

Page 12 of 12

Airplane Flight Manual

CSP A-012 DOT Approved