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

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### Airplane Flight Manual CSP A-012 DOT ApprovedTEMPORARY 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 MSTTEMPORARY 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 MSTTEMPORARY 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 MSTTEMPORARY 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 MSTTEMPORARY 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 MSTTEMPORARY 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 MSTTEMPORARY 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 MSTTEMPORARY 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 N 1 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 MSTTEMPORARY 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 MSTTEMPORARY 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 ApprovedTEMPORARY 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