F

Model CL−600−2D24

(Series 900) Model CL−600−2D15

(Series 705) <2705>

AIRPLANE FLIGHT MANUAL

Volume 1

CSP C−012

MASTER

Information copy only. This material is not customized to a specific

airplane configuration. The user must ascertain that this material is

applicable for the intended use.

BOMBARDIER INC.

BOMBARDIER AEROSPACE COMMERCIAL AIRCRAFT

CUSTOMER SUPPORT

123 GARRATT BLVD., TORONTO, ONTARIO

CANADA M3K 1Y5

Copyright © 2002 − 2015 by Bombardier Inc.

All rights reserved. No part of this work may be reproduced or copied in any form or by any means without written permission of Bombardier Inc.

The Bombardier logo is a registered trademark of Bombardier Inc.

Initial Issue:

Revision 11A:

Sep 09/2002

B

May 25/2015
"The information, technical data and the designs disclosed herein are the

exclusive property of Bombardier Inc. or contain proprietary rights of others and

are not to be used or disclosed to others without the written consent of

Bombardier Inc. The recipient of this document, by its retention and use, agrees

to hold in confidence the technical data and designs contained herein. The

foregoing shall not apply to persons having proprietary rights to such information,

technical data or such designs to the extent that such rights exist."
This is revision 11A to the MASTER Airplane Flight Manual , CSP C−012.

To bring this manual up to date, remove old pages and insert revised pages as follows:

REMOVE: INSERT:

Chapter

Section

Subject Page

Chapter

Section

Subject Page

Title Page / Disclaimer All Title Page / Disclaimer All

00−02 00−02−55 to 00−02−58 00−02 00−02−55 to 00−02−60

00−04 00−04−1 to 00−04−14

Limitations 02−00−4 to 02−00−5 Limitations 02−00−4 to 02−00−5

02−08−8 02−08−8

Normal Procedures 04−02−10 Normal Procedures 04−02−10

04−02−13 04−02−13

Abnormal Procedures 05−00−7 to 05−00−8 Abnormal Procedures 05−00−7 to 05−00−8

05−15−12 05−15−12 to 05−15−14

F TRANSMITTAL LETTER

Transmit−1

Rev. 11A, May 25/2015

DOT Approved Airplane Flight Manual

CSP C−012

 NOTE

Re. pages 04-02-10 and 04-02-13. These pages were reissued with revision bars due to changes in the publishing software 

attributes, however the text remains unchanged.
F TRANSMITTAL LETTER

Transmit−2

Rev. 11A, May 25/2015

DOT Approved Airplane Flight Manual

CSP C−012

THIS PAGE INTENTIONALLY LEFT BLANK
Title Page /

Disclaimer

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LIST OF EFFECTIVE PAGES

00−04−7

Rev. 11A, May 25/2015

DOT Approved Airplane Flight Manual

CSP C−012

Page Date Page Date Page Date

* The asterisk indicates pages changed, added or deleted.

PAGE PRINTED ON 10-9-2015
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LIST OF EFFECTIVE PAGES

00−04−8

Rev. 11A, May 25/2015

DOT Approved Airplane Flight Manual

CSP C−012

Page Date Page Date Page Date

* The asterisk indicates pages changed, added or deleted.

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LIST OF EFFECTIVE PAGES

00−04−9

Rev. 11A, May 25/2015

DOT Approved Airplane Flight Manual

CSP C−012

Page Date Page Date Page Date

* The asterisk indicates pages changed, added or deleted.

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LIST OF EFFECTIVE PAGES

00−04−10

Rev. 11A, May 25/2015

DOT Approved Airplane Flight Manual

CSP C−012

Page Date Page Date Page Date

* The asterisk indicates pages changed, added or deleted.

PAGE PRINTED ON 10-9-2015
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LIST OF EFFECTIVE PAGES

00−04−11

Rev. 11A, May 25/2015

DOT Approved Airplane Flight Manual

CSP C−012

Page Date Page Date Page Date

* The asterisk indicates pages changed, added or deleted.

PAGE PRINTED ON 10-9-2015
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LIST OF EFFECTIVE PAGES

00−04−12

Rev. 11A, May 25/2015

DOT Approved Airplane Flight Manual

CSP C−012

Page Date Page Date Page Date

* The asterisk indicates pages changed, added or deleted.

PAGE PRINTED ON 10-9-2015
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LIST OF EFFECTIVE PAGES

00−04−13

Rev. 11A, May 25/2015

DOT Approved Airplane Flight Manual

CSP C−012

Page Date Page Date Page Date

* The asterisk indicates pages changed, added or deleted.

PAGE PRINTED ON 10-9-2015
LIST OF EFFECTIVE PAGES

00−04−14

Rev. 11A, May 25/2015

DOT Approved Airplane Flight Manual

CSP C−012

THIS PAGE INTENTIONALLY LEFT BLANK

PAGE PRINTED ON 10-9-2015
INTRODUCTION

INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 01 1

LANDING DISTANCE FACTORS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 01 1

REJECTED TAKE OFF

REJECTED TAKE-OFF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 02 1

Rejected Take-off Before Achieving V1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 02 1

POWER PLANT

POWER PLANT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 03 1

L ENG FIRE or R ENG FIRE or Severe Engine Damage (In Flight) . . . . . . . . . . . . . 03 03 1

L ENG FIRE or R ENG FIRE or Severe Engine Damage (On Ground) . . . . . . . . . . . 03 03 1

Double Engine Failure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 03 2

L REV DEPLOYED or R REV DEPLOYED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 03 5

L ENG OIL PRESS or R ENG OIL PRESS or Low Engine Oil Pressure

Indication . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 03 6

Uncommanded Acceleration / ENGINE OVERSPD . . . . . . . . . . . . . . . . . . . . . . . . . 03 03 6

SMOKE/FIRE/FUMES

SMOKE/FIRE/FUMES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 04 1

General Notes, Cautions and Warnings . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 04 1

Smoke/Fire/Fumes Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 04 1

Smoke or Fumes Removal Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 04 9

SMOKE AFT LAV or SMOKE FWD LAV . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 04 9

SMOKE AFT CARGO or SMOKE FWD CARGO . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 04 10

AIR CONDITIONING AND PRESSURIZATION

AIR-CONDITIONING AND PRESSURIZATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 05 1

CABIN ALT (Warning Message) or Emergency Descent Procedure . . . . . . . . . . . . . 03 05 1

DIFF PRESS <TC> or <FAA> or <JAA> . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 05 2

DIFF PRESS <AR>. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 05 3

AUTOMATIC FLIGHT CONTROL SYSTEM

AUTOMATIC FLIGHT CONTROL SYSTEM (AFCS) . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 06 1

AFCS MSG FAIL or Autopilot Failure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 06 1

Uncommanded Yaw Motion . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 06 1

EMERGENCY PROCEDURES

Table of Contents

03 00 1

Rev. 8, Sep 27/2013

CHAPTER 3 - EMERGENCY PROCEDURES

DOT Approved Airplane Flight Manual

CSP C 012

PAGE PRINTED ON 10-9-2015
AUXILIARY POWER UNIT

AUXILIARY POWER UNIT (APU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 07 1

APU FIRE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 07 1

APU OVERSPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 07 1

APU OVERTEMP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 07 1

BLEED AIR LEAKS

BLEED AIR LEAKS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 08 1

L BLEED DUCT or R BLEED DUCT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 08 1

DITCHING AND FORCED LANDING

DITCHING AND FORCED LANDING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 1

Recommended Configuration . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 1

DITCHING OR FORCED LANDING IMMINENT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 1

Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 1

PLANNED DITCHING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 2

General Notes, Cautions and Warnings . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 2

Preliminary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 2

Approach . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 3

Prior to Water Contact . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 4

After Water Contact . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 4

FORCED LANDING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 5

General Notes, Cautions and Warnings . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 5

Preliminary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 5

Approach . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 6

Prior to Contact . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 6

After Contact . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 7

EVACUATION

EVACUATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 10 1

Passenger Evacuation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 10 1

ELECTRICAL

ELECTRICAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 11 1

EMER PWR ONLY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 11 1

Loss of all AC Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 11 3

EMERGENCY PROCEDURES

Table of Contents

03 00 2

Rev. 8, Sep 27/2013

DOT Approved Airplane Flight Manual

CSP C 012

PAGE PRINTED ON 10-9-2015
FLIGHT CONTROLS

FLIGHT CONTROLS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 12 1

Aileron System Jammed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 12 1

Elevator System Jammed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 12 2

Rudder System Jammed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 12 3

Stabilizer Trim Runaway . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 12 4

Stall Recovery . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 12 5

FUEL SYSTEM

FUEL SYSTEM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 13 1

LO FUEL (Caution Message) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 13 1

ICE AND RAIN PROTECTION

ICE AND RAIN PROTECTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 14 1

WING OVHT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 14 1

ANTI-ICE DUCT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 14 1

L COWL A/I DUCT or R COWL A/I DUCT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 14 2

LANDING GEAR, WHEEL AND BRAKE SYSTEM

LANDING GEAR, WHEEL AND BRAKE SYSTEM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 15 1

MLG BAY OVHT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 15 1

BRAKE OVHT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 15 1

GEAR DISAGREE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 15 2

LDG GEAR Lever Jammed in the UP Position . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 15 3

Landing Gear Up / Unsafe Landing Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 15 4

PARKING BRAKE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 15 6

During Landing – Excessive Asymmetry or Loss of Braking . . . . . . . . . . . . . . . . . . . 03 15 6

NOSE DOOR OPEN . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 15 7

PASSENGER DOOR

PASSENGER DOOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 16 1

PASSENGER DOOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 16 1

AURAL/VISUAL WARNING SYSTEM

AURAL/VISUAL WARNING SYSTEM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 17 1

Configuration Warning . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 17 1

EMERGENCY PROCEDURES

Table of Contents

03 00 3

Rev. 8, Sep 27/2013

DOT Approved Airplane Flight Manual

CSP C 012

PAGE PRINTED ON 10-9-2015
HYDRAULIC POWER

HYDRAULIC POWER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 18 1

HYD 1 HI TEMP (Caution Message) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 18 1

HYD 2 HI TEMP (Caution Message) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 18 3

UNRELIABLE AIRSPEED

UNRELIABLE AIRSPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 19 1

Unreliable Airspeed In-flight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 19 1

LIST OF ILLUSTRATIONS

HYDRAULIC POWER

Figure 03 18 1 Maximum Landing Weight Limited by Maximum Brake

Energy – Single Hydraulic System Failure . . . . . . . . . . . . . . . . . 03 18 8

EMERGENCY PROCEDURES

Table of Contents

03 00 4

Rev. 10, Dec 22/2014

DOT Approved Airplane Flight Manual

CSP C 012

PAGE PRINTED ON 10-9-2015
1. UNRELIABLE AIRSPEED

A. Unreliable Airspeed In-flight

Indication: Pitch attitude, thrust setting or external noise not consistent with indicated

airspeed.

Large airspeed differences shown between primary flight displays and/or

standby instrument.

Loss of multiple airspeed indication.

STALL FAIL, EFIS COMP MON, EFIS COMP INOP caution messages

and/or red IAS flag.

If above minimum safe altitude:

(1) Autopilot ............................................................................................................Disengage

(2) FDs ....................................................................................................................... Deselect

(3) Use standby attitude indicator / ISI.

CAUTION

Respect stall warning/stick shaker.

(4) Proceed to step (7).

If below minimum safe altitude:

(1) Autopilot ............................................................................................................Disengage

(2) FDs ....................................................................................................................... Deselect

(3) Use standby attitude indicator / ISI.

(4) Pitch/N1 ...................................................................................................... 10 degrees/TO

(5) Airplane .................................................................. Go-around, clean up and climb above

minimum safe altitude

Above 15000 feet:

(6) Pitch/N1 ...................................................................................................... 5 degrees/CLB

CAUTION

Respect stall warning/stick shaker.

EMERGENCY PROCEDURES

Unreliable Airspeed

03−19−1

Rev. 10, Dec 22/2014

DOT Approved Airplane Flight Manual

CSP C 012

PAGE PRINTED ON 9-22-2015
(7) Set and monitor pitch and roll using standby attitude indicator or ISI. <1099>

(7) Set and monitor pitch and roll using PFD. <1025> or <1100>

When above minimum safe altitude:

(8) Pitch/N1 .......................................................... Set as per Table A to achieve approximate

level flight.

EMERGENCY PROCEDURES

Unreliable Airspeed

03−19−2

Rev. 10, Dec 22/2014

DOT Approved Airplane Flight Manual

CSP C 012

PAGE PRINTED ON 9-22-2015
Table A – Level Flight Cruise – FLAPS 0

ALT (ft) Target

Weight kg (lb)

Expected

Indicated

Airspeed/

Mach

20412

(45000)

22680

(50000)

24948

(55000)

27216

(60000)

29484

(65000) KIAS/M

40000

Pitch

(degree) 0.5 1.0 1.0 1.0 1.0 210

to

245

.70 to

.81

N1 (%) 79.6 80.6 81.6 82.7 84.3

35000

Pitch

(degree) 0.0 0.0 0.5 0.5 0.5 230

to

275

.69 to

.81

N1 (%) 78.2 78.9 79.6 80.3 81.1

30000

Pitch

(degree) −0.5 −0.5 0.0 0.0 0.5 250

to

290

–

N1 (%) 77.6 78.0 78.4 79.0 79.6

25000

Pitch

(degree) −1.0 −0.5 0.0 0.0 0.5 250

to

290

–

N1 (%) 74.0 74.5 74.9 75.5 76.2

20000

Pitch

(degree) −1.0 −0.5 0.0 0.0 0.5 250

to

290

–

N1 (%) 70.4 70.8 71.2 71.8 72.5

15000

Pitch

(degree) −1.0 −0.5 0.0 0.0 0.5 250

to

290

–

N1 (%) 66.0 67.3 67.9 68.3 68.7

10000

Pitch

(degree) 0.5 1.0 1.5 2.0 2.5 210

to

230

–

N1 (%) 55.1 55.9 56.7 57.6 58.7

5000

Pitch

(degree) 0.5 1.0 1.5 2.0 2.5 210

to

230

–

N1 (%) 51.8 52.5 53.3 54.1 55.2

If any indicated speed is outside the expected indicated airspeed range, it should be

considered UNRELIABLE.

EMERGENCY PROCEDURES

Unreliable Airspeed

03−19−3

Rev. 10, Dec 22/2014

DOT Approved Airplane Flight Manual

CSP C 012

PAGE PRINTED ON 9-22-2015
Table A – Level Flight Cruise – FLAPS 0 (continued)

ALT (ft) Target

Weight kg (lb)

Expected

Indicated

Airspeed/

Mach

31751

(70000)

34019

(75000)

36287

(80000)

38329

(84500) – KIAS/M

40000

Pitch

(degree) 1.0 – – – – 210

to

245

.70 to

.81

N1 (%) 85.6 – – – –

35000

Pitch

(degree) 1.0 1.0 1.0 1.0 – 230

to

275

.69 to

.81

N1 (%) 82.0 82.9 84.1 85.7 –

30000

Pitch

(degree) 0.5 1.0 1.0 1.5 – 250

to

290

–

N1 (%) 80.4 81.2 81.8 82.7 –

25000

Pitch

(degree) 0.5 1.0 1.0 1.5 – 250

to

290

–

N1 (%) 76.9 77.8 78.5 79.3 –

20000

Pitch

(degree) 0.5 1.0 1.5 1.5 – 250

to

290

–

N1 (%) 73.2 73.9 74.6 75.4 –

15000

Pitch

(degree) 0.5 1.0 1.5 1.5 – 250

to

290

–

N1 (%) 69.3 70.2 70.9 71.7 –

10000

Pitch

(degree) 3.0 3.0 3.5 4.0 – 210

to

230

–

N1 (%) 60.2 61.9 63.3 64.7 –

5000

Pitch

(degree) 3.0 3.0 3.5 4.0 – 210

to

230

–

N1 (%) 56.4 58.0 59.3 60.6 –

If any indicated speed is outside the expected indicated airspeed range, it should be

considered UNRELIABLE.

EMERGENCY PROCEDURES

Unreliable Airspeed

03−19−4

Rev. 10, Dec 22/2014

DOT Approved Airplane Flight Manual

CSP C 012

PAGE PRINTED ON 9-22-2015
NOTE

Procedures for EFIS COMP MON, EFIS COMP INOP, STALL FAIL

and RUD LIMITER caution messages and/or red IAS flag are

incorporated in this procedure.

(9) STALL PTCT, PUSHER switch (left or right) ...............................................................OFF

(10) Autopilot or FD ...............................................................................................PTCH/ROLL

NOTE

1. Pitch/Thrust settings will give approximate level flight, and may

result in slight climb or descent. Adjust pitch to stop climb/descent; if

displayed, VSI can be used.

2. Airspeed trend vector may be erroneous.

3. If overspeed warning sounds, select the affected AUDIO WARNING

switch to DISABLE.

4. Altitude, Mode C and TCAS may be in error by up to 600 feet.

5. Groundspeed indication may be unreliable.

6. FMS cruise time and fuel predictions may be incorrect.

7. Mach trim may be inoperative or operate erratically. Disengage

Mach trim if erratic stabilizer motion is observed.

8. Using the FD/autopilot in PTCH, ALT, HDG and ROLL modes will

help reduce workload.

9. Rudder Travel Limiter (RTL) display on EICAS synoptic will display

actual RTL limits even if RTL goal posts are amber. These limits

may be inappropriate for the phase of flight.

CAUTION

1. Do not use any FD/autopilot SPEED mode.

2. Rudder travel limits may be inappropriate for phase of flight. For

cruise and descent flight, excessive rudder input may result in

unacceptable handling characteristics or exceedence of structural

limits. For approach, landing and go-around flight, rudder authority

may be limited. Differential thrust and aileron input may be required

to assist in maintaining directional control. Select a runway with

minimum cross-wind.

(11) When the airplane is stabilized, proceed to EVALUATION within this section to regain

use of PFD / airspeed if possible.

EMERGENCY PROCEDURES

Unreliable Airspeed

03−19−5

Rev. 10, Dec 22/2014

DOT Approved Airplane Flight Manual

CSP C 012

PAGE PRINTED ON 9-22-2015
EVALUATION

(1) AIR DATA source selector ....................................................................... Select to NORM

(2) Both PFDs and standby airspeed indicator /

ISI ..........................................................................................................Compare airspeed

(3) Determine which of the following conditions apply:

If no indicated airspeed is considered reliable, proceed to CONDITION D.

If both PFDs agree and the indicated airspeed is considered reliable, proceed to

CONDITION A.

If one PFD and standby airspeed indicator / ISI agree and the indicated airspeed is

considered reliable, proceed to CONDITION B.

If only one indicated airspeed is considered reliable, proceed to CONDITION C.

WARNING

An airspeed should be considered reliable only if it is consistent with

pitch, thrust and external noise and is consistent with the expected

airspeed from Table A.

CONDITION A – If both PFDs agree and the indicated airspeed is consistent with

pitch, thrust and external noise, and the expected airspeed from Table A:

(4) Use airspeed/altitude information per normal operations.

(5) Accomplish remaining CAS messages.

CONDITION B – If one PFD and standby airspeed indicator / ISI agree and the

indicated airspeed is consistent with pitch, thrust and external noise, and the

expected airspeed from Table A:

(4) Autopilot ............................................................................................................Disengage

(5) FDs ....................................................................................................................... Deselect

(6) AIR DATA source selector ..............................................................Select to reliable side.

(7) FDs ....................................................................................................... Engage, if desired.

(8) Autopilot ............................................................................................... Engage, if desired.

(9) Use airspeed/altitude information per normal operations.

(10) Accomplish remaining CAS messages.

EMERGENCY PROCEDURES

Unreliable Airspeed

03−19−6

Rev. 10, Dec 22/2014

DOT Approved Airplane Flight Manual

CSP C 012

PAGE PRINTED ON 9-22-2015
CONDITION C – If only one indicated airspeed is consistent with pitch, thrust and

external noise, and the expected airspeed from Table A:

WARNING

Do not rely on only one airspeed unless it is in agreement with the

expected airspeed column in Table A.

Standby airspeed indicator / ISI is identified as reliable airspeed source:

(4) Use airspeed/altitude information per normal operations.

(5) Accomplish remaining CAS messages.

One PFD is identified as reliable airspeed source:

(4) Autopilot ............................................................................................................Disengage

(5) FDs ....................................................................................................................... Deselect

(6) AIR DATA source selector ..............................................................Select to reliable side.

(7) FDs ....................................................................................................... Engage, if desired.

(8) Autopilot ............................................................................................... Engage, if desired.

(9) Use airspeed/altitude information per normal operations.

(10) Accomplish remaining CAS messages.

EMERGENCY PROCEDURES

Unreliable Airspeed

03−19−7

Rev. 10, Dec 22/2014

DOT Approved Airplane Flight Manual

CSP C 012

PAGE PRINTED ON 9-22-2015
CONDITION D – If no indicated airspeed is consistent with pitch, thrust and external

noise, and the expected airspeed from Table A:

(4) Airspeed indications ............................................................................................Disregard

(5) Pitch/N1 .................................................................................................................Maintain

(6) Land at the nearest suitable airport.

NOTE

1. If environmental conditions (heavy rain, icing, ice crystals, volcanic

ash, etc) are suspected to have caused unreliable airspeed, exit

conditions as soon as possible, including descent, if required.

2. Plan to recover to an airfield with an ILS, under Visual

Meteorological Conditions if possible.

3. The following may be unreliable:

Ground proximity warning,

Enhanced ground proximity warning, <2040>

Windshear detection,

Flap overspeed,

NOSE DOOR OPEN warning message

Automatic function of passenger signs.

CAUTION

If at any time down to and including minimum safe altitude, it is suspected

that a reliable airspeed source may be available, restart the Unreliable

Airspeed In-flight procedure in order to confirm airspeed.

(7) Actual landing distance ........................................................................................ Increase

Without Thrust Reversers With Thrust Reversers

1.25 (25%) 1.20 (20%)

(8) When ready for descent, proceed to RECOVERY TO AN AIRPORT within this section.

EMERGENCY PROCEDURES

Unreliable Airspeed

03−19−8

Rev. 10, Dec 22/2014

DOT Approved Airplane Flight Manual

CSP C 012

PAGE PRINTED ON 9-22-2015
RECOVERY TO AN AIRPORT

When ready to commence descent:

CAUTION

Rudder travel limits may be inappropriate for phase of flight. For cruise and

descent flight, excessive rudder input may result in unacceptable handling

characteristics or exceedence of structural limits. For approach, landing and

go-around flight, rudder authority may be limited. Differential thrust and aileron

input may be required to assist in maintaining directional control. Select a runway

with minimum cross-wind.

(1) Pitch ...................................................................... Adjust as per Table B, and continue to

adjust pitch during descent:

Table B – Descent – FLAPS 0 – IDLE

Altitude (ft) 0 5000 10000 15000 20000 25000 30000 35000 40000

Pitch

(degree) −2.5 −2.5 −3.0 −3.5 −3.5 −3.5 −3.0 −3.0 −2.0

(2) Thrust levers .............................................................................................................. IDLE

NOTE

With anti-ice ON, increase N1 if required to obtain the minimum N2 of 75%

For an N1 increase of 5%, add 0.5 degree to the pitch from Table B.

For an N1 increase of 10%, add 1.0 degree to the pitch from Table B.

For an N1 increase of 15%, add 1.5 degree to the pitch from Table B.

CAUTION

Do not extend flaps until directed later in the procedure. The range of

airspeeds possible in Table B could result in a significant flap overspeed

and flap damage. The aircraft must be leveled off and slowed down

before flaps can be extended.

NOTE

Plan to intercept a long final to allow time to re-configure for

approach/landing and set pitch/N1.

If intermediate level off is required during the descent:

EMERGENCY PROCEDURES

Unreliable Airspeed

03−19−9

Rev. 10, Dec 22/2014

DOT Approved Airplane Flight Manual

CSP C 012

PAGE PRINTED ON 9-22-2015
(3) Pitch/N1 ........................................................ Set as per Table C, then adjust pitch to stop

climb/descent.

Table C – Level Flight – Cruise FLAPS 0

ALT (ft) Target

Weight kg (lb)

Expected

Indicated

Airspeed/

Mach

20412

(45000)

22680

(50000)

24948

(55000)

27216

(60000)

29484

(65000) KIAS/M

35000

Pitch

(degree) 0.0 0.0 0.5 0.5 0.5 230

to

275

.69 to

.81

N1 (%) 78.2 78.9 79.6 80.3 81.1

30000

Pitch

(degree) −0.5 −0.5 0.0 0.0 0.5 250

to

290

–

N1 (%) 77.6 78.0 78.4 79.0 79.6

25000

Pitch

(degree) −1.0 −0.5 0.0 0.0 0.5 250

to

290

–

N1 (%) 74.0 74.5 74.9 75.5 76.2

20000

Pitch

(degree) −1.0 −0.5 0.0 0.0 0.5 250

to

290

–

N1 (%) 70.4 70.8 71.2 71.8 72.5

15000

Pitch

(degree) −1.0 −0.5 0.0 0.0 0.5 250

to

290

–

N1 (%) 66.0 67.3 67.9 68.3 68.7

If any indicated speed is outside the expected indicated airspeed range, it should be

considered UNRELIABLE.

EMERGENCY PROCEDURES

Unreliable Airspeed

03−19−10

Rev. 10, Dec 22/2014

DOT Approved Airplane Flight Manual

CSP C 012

PAGE PRINTED ON 9-22-2015
Table C – Level Flight – Cruise FLAPS 0 (continued)

ALT (ft) Target

Weight kg (lb)

Expected

Indicated

Airspeed/

Mach

31751

(70000)

34019

(75000)

36287

(80000)

38329

(84500) – KIAS/M

35000

Pitch

(degree) 1.0 1.0 1.0 1.0 – 230

to

275

.69 to

.81

N1 (%) 82.0 82.9 84.1 85.7 –

30000

Pitch

(degree) 0.5 1.0 1.0 1.5 – 250

to

290

–

N1 (%) 80.4 81.2 81.8 82.7 –

25000

Pitch

(degree) 0.5 1.0 1.0 1.5 – 250

to

290

–

N1 (%) 76.9 77.8 78.5 79.3 –

20000

Pitch

(degree) 0.5 1.0 1.5 1.5 – 250

to

290

–

N1 (%) 73.2 73.9 74.6 75.4 –

15000

Pitch

(degree) 0.5 1.0 1.5 1.5 – 250

to

290

–

N1 (%) 69.3 70.2 70.9 71.7 –

If any indicated speed is outside the expected indicated airspeed range, it should be

considered UNRELIABLE.

For continued descent:

(3) Pitch ................................................................................................Adjust as per Table D:

Table D – Descent – FLAPS 0 – IDLE

Altitude (ft) 0 5000 10000 15000 20000 25000 30000 35000 40000

Pitch

(degree) −2.5 −2.5 −3.0 −3.5 −3.5 −3.5 −3.0 −3.0 −2.0

At initial approach altitude:

(4) Pitch/N1 ........................................................ Set as per Table E, then adjust pitch to stop

climb/descent.

EMERGENCY PROCEDURES

Unreliable Airspeed

03−19−11

Rev. 10, Dec 22/2014

DOT Approved Airplane Flight Manual

CSP C 012

PAGE PRINTED ON 9-22-2015
Table E – Level Flight – Approach FLAPS 0

ALT (ft) Target

Weight kg (lb) Expected

Indicated

Airspeed

KIAS

20412

(45000)

22680

(50000)

24948

(55000)

27216

(60000)

29484

(65000)

15000

Pitch

(degree) 0.5 1.0 1.5 2.0 2.5

210 to 230

N1 (%) 58.7 59.5 60.3 61.3 62.4

10000

Pitch

(degree) 0.5 1.0 1.5 2.0 2.5

210 to 230

N1 (%) 55.1 55.9 56.7 57.6 58.7

5000

Pitch

(degree) 0.5 1.0 1.5 2.0 2.5

210 to 230

N1 (%) 51.8 52.5 53.3 54.1 55.2

0

Pitch

(degree) 0.5 1.0 1.5 2.0 2.5

210 to 230

N1 (%) 48.4 49.0 49.6 50.3 51.5

If any indicated speed is outside the expected indicated airspeed range, it should be

considered UNRELIABLE.

EMERGENCY PROCEDURES

Unreliable Airspeed

03−19−12

Rev. 10, Dec 22/2014

DOT Approved Airplane Flight Manual

CSP C 012

PAGE PRINTED ON 9-22-2015
Table E – Level Flight – Approach FLAPS 0 (continued)

ALT (ft) Target

Weight kg (lb) Expected

Indicated

Airspeed

KIAS

31751

(70000)

34019

(75000)

36287

(80000)

38329

(84500) –

15000

Pitch

(degree) 3.0 3.0 3.5 4.0 – 210 to 230

N1 (%) 63.9 65.5 67.1 68.6 –

10000

Pitch

(degree) 3.0 3.0 3.5 4.0 – 210 to 230

N1 (%) 60.2 61.9 63.3 64.7 –

5000

Pitch

(degree) 3.0 3.0 3.5 4.0 – 210 to 230

N1 (%) 56.4 58.0 59.3 60.6 –

0

Pitch

(degree) 3.0 3.0 3.5 4.0 – 210 to 230

N1 (%) 52.6 54.2 55.4 56.6 –

If any indicated speed is outside the expected indicated airspeed range, it should be

considered UNRELIABLE.

NOTE

Allow sufficient time for stabilization prior to reconfiguring the airplane due to the

pitch change as flaps are extended from 0 to 20.

When stabilized:

(5) FLAPS ............................................................................................................ Select to 20.

(6) Pitch/N1 .........................................................Set as per Table F, then adjust pitch to stop

climb/descent.

Table F – Approach (Level Flight) – FLAPS 20 – Gear UP

Weight kg (lb)

20412

(45000)

22680

(50000)

24948

(55000)

27216

(60000)

29484

(65000)

Pitch (degree) −1.0 −0.5 0.0 1.0 2.0

N1 (%) 55.8 56.8 57.7 59.6 61.8

EMERGENCY PROCEDURES

Unreliable Airspeed

03−19−13

Rev. 10, Dec 22/2014

DOT Approved Airplane Flight Manual

CSP C 012

PAGE PRINTED ON 9-22-2015
Table F – Approach (Level Flight) – FLAPS 20 – Gear UP (continued)

Weight kg (lb)

31751

(70000)

34019

(75000)

36287

(80000)

38329

(84500) –

Pitch (degree) 2.5 3.5 4.0 4.5 –

N1 (%) 63.6 65.5 66.9 68.2 –

NOTE

Heading and ILS/VOR course deviation indicator information on the PFD are

reliable and will aid situational awareness.

(7) Final course .......................................................................................................... Intercept

Upon intercept of final course (long final):

(8) LDG GEAR lever ...........................................................................................................DN

(9) FLAPS ............................................................................................................ Select to 30.

(10) Pitch/N1 ........................................................Set as per Table G, then adjust pitch to stop

climb/descent.

Table G – Approach (Level Flight) – FLAPS 30 – Gear DN

Weight kg (lb)

20412

(45000)

22680

(50000)

24948

(55000)

27216

(60000)

29484

(65000)

Pitch (degree) −1.5 −0.5 0.0 1.0 2.0

N1 (%) 63.8 64.1 65.0 66.2 67.5

EMERGENCY PROCEDURES

Unreliable Airspeed

03−19−14

Rev. 10, Dec 22/2014

DOT Approved Airplane Flight Manual

CSP C 012

PAGE PRINTED ON 9-22-2015
Table G – Approach (Level Flight) – FLAPS 30 – Gear DN (continued)

Weight kg (lb)

31751

(70000)

34019

(75000)

36287

(80000)

38329

(84500) –

Pitch (degree) 3.0 4.0 5.0 6.0 –

N1 (%) 69.3 71.1 73.0 74.8 –

CAUTION

Do not descend for final approach with flaps 30. The aircraft must remain

level with gear down/flaps 30 or a flap overspeed and flap damage could

result. Flaps 45 is selected at the start of the descent on the

glideslope/glidepath.

At glideslope capture or descent point:

(11) FLAPS ............................................................................................................ Select to 45.

(12) Pitch/N1 ............................................................................................... Set as per Table H:

Table H – Approach – FLAPS 45 – Gear DN – 3 degree G/S

ALT (ft) Target

Weight kg (lb)

20412

(45000)

22680

(50000)

24948

(55000)

27216

(60000)

29484

(65000)

15000

Pitch

(degree) 0.5 0.5 0.5 1.0 1.0

N1 (%) 59.9 62.6 65.5 67.4 69.6

10000

Pitch

(degree) 0.5 0.5 0.5 1.0 1.0

N1 (%) 55.9 58.5 60.9 63.2 65.5

5000

Pitch

(degree) 0.5 0.5 0.5 1.0 1.0

N1 (%) 52.1 54.7 57.0 59.2 61.4

0

Pitch

(degree) 0.5 0.5 0.5 1.0 1.0

N1 (%) 48.6 51.1 53.3 55.4 57.6

This table results in airspeeds equal to VREF ± 10 kts.

EMERGENCY PROCEDURES

Unreliable Airspeed

03−19−15

Rev. 10, Dec 22/2014

DOT Approved Airplane Flight Manual

CSP C 012

PAGE PRINTED ON 9-22-2015
Table H – Approach – FLAPS 45 – Gear DN – 3 degree G/S (continued)

ALT (ft) Target

Weight kg (lb)

31751

(70000)

34019

(75000)

36287

(80000)

38329

(84500) –

15000

Pitch

(degree) 1.0 1.0 1.0 1.0 –

N1 (%) 71.8 74.0 75.9 78.0 –

10000

Pitch

(degree) 1.0 1.0 1.0 1.0 –

N1 (%) 67.6 69.7 71.5 73.6 –

5000

Pitch

(degree) 1.0 1.0 1.0 1.0 –

N1 (%) 63.5 65.6 67.4 69.4 –

0

Pitch

(degree) 1.0 1.0 1.0 1.0 –

N1 (%) 59.6 61.6 63.4 65.3 –

This table results in airspeeds equal to VREF ± 10 kts.

(13) Pitch ......................................................................... Set to maintain glideslope/glidepath.

(14) N1 ...........................................................................Maintain as per Table H – Approach –

FLAPS 45 – Gear DN – 3 degree G/S.

EMERGENCY PROCEDURES

Unreliable Airspeed

03−19−16

Rev. 10, Dec 22/2014

DOT Approved Airplane Flight Manual

CSP C 012

PAGE PRINTED ON 9-22-2015