38 1 30MB
Operations Reference Manual
the evolution of mobility
BOMBARDIER AIRCRAFT TRAINING DFW Training Center Montreal Training Centre 2929 West Airfield Drive 8575 Côte-de-Liesse Road P.O. Box 619011 Saint-Laurent, Quebec, Canada DFW Airport, TX 75261 H4T 1G5 Telephone (469) 791-4200 Telephone (514) 344-6620 Toll-Free North America Toll-Free North America 1 (888) 679-4200 1 (877) 551-1550 Fax (469) 791-4201 Fax (514) 344-6643 www.batraining.com www.cic.bombardier.com
Please be aware that this version of the Bombardier Training Manual has been updated only for the current training course(s) that you are attending, and may only be used as part of the current course(s). If you would like to continue using this version after completing the training course(s), understand that the content may become outdated. If you would like the benefit of ongoing updates, we require you to register for a subscription service for this Bombardier Training Manual at the following website: http://www.batraining.com. Bombardier Inc., by its groups, divisions, or its corporate subsidiary Learjet Inc. (collectively "Bombardier"), provides this information to its customers and to the government in confidence. This is proprietary confidential information, which we consider excluded from the application of the Access to Information Act or any other similar statute with respect to access to information, and may also be a trade secret of Bombardier. Public release of this information would be harmful to Bombardier or its corporate subsidiary Learjet Inc. Any intention to disclose such information, or part thereof, must be indicated in advance and in writing to the Vice-President Legal Services, Bombardier Aerospace. It is understood that this documentation, comprising technical data and other information in any media shall not be reproduced or disclosed, in whole or in part, without Bombardier's prior written authorization. It is proprietary and confidential to Bombardier or its corporate subsidiary Learjet Inc. All rights and all patent, copyright, trademark, trade secrets, and other intellectual property rights herein belong to Bombardier or its corporate subsidiary Learjet Inc. This documentation, technical data, and other information shall not be modified, translated, reverse assembled, reverse engineered, or decompiled and shall be used solely for training purposes. Copyright © 1999-2012 Bombardier Inc. or its subsidiaries. All rights reserved. Bombardier and Challenger are either Unregistered or Registered trademarks of Bombardier Inc. or its subsidiaries.
002
INTRODUCTION OPERATIONS REFERENCE MANUAL
Introduction
CONTENTS 1.
EXPANDED CHECKLIST
2.
PROCEDURES
3.
SYSTEMS
4.
LIMITATIONS
5.
PERFORMANCE
6.
SERVICING
7.
ADVERSE WEATHER / WINDSHEAR
8.
LONG-RANGE NAVIGATION
9.
SECURITY CHECKLIST
10. RVSM 11. APPENDIX
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
INTRO-1
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INTRODUCTION OPERATIONS REFERENCE MANUAL
Page Intentionally Left Blank
INTRO-2
June 2012
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
TABLE OF CONTENTS General ...................................................................................................................... 1-1 Normal Power-Up Check ........................................................................................... 1-2 Systems Check ........................................................................................................ 1-15 Before Start Checks ................................................................................................. 1-51 Start Check .............................................................................................................. 1-61 Failure to Start.......................................................................................................... 1-66 After Engine Start Check.......................................................................................... 1-66 Taxi Check ............................................................................................................... 1-77 Takeoff Check .......................................................................................................... 1-81 After Takeoff Check ................................................................................................. 1-87 Climb Check............................................................................................................. 1-89 Cruise Check............................................................................................................ 1-93 Descent Check......................................................................................................... 1-95 In Range Check ....................................................................................................... 1-99 Before Landing Check............................................................................................ 1-101 After Landing Check............................................................................................... 1-105 Shutdown Check .................................................................................................... 1-108 Securing Check...................................................................................................... 1-116
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
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EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
THIS PAGE INTENTIONALLY LEFT BLANK
1-ii
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FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
GENERAL Before power (electrical, hydraulic or pneumatic) can be safely applied to the airplane, the external inspection must be made, either by qualified technical/maintenance ground staff or by the pilot. Once power has been applied to the airplane, the pilot performs the cabin inspection, the external walkaround and the systems check (if required). The cabin inspection and systems checks are required: • • • • •
Before the airplane’s first flight of the day After a crew change After any related non-routine maintenance action If the airplane was left unattended by qualified personnel, or If the pilot-in-command has any doubt about the airplane status
1 First flight of the day: • The Normal Power-Up Check and the Systems Check must be accomplished in its entirety on the first flight of the day • On subsequent flights, if the airplane is powered-down (or if the flight crew is replaced), the above checks are accomplished with the exception of those items suffixed with 1 2 Last flight of the day: • Verification of the master chip detector indicators must be carried out on the last flight of the day
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
1-1
June 2012
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
NORMAL POWER-UP CHECK 1.
Airplane and flight pubs ....................................................................ON BOARD Airplane publications include: • • • • • • •
Airplane Flight Manual Operating Manuals Volumes 1 and 2 Flight Planning and Cruise Control Manual Weight and Balance Manual Collins FMS 6000 Pilot Guide Quick Reference Handbook Volumes 1 and 2 Minimum Equipment List (if applicable) NOTE
Refer to FCOM Vol 2, Circuit Breaker Reset for Bombardier Aerospace philosophy and policy with respect to the resetting of tripped circuit breakers. Circuit breakers (panels 1-4)................................................................. CLOSED • STAB CH1 and CH2 HSTCU circuit breakers (2F8 and 4B8) 1 Review Location STAB CH 1 HSTCU
STAB CH 2 HSTCU
3
3
8
3.
4.
8
604_ORM_01_234
2.
Emergency equipment............................................................................. CHECK • Crash axe (behind left crew seat) • Halon fire extinguisher (behind right crew seat and designated area in the cabin) • Life vests (underside of the seats) • Oxygen masks and flashlights • Portable oxygen bottle or PBEs, as appropriate Hydraulic pumps ............................................................................................ OFF
ON OFF AUTO 1
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ON OFF AUTO
ON OFF AUTO
OFF ON 3A
3B
2
604_ORM_01_076
HYDRAULIC
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
5.
NOSE STEER .................................................................................................. OFF
6.
LDG GEAR lever............................................................................................... DN HORN NOSE STEER ARMED
LDG GEAR MUTED
OFF ANTI-SKID
TEST
UP
ARMED
DN
OFF DN LCK REL OVHT
7.
604_ORM_01_077
MLG BAY OVHT TEST FAIL
FLIGHT SPOILER lever ................................................................... RETRACTED
FLIGHT SPOILER 0
1/4 RETRACT
1/2
MAX
604_ORM_01_078
3/4
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
1-3
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EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
FLAPS lever/position .............................................................CHECK/MATCHED • Set FLAP lever so that it agrees with actual flap position noted in the safety inspection. This is normally 0.
- GEAR -
0
0 STAB NU
20
5.0
20
30
45
45
AIL
LWD
RWD
RUDDER
ND
30
- TRIM -
NL
NR
604_ORM_01_079
FLAPS 0
9.
- FLAPS -
DN DN DN
Weather radar ................................................................................................. OFF
SEC
-1 -2 -3
NORM
+1 +2 +3
XFR
STAB
TILT
MAP WX TEST WX+T OFF TURB
604_ORM_01_080
8.
ADG
1-4
June 2012
605_ORM_01_005
10. ADG manual release ..............................................................................STOWED
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
11. BATT MASTER.................................................................................................. ON NOTE 1. Flight compartment standby lights come on when the battery bus is powered and normal AC power is off. 2. When using the main battery as the only source of power, do not exceed 5 minutes of operation, as there will be insufficient cooling of the displays. 12. DC ELECTRICAL page...............................................CHECK 22 VDC MINIMUM • Push the DC ELEC button on the CCP • Check voltages >22 V (minimum for APU starting)
DC ELECTRICAL AC BUS 1
AC BUS 2
TRU 1
TRU 2
0 V 0 A
0 V 0 A
AC ESS BUS
ESS TRU 2 0 V 0 A
ESS TRU 1 0 V 0 A
BUS 1
ESS BUS
BUS 2
BATT BUS
TIE
UTIL BUS 1
EMER BUS
MAIN BATT DIR BUS
UTIL BUS 2 EXT DC 28 V 19 A
APU BATT 24 V 18 A
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
MAIN BATT 24 V 18 A
604_ORM_01_001
APU BATT DIR BUS
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EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
13. Firex monitor system test 1 ............................................................ COMPLETE a) FIREX MONITOR switches (all) ...................... Select TEST and hold • Check advisory messages, on during the test and out after test completion
TEST
FIREX MONITOR TEST TEST
FIRE DET
WARN
R ENG SQUIB 2 OK R ENG SQUIB 1 OK L ENG SQUIB 2 OK L ENG SQUIB 1 OK APU SQUIB 2 OK APU SQUIB 1 OK
AURAL WARN TEST 1
2 2
ENG BOTTLE
TEST
L
SPS TEST TEST
R
APU BOTTLE
TEST
FAIL
OVSP TEST
LAMP TEST 1
1
2
2
G SWITCH
604_ORM_01_002
1
14. Fire detection system test 1 ........................................................... COMPLETE a) FIRE DET switch ....................................... Select to WARN and hold • Fire bell sounds, JETPIPE OVERHEAT aural on and all FIRE PUSH and BOTTLE ARMED PUSH TO DISC switch/lights illuminate during the test • Check for warning messages, on during the procedure and out after completion FIREX MONITOR TEST TEST
FIRE DET
N WARN
AURAL WARN TEST 1
2 1
2
ENG BOTTLE
TEST
L
SPS TEST TEST
R
APU BOTTLE
TEST
FAIL
OVSP TEST
R JETPIPE OVHT R ENGINE FIRE L JETPIPE OVHT L ENGINE FIRE APU FIRE
LAMP TEST 1
1
2
2
G SWITCH
Fire Bell On “JETPIPE OVERHEAT”
1-6
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604_ORM_01_003
TEST
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
14. Fire detection system test 1 ..................................................................(Cont’d) b) FIRE DET switch ........................................... Select to FAIL and hold • Check for caution messages, on during the procedure and out after completion
TEST
FIREX MONITOR TEST TEST
FIRE DET
WARN
R JETPIPE OVHT FAIL R FIRE FAIL L JETPIPE OVHT FAIL L FIRE FAIL APU FIRE FAIL
AURAL WARN TEST 1
2 2
TEST
L
FAIL
APU BOTTLE
ENG BOTTLE
SPS TEST TEST
R
OVSP TEST
TEST
604_ORM_01_004
1
LAMP TEST 1
1
2
2
G SWITCH
15. NAV lights ......................................................................................................... ON IND LTS
MISC LTS
OVHD
DOME
OFF
OFF
DIM D
ON
ON
BRT OFF
BRT
EXTERNAL LTS NAV OFF O ON
A/COLL WING-INSP BEACON OFF OFF OFF O ON
O ON
O ON
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
LOGO OFF O ON
604_ORM_01_082
BOARD
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EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
16. APU (if required).........................................................................................START a) APU GEN switch ..................................................... OFF and RESET
b) 10TH STAGE, APU LCV switch/light ............................. Pressed Out
BLEED AIR NORM
14TH STAGE DUCT FAIL
OPEN
CLOSED L
DUCT MON
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June 2012
DUCT FAIL CLOSED
ISOL
R
10TH STAGE DUCT FAIL
FAIL
CLOSED
OPEN
L
APU LCV
OPEN
DUCT FAIL CLOSED
ISOL
R
604_ORM_01_201
LOOP A LOOP B
TEST
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
16. APU (if required)...................................................................................... (Cont’d) c) APU, PWR FUEL switch/light................................................ Press In • Check RPM and EGT indications appear on the EICAS page
0
PUMP FAIL SOV CLOSED
START
PWR FUEL
START/ STOP
604_ORM_01_005
APU
APU
0
AVAIL
EGT
RPM
EICAS Status Page
d) APU, START/STOP switch/light ............................................ Press In On at 95% rpm + 4 sec
START
START
AVAIL
AVAIL
START/ STOP
START/ STOP
(100% + 15 sec) APU GEN OFF
604_ORM_01_006
On through 60% rpm
After APU RPM and EGT have stabilized: e) APU GEN switch ............................................................Select to ON
ELECTRICAL POWER BATT MASTER
EXT. POWER AVAIL
OFF
IN USE
ON O
AC
IN USE DC
AC POWER GEN 1
APU GEN OFF/ R RESET
GEN 2
OFF/ RESET ON O
ON O
FAIL
OFF/ RESET O ON
FAIL AUTOXFER
ESS. POWER
OFF
DC POWER
ALTN
CLOSED
AC ESS XFER
MAIN BUS TIE
604_ORM_01_083
OFF
If APU and AC external power are not available: 16. Battery/External Air - Engine Start .................................................. COMPLETE • Proceed to step 23
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
1-9
June 2012
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
17. AC and DC electrics..................................................................... ESTABLISHED a) AC ELECTRICAL page ............................................................ Select • Check voltage (115 V), frequency (400 Hz) and load indications (approximately 8 kVA) are shown for APU generator output and all AC buses are green outline AC ELECTRICAL
115 V 400 HZ
ADG
UTIL BUS 1
UTIL BUS 2
BUS 1
BUS 2 ESS BUS
0 KVA 0V 0 HZ
EXT AC
8 KVA 115 V 400 HZ
GEN 1
0 KVA 0V 0 HZ GEN 2
GEN APU
604_ORM_01_007
116 V 400 HZ
b) DC ELECTRICAL page ............................................................ Select • Check all TRUs (28 V+) and load indications (approx.10 amps for main TRUs and 20 amps for essential TRUs) • Check all DC buses are green outline, and battery chargers are operating (26 V + with 0 amps shown in each battery symbol) DC ELECTRICAL AC BUS 1
AC BUS 2
TRU 1
TRU 2
28 V 10 A
28 V 10 A
AC ESS BUS
ESS TRU 2 28 V 21 A
ESS TRU 1 28 V 20 A
BUS 1
ESS BUS
BUS 2
BATT BUS
TIE
UTIL BUS 1
EMER BUS
MAIN BATT DIR BUS
UTIL BUS 2 EXT DC 28 V 19 A
1-10
June 2012
APU BATT 28 V 0 A
MAIN BATT 28 V 0 A
604_ORM_01_202
APU BATT DIR BUS
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
18. Lamp test 1 ...................................................................................... COMPLETE a) LAMP TEST switch ............................................ Select to 1 and hold • Check all switch/lights come on • Release the switch and check all switch/lights go out b) LAMP TEST switch ............................................ Select to 2 and hold • Check all switch/lights come on • Release the switch and check all switch/lights go out
19. Bleed leak detection test 1 ............................................................. COMPLETE a) DUCT MON knob ........................................Rotate to TEST and hold
TEST
LOOP A LOOP B
14TH STAGE DUCT FAIL
OPEN
CLOSED L
DUCT MON
DUCT FAIL CLOSED
ISOL
R 1OTH DUCT L 14TH DUCT L 1OTH DUCT R 14TH DUCT ANTI-ICE DUCT 604_ORM_01_009
BLEED AIR NORM
R
10TH STAGE DUCT FAIL
FAIL
CLOSED
OPEN
L
APU LCV
OPEN
DUCT FAIL CLOSED
ISOL
R
“Bleed Air Duct”
DUCT TEST OK
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
1-11
June 2012
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
19. Bleed leak detection test ........................................................................ (Cont’d) b) DUCT MON knob .................................... Select to LOOP A and hold LOOP A TEST OK
BLEED AIR NORM LOOP A LOOP B
Without warning messages
DUCT FAIL
OPEN
CLOSED L
DUCT MON
DUCT FAIL CLOSED
ISOL
R
10TH STAGE DUCT FAIL
FAIL
CLOSED
OPEN
L
APU LCV
OPEN
DUCT FAIL CLOSED
ISOL
R
604_ORM_01_053
TEST
14TH STAGE
c) DUCT MON knob .................................... Select to LOOP B and hold LOOP B TEST OK
BLEED AIR NORM LOOP A LOOP B
DUCT FAIL
OPEN
CLOSED L
DUCT MON
Without warning messages DUCT FAIL CLOSED
ISOL
R
10TH STAGE DUCT FAIL
FAIL
CLOSED
OPEN
L
APU LCV
OPEN
DUCT FAIL CLOSED
ISOL
R
604_ORM_01_054
TEST
14TH STAGE
d) DUCT MON knob .................................................. Release to NORM • Check that no messages appear 20. APU LCV ...................................................................................................... OPEN • If time permits, wait 2 minutes before selecting the APU air on • Check APU LCV OPEN caption on
1-12
June 2012
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
21. 10TH STAGE ISOL....................................................................................... OPEN • Check white OPEN light illuminated in switch/light • APU air indicates on when all 10TH-STAGE switch/lights white captions are illuminated BLEED AIR NORM
14TH STAGE
LOOP A LOOP B
DUCT FAIL
DUCT FAIL
OPEN
CLOSED L
DUCT MON
CLOSED R
ISOL
10TH STAGE DUCT FAIL
FAIL
DUCT FAIL
OPEN
CLOSED
OPEN
L
APU LCV
CLOSED R
ISOL
604_ORM_01_055
TEST
22. PACKs ............................................................................................................... ON • Check left and right PACK OFF lights out AIR CONDITIONING CKPT NORM
STBY
PACK MAN
CABIN
L
R
FAIL
FAIL
OFF
OFF
NORM
STBY
MAN
RAM-AIR
CABIN TEMP
OPEN
CKPT HEAT COLD
HOT
OFF O
COLD
ON
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
HOT
604_ORM_01_056
CKPT TEMP
1-13
June 2012
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
23. IRS ................................................................................................................... NAV • Set all IRS selectors to NAV
NAV
NAV
OFF
ATT
OFF
1
IRS
ATT
2
604_ORM_01_057
NAV OFF
ATT
3
IRS
24. ALL FMS.................................................................................................. POS INIT Initialize position: a) On STATUS page ( IDX > STATUS), check database is current (no amber or dashed indications) and software version -034 or later. b) IDX > POS INIT NEXT > GPS1/2 POS (select on-side GPS) PREV > SET POS (push > SET POS again if RESET INITIAL POS message shown on FMS control panel). c) IDX NEXT > FMS CTRL > SYNC. Select either FMS as Sync Master.
POS
BRT
STATUS
TEXT DISPLAY NAV DATA
118.90
16MAR06 12APR06
> 119.90
16FEB06 15MAR06 --MODE--
110.50
PRE2
SEC DATA BASE UTC
PROGRAM ATC1
1-14
June 2012
] IDX
TUNE
EXEC
PREV
NEXT
604_ORM_01_203
12:37
DIR
COM2
WORLD
ACTIVE DATA BASE
MSG
1/2
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
SYSTEMS CHECK 1.
Seat and harness .................................................................................... ADJUST • Sunvisors, chart holders and map lights • Headset/boom microphone
2.
Rudder pedals ......................................................................................... ADJUST NOTE The nose doors are operated by No. 3 hydraulic pressure and controlled by the switch located in the AC external power panel (right forward fuselage). When nosewheel area is confirmed clear:
3.
Hydraulic pump 3A .......................................................................................... ON • Push the HYD button on EICAS control panel to display the HYDRAULIC synoptic page. Check pump 3A pressure is approximately 3000 psi
HYDRAULIC ON OFF AUTO 1
ON OFF AUTO
ON OFF AUTO
OFF ON 3A
3B
2
HYDRAULIC 30 °C
32 °C
30 °C
49%
82%
76%
3A
3B
2B
INBD BRAKES 3000 PSI
OUTBD BRAKES 0 PSI
0 PSI
3000 PSI
0 PSI
RUDDER L ELEVATOR L AILERON FLT SPLR GND SPLR
RUDDER L ELEVATOR R L AILERON R LDG GEAR N/W STEER NOSE DOOR
RUDDER ELEVATOR R AILERON R FLT SPLR MLG AUX ACT
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
2A
604_ORM_01_075
1B 1A
1-15
June 2012
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
Nosewheel door ..................................................................................... CLOSED • Check nose doors are closed. Note: Doors are open with NOSE DOOR OPEN warning message shown NOSE DOOR OPEN PASSENGER DOOR R ENG OIL PRESS L ENG OIL PRESS L WSHLD HEAT L WINDOW HEAT R WSHLD HEAT R WINDOW HEAT OUTBD BRAKE PRESS R PROBE HEAT OFF
Oxygen system check ..................................................................... COMPLETE a) Oxygen pressure ...................................................................... Check • On ED2, check pressure is sufficient and verify OXY LO PRESS caution message out
OXY
1840
C ALT
300
RATE
0
¨3
2; CYOW
23MAY06 23JUN06
TOW/ GWT/MTOW V2: 142 39.1 / 39.1 / 45.2 RW06L --MODE-TOFL/RW33 VFTO: 169
7747 /13700 FT ENG BLEED
BOTH/ONE [ NO GPS RAIM
SEND> ]
THRUST REV
1/2BNK
TO
DR
TO PATH GS
4
AP
60
20
2
300
10
1
200
0
40 VT 150 V2 133 VR 121 V1 113 M.765
25000
ALTS
VOR1
200 80
EXEC
1
100 000
10
50 FT
2
1
100
2
29.92 IN
4
20
604_ORM_01_109
MSG
YUL
ETA
10. FMS messages ......................................................................................... CHECK • On each FMS, select MSG to display message page, review messages
1-58
June 2012
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
11. Radios/Navaids ...............................................................SET FOR DEPARTURE • Set up the radios and Nav aids for departure: • Select com radios frequencies. Select desired VHF com for transmitting on both audio panels • Optionally, the nav radios can be selected to AUTO on either FMS TUNE page (TUNE button). This selection enables the FMS to use channel 1 of the on-side DME for DME-DME position solutions • NAV1 and NAV2 MAN/AUTO selection as required • Cyan AUTO appears on the RTU for the nav set-up • Do not enter nav frequencies or select DME HOLD as this overrides the auto selection and VHF nav frequency tuning reverts to manual control
POS
BRT
RADIO TUNING COM1
118.00
TEXT DISPLAY
> 119.90 NAV2
NAV1
116.30
--MODE--
NAV1
110.50 NAV2
AUTO/MAN
AUTO/MAN
ENG BLEED
ADF
]
ATC2
ATC1
DIR
COM2
118.90 PRE2
PRE1
136.90
MSG
1/5
FPLM
LEGS
DEP ARR
ACT
COM1
PERF
IDX
TUNE
EXEC
PREV
NEXT
T
R
B
ACT
116.30 ADF 1
281.0 NEXT PAGE
PRE
NAV1 PRE AUT 110.50
DME-H
1/2
TCAS AUTO REL
ATC1
6041
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
IDENT
136.90
604_ORM_01_111
118.00
1-59
June 2012
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
12. Takeoff data .................................................................................................... SET • Select MFD DATA “TAKEOFF REFERENCE” page and review the data
FPLN
LEGS
MFD DATA
MFD MENU
MFD ADV
1
2
3
4
5
6
7
8
9
.
O
+/-
RWY RWY RWY RWY RWY
TAKEOFF REFERENCE ID WIND LENGTH SLOPE COND
WIND OAT QNH P AL T TOW GWT MTOW
1/2 V1: 11O VR: 122 V2: 132
21O°/ 12 KT +18°C 29.92 1N 133O FT
VFTO/VT: 157 TOFL: 4126 FT
37.3 LB 37.3 LB 41.9 LB
ENG BLEED APR THRUST REV CG
FMS CDU
RW19R H12 R3 1O3OO FT DO.2% WET
OCR CLB GRAD: 533 FT/NM
OFF ARMED BOTH 29 %
TRIM: 5.O TO: 9O.7 MCT: 92.3
604_ORM_01_110
KICT DIR
MFD Takeoff Reference Page
• Ensure N1, V1, VR, V2, VT and stabilizer trim are set for takeoff
200 80
0.0
- GEAR -
DN DN DN 60
0 ITT
0.0 N2
40 VT 157 V2 132 VR 122 V1 110
STAB NU
5.0 ND
604_ORM_01_235
N1 86.0 TO
13. Takeoff briefing.................................................................................. COMPLETE • Use TSRED format as detailed in ORM Procedures Chapter
1-60
June 2012
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
START CHECK 1.
PASSENGER Door ................................................................................. CLOSED • Check advisory message on DOOR CLOSED 604_ORM_01_212
Fuel quantity and balance ........................................................................CHECK • Check fuel quantity is sufficient for the proposed trip and main tank quantities are within 400 lb of each other • Check fuel temperature is within normal limits 0 0 15 0.0
FF (PPH) OIL PRESS OIL TEMP FAN VIB
- FUEL (LBS) - TOTAL
4890
16780 4890
BEACON, (if installed) ..................................................................................... ON IND LTS
MISC LTS BOARD
OVHD
DOME
OFF
OFF
DIM
ON
ON
B BRT OFF
BRT
EXTERNAL LTS NAV OFF O ON
A/COLL WING-INSP BEACON OFF OFF OFF O ON
O ON
O ON
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
LOGO OFF O ON
604_ORM_01_116
3.
5000 2000
0 0 15 0.0
604_ORM_01_015
2.
1-61
June 2012
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
4.
L and R BOOST PUMPs................................................................................... ON • When the first switch/light is pressed in, check ON captions illuminate in both BOOST PUMP switch/lights and advisory messages are shown on EICAS R FUEL PUMP ON L FUEL PUMP ON
FUEL BOOST PUMP
INOP
INOP
ON
ON
L
R
XFLOW
ON
OPEN
ON
L TO AUX
GRAVITY
R TO AUX
TAIL TANK TRANSFER
5.
FAIL FA F
AUTO A AU IINHIB IN
FAIL FA F
FAIL FA F
ON
MANUAL
ON
OPEN
PRI
MANUAL OVRD
SEC
DUMPS AT 0º FLAPS ONLY
604_ORM_01_039
DUMP
BLEED AIR ................................................................................. SET FOR START • If APU-assisted start, check all 10TH STAGE switch/lights illuminated IN
OUT
IN
BLEED AIR NORM LOOP A LOOP B
14TH STAGE DUCT FAIL
OPEN
CLOSED L
DUCT MON
1-62
June 2012
DUCT FAIL CLOSED
ISOL
R
10TH STAGE DUCT FAIL
FAIL
CLOSED
OPEN
L
APU LCV
ISOL
R
OUT
IN
IN
OUT
OPEN
DUCT FAIL CLOSED
604_ORM_01_018
TEST
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
IGNITION (A or B) .......................................................................................... ARM • Select A or B to armed position and check ARM switch/light caption illuminates
L-ENG-R S T A R T
START
START
IGNITION S T A R T
ARM
A
ON ON
S T O P
STOP
STOP
S T O P
ARM
CONT
B
ON
604_ORM_01_041
6.
On airplanes 5301 to 5330 without Bombardier SB 604-21-002: 7.
Packs,.............................................................................................................. OFF • The simulator is in compliance with the above service bulletin. Do not select the packs off
8.
Engines .......................................................................................................START a) Thrust levers ..................................................................... SHUTOFF b) R ENG START switch ............................................... Press and hold • Hold the START switch until the START caption illuminates • Check that the selected ignition advisory message appears and applicable ON switch/light illuminates • Check N1 increasing • When N2 reaches 20% and ITT is below 120°C - Thrust lever IDLE
L-ENG-R S T A R T
START
IGNITION
START
S T A R T
STOP
S T O P
ARM ON
A ON
STOP
ARM
CONT
B
ON
IGNITION A 0.0
20.2 N1 85.0 TO
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
604_ORM_01_213
S T O P
1-63
June 2012
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
8.
Engines ........................................................................................START (Cont’d) c) Engine instruments................................................................. Monitor • ITT indicates 450°C to 600°C during starting (max 900°C) • Starter disengages and START light goes out, ignition switch/light goes out, and advisory message removed at approximately 55% N2 • N1 stabilizes above 22% • Oil pressure indicates normal (above 25 psi)
L-ENG-R S T A R T
START
IGNITION
START
S T A R T
STOP
S T O P
ARM ON
A ON
S T O P
STOP
ARM
CONT
B
ON
IGNITION A 0.0
26.9
Message removed N1 85.0 TO
0
458 ITT
0.0
63.4
0 0 15 0.0
FF (PPH) OIL PRESS OIL TEMP FAN VIB
- FUEL (LBS) - TOTAL
4890
1-64
June 2012
5000 2000
3500 82 115 1.2
16780 4890
604_ORM_01_214
N2
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
8.
Engines ........................................................................................ START (Cont’d) d) Fuel system check valve operation 1 ................................... VERIFY e) L and R BOOST PUMP switch/lights ........................................... Out • Check both boost pump INOP switch/light captions come on and the fuel caution messages appear f) L and R BOOST PUMP switch/lights ............................................ On • Check INOP captions go out and the fuel caution messages are removed L FUEL PUMP R FUEL PUMP L FUEL LO PRESS
FUEL BOOST PUMP
INOP
INOP
ON
ON
L
R
XFLOW
ON
OPEN
ON
L TO AUX
GRAVITY
R TO AUX
TAIL TANK TRANSFER
FAIL F FA
AUTO A AU IN INHIB
FAIL F FA
FAIL F FA
ON
MANUAL
ON
OPEN
PRI
MANUAL OVRD
SEC
DUMPS AT 0º FLAPS ONLY
604_ORM_01_042
DUMP
g) Left engine starting................................................................Resume h) Other engine ...........................................................................START • Limit first engine to 70% N2 during the second engine starting • Use similar procedures as for right engine • Check N2 idle indications are within 2% of each other
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
1-65
June 2012
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
FAILURE TO START 1.
Thrust lever.......................................................................................... SHUT OFF • Select the thrust lever of the starting engine to shut off
2.
IGNITION ......................................................................................................... OFF
3.
Dry motor ....................................................................................... ACCOMPLISH • Motor until ITT is reduced below 120°C (maximum 90 seconds)
AFTER ENGINE START CHECK 1.
GEN 1 and GEN 2 ............................................................................................. ON
APU GEN OFF/ RESET
GEN 2
OFF/ RESET ON
ON
FAIL
OFF/ RESET ON
FAIL AUTOXFER XFER
OFF
OFF
604_ORM_01_225
AC POWER GEN 1
On airplanes 5301 to 5320 without Bombardier SB 604-33-002: 2.
STBY INSTR circuit breaker (1P9) .......................................................... CHECK • Reset if necessary • Note that the simulator is in compliance with the above service bulletin. This check is not required
3.
AC and DC ELECTRICAL pages ............................................................. CHECK • Check voltage, frequency and load indications and the AC buses are outlined in green on the AC ELECTRICAL page • Check the TRUs are on-line with normal voltage and load indications show on the DC ELECTRICAL page • Check that the MAIN BUS TIE symbol indicates open DC ELECTRICAL
AC ELECTRICAL AC BUS 1
115 V 400 HZ
ADG
UTIL BUS 1
AC BUS 2
TRU 1
TRU 2
28 V 10 A
28 V 10 A
UTIL BUS 2
ESS TRU 2 28 V 21 A
ESS TRU 1 28 V 20 A
BUS 2 ESS BUS
116 V 400 HZ
EXT AC
BUS 1
ESS BUS
BUS 2
BATT BUS
TIE APU BATT DIR BUS
7 KVA 115 V 400 HZ
8 KVA 115 V 400 HZ
8 KVA 115 V 400 HZ
GEN 1
GEN
GEN 2
UTIL BUS 1
June 2012
MAIN BATT DIR BUS
UTIL BUS 2
APU
1-66
EMER BUS
EXT DC 28 V 19 A
APU BATT 28 V 0 A
MAIN BATT 28 V 0 A
604_ORM_01_043
BUS 1
AC ESS BUS
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
4.
APU GEN....................................................................................... AS REQUIRED
APU GEN OFF/ RESET
GEN 2
OFF/ RESET ON O
ON
FAIL
OFF/ RESET ON
FAIL AUTOXFER
OFF
OFF
604_ORM_01_215
AC POWER GEN 1
5.
APU................................................................................................ AS REQUIRED
6.
IGNITION .................................................................................................. DISARM • Check that the ARM caption in the switch goes out
L-ENG-R START
IGNITION S T A R T
START
ARM
A
ON ON
S T O P
7.
STOP
S T O P
STOP
ARM
CONT
B
ON
604_ORM_01_216
S T A R T
PACKs ............................................................................................................... ON • Check that the OFF captions go out in both PACK switch/lights AIR CONDITIONING CKPT NORM
STBY
PACK MAN
CABIN
L
R
FAIL
FAIL
OFF
OFF
NORM
STBY
MAN
RAM-AIR
CABIN TEMP
OPEN
CKPT HEAT COLD
HOT
OFF O
COLD
ON
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
HOT
604_ORM_01_217
CKPT TEMP
1-67
June 2012
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
8.
14TH stage valve check.................................................................... COMPLETE a) 14TH STAGE L switch/light ................................................. Press out • Check L CLOSED light on b) 14TH STAGE R switch/light ................................................ Press out • Check R CLOSED light on c) 14TH STAGE L and R switch/lights....................................... Press in • Check L and R CLOSED lights out
BLEED AIR
14TH STAGE
LOOP A LOOP B
TEST
DUCT FAIL
L
CLOSED
ISOL
R
10TH STAGE
DUCT MON
9.
DUCT FAIL
OPEN
CLOSED
DUCT FAIL
FAIL
DUCT FAIL
OPEN
CLOSED
OPEN
L
APU LCV
CLOSED
R
ISOL
605_ORM_01_198
NORM
Wing anti-ice check........................................................................... COMPLETE • Check the amber band on N2 gauge and that the engines’ ITT increases • Check advisory shown and green L HEAT and R HEAT lights illuminate on the ANTI-ICE panel. This may take several seconds to appear ANTI-ICE WING L HEAT R HEAT
NORM
ON
ON
L
R
DET WING
WSHLD/WIND OFF/ RESET
PROBES OFF/ RESET
TEST
LOW HI
L
R
458
458 85.O MCT
ITT
63.3
VIB
1-68
June 2012
63.3 N2
LOW
OFF O
HI
ON
L
OFF ON
R
R WING A/ICE L WING A/ICE MASTER CAUTION
Momentary Indications
VIB WING A/ICE ON
604_ORM_01_218
STBY OFF
TEST
COWL
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
10. Wing Anti-ice/Isolation Valve check 1 ........................................... COMPLETE a) 14TH STAGE ISOL switch .................................................... Press in • Check white OPEN caption comes on b) 14TH STAGE ISOL switch .................................................. Press out • Check OPEN caption goes out BLEED AIR NORM
14TH STAGE
LOOP A LOOP B
DUCT FAIL
CLOSED
L
DUCT MON
DUCT FAIL
OPEN
CLOSED
R
ISOL
10TH STAGE DUCT FAIL
FAIL
CLOSED
OPEN
L
APU LCV
DUCT FAIL
OPEN
CLOSED R
ISOL
604_ORM_01_219
TEST
11. Anti-ice cowl check 1 ..................................................................... COMPLETE a) ANTI-ICE COWL L and R switch/lights ................................. Press in • Check that the engines’ ITT increases • Check both COWL switch/lights illuminate green and advisory messages displayed. Note that the WING/COWL A/ICE ON advisory message is displayed when the wing and cowl anti-ice systems are selected b) ANTI-ICE COWL L and R switch/lights ............................... Press out • Check that both switch/lights go out and advisory messages out ANTI-ICE WING L HEAT R HEAT
ON
ON
L
R
DET WING
WSHLD/WIND OFF/ RESET
PROBES OFF/ RESET
TEST
LOW HI
L
R
458
458 85.O MCT
ITT
WING/COWL A/ICE ON
LOW
OFF O
OFF
HI
ON
ON
L
L COWL A/ICE R COWL A/ICE MASTER CAUTION
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
R
Momentary Indications
604_ORM_01_044
STBY OFF NORM
TEST
COWL
1-69
June 2012
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
12. Wing and cowl anti-ice ................................................................ AS REQUIRED • See AFM Limitations for wing and cowl anti-icing requirements 13. Flight controls .......................................................................................... CHECK a) FLIGHT CONTROLS synoptic page ....................................... Select • Operate ailerons and check for freedom of movement in each direction and that the ailerons return to neutral position when released • Operate elevators and check for full elevator freedom of movement in each direction and that the elevators return to the neutral position when released. Check that no ELEVATOR SPLIT caution message is shown • Operate the rudder pedals and check for full rudder freedom of movement in each direction. Check that the rudder returns to neutral position when released • Check that no related hydraulic messages are shown
PRI
STAT
HYD
ELEC
CAS
F/CTL
FLIGHT CONTROLS
FLAPS 20 AIL
AIL FLAPS MOTOR OVERHEAT
ELEVATOR SPLIT
RUDDER ELEV
No message shown
1-70
June 2012
ELEV
604_ORM_01_049
EICAS Control Panel
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
14. Ground spoilers check 1 ................................................................ COMPLETE a) DISARM ................................................................................... Select • Check no spoiler deployment or messages GND SPOILERS
ARM AUTO D DISARM
R ARMED
L ARMED EMER STOW
OFF
UNLK
UNLK
L
R
OFF
THRUST REVERSER
FLAPS 20 AIL
AIL
604_ORM_01_050
FLIGHT CONTROLS
b) ARM ........................................................................................ Select • FLIGHT CONTROLS page - check both ground spoilers fully deploy GND SPOILERS
ARM AUTO
FLIGHT CONTROLS
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
604_ORM_01_221
DISARM
1-71
June 2012
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
14. Ground spoilers check 1 ...................................................................... (Cont’d) c) AUTO ....................................................................................... Select • Check that both ground spoiler panels stow GND SPOILERS
ARM AUTO
FLIGHT CONTROLS
1-72
June 2012
604_ORM_01_222
DISARM
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
15. Flight spoilers check 1 ................................................................... COMPLETE a) Flight spoiler lever .........................................................Select full aft • FLIGHT CONTROLS page - check flight and ground spoilers fully deploy and the caution message is not shown FLIGHT CONTROLS
FLIGHT SPOILER
1/4 RETRACT
FLAPS 20 AIL
1/2
AIL
604_ORM_01_051
0
3/4
FLIGHT SPOILERS MAX
No caution message shown
b) Flight spoiler lever .................................................Select full forward • Check that the flight and ground spoilers stow
FLIGHT SPOILER 0
FLAPS 20 AIL
1/4 RETRACT
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
AIL
604_ORM_01_223
FLIGHT CONTROLS
1-73
June 2012
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
16. NOSE STEER ............................................................................................ ARMED a) Check that no STEERING INOP caution message is shown HORN NOSE STEER ARMED
LDG GEAR MUTED
OFF ANTI-SKID
TEST
ARMED
UP
DN
OFF
OVHT
1-74
June 2012
FAIL
604_ORM_01_074
DN LCK REL MLG BAY OVHT TEST
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
17. APR check ......................................................................................... COMPLETE • Select the ENG SPEED switches to ON • Select each TEST position and check for related indications: APR TEST 1 OK
ENGINE CONTROL ARM
TEST T 1
OFF
OFF
TE TEST 3
TEST 2
TEST
ON
OFF
APR
LH
OFF
RH
ENG SPEED
VIB
APR TEST 2 OK
ENGINE CONTROL ARM
TEST 1
OFF
OFF
TE TEST 3
T TEST 2
TEST
ON
OFF
APR
LH
OFF
RH
ENG SPEED
VIB
APR TEST 3 OK
ENGINE CONTROL TEST 1 OFF
T TEST 3
TE TEST 2
TEST
ON
OFF
APR
LH
OFF
RH
ENG SPEED
VIB
26.9
604_ORM_01_046
ARM OFF
26.9
APR
APR N1 90.0 TO
• Select ARM when checks are complete and all indications out
ARM A
TEST 1
OFF
OFF
TEST 3
TE TEST 2
APR
TEST OFF VIB
ON
LH
OFF ENG SPEED
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
RH
604_ORM_01_220
ENGINE CONTROL
1-75
June 2012
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
18. ADG AUTO DEPLOY CONTROL................................................................... UNIT a) ADG test switch...........................................................Select to UNIT • Check the TEST light illuminates for 2 seconds, then goes out LAMP
PWR TXFR OVERRIDE
ADG AUTO DEPLOY CONTROL
1-76
June 2012
604_ORM_01_047
TEST UNIT
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
TAXI CHECK 1.
Brakes ........................................................................................................CHECK a) Airplane ........................................................................................ Roll • Allow the airplane to roll and gently apply brakes • Check that no anti-skid or brake messages come on b) Brakes .......................................................................................Warm • Perform the following number of firm brake applications from 25 knots to 10 knots. Perform the prescribed number of brake applications during the last mile/kilometer of taxi prior to and not including the final stop or snub before takeoff. Do not drag the brakes. AIRPLANE WEIGHT
NUMBER OF BRAKE APPLICATIONS
Greater than 42,000 lb
5
36,000 lb to 42,000 lb
6
Less than 36,000 lb
7
NOTE 1. Use of symmetric braking is recommended, to ensure uniform brake heating. 2. Warming of the brakes will preclude the chance of water saturated brakes freezing at altitude and being locked for landing touchdown. 2.
FLAPS ................................................................................................................ 20 a) FLIGHT CONTROLS synoptic page ........................................ Select • Check EICAS indicates flaps at 20 on the primary page and the FLIGHT CONTROLS synoptic page - GEAR -
- FLAPS -
20
FLIGHT CONTROLS
STAB NU
- TRIM -
5.0 ND
AIL
LWD
RWD
RUDDER NL
FLAPS 20 NR
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
604_ORM_01_048
DN DN DN
1-77
June 2012
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
3.
Thrust reversers check 1 ................................................................ COMPLETE a) Thrust reverse levers..................................................................... Lift • Check the amber REV icon appears in the related N1 scale followed by a green REV icon b) Thrust reverse levers........................................................ Push down • Check the amber REV icon appears and goes out 27.5
27.6
REV MAX POWER
N1 90.3
MAX POWER
IDLE SHUT OFF
604_ORM_01_052
IDLE SHUT OFF
REV
1-78
June 2012
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
4.
Aileron and rudder trims ..................................................................... NEUTRAL
5.
Stabilizer trim ....................................................................... SET FOR TAKEOFF • Check both channels are engaged • Check trim is set for the takeoff CG - GEAR -
- FLAPS -
20
DN DN DN - TRIM -
5.0 ND
STAB TRIM CH 1
CH 2
ENGAGE
LWD
AIL
RWD
RUDDER NL
NR
MACH TRIM INOP ENGAGE/ DISENGAGE
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
604_ORM_01_224
STAB NU
1-79
June 2012
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
STABILIZER TRIM SETTING FOR TAKEOFF C.G. RANGE (% MAC)
TRIM SETTING
16.0 - 16.2
7.2
16.3 - 17.2
7.0
17.3 - 18.3
6.8
18.4 - 19.3
6.6
19.4 - 20.3
6.4
20.4 - 21.3
6.2
21.4 - 22.4
6.0
22.5 - 23.4
5.8
23.5 - 24.4
5.6
24.5 - 25.5
5.4
25.6 - 26.5
5.2
26.6 - 27.5
5.0
27.6 - 28.5
4.8
28.6 - 29.6
4.6
29.7 - 30.6
4.4
30.7 - 31.6
4.2
31.7 - 32.6
4.0
32.7 - 33.7
3.8
33.8 - 34.7
3.6
34.8 - 36.5
3.4
36.6 - 38.0
3.2
NOTE 1. Trim data from the FMS should be rounded down to the next lowest multiple of 0.2 trim units. 2. On airplanes NOT incorporating Service Bulletin 604-34-035: • Usage of trim data from the FMS is prohibited. Flight instruments.................................................................... CHECK AND SET • Check there are no abnormal annunciations on the EFIS, the slip-skid indicators are normal, and EFIS is set for departure
7.
Fuel balance ............................................................................................. CHECK • Check main tank fuel quantities are within 400 lb of each other 470 60 95 0.0
FF (PPH) OIL PRESS OIL TEMP FAN VIB
- FUEL (LBS) - TOTAL
4890
1-80
June 2012
5000 2000
470 60 95 0.0
16780 4890
604_ORM_01_228
6.
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
TAKEOFF CHECK 1.
Correct runway......................................................................................CONFIRM
2.
Ignition .......................................................................................... AS REQUIRED • IGNITION, CONT switch/light - Press in to turn ON, if required
S T A R T
START
START
IGNITION A/B
IGNITION S T A R T
ARM
A
ON ON
S T O P
STOP
STOP
S T O P
ARM
B
CONT
ON
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
604_ORM_01_117
L-ENG-R
1-81
June 2012
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
3.
Wing and cowl anti-ice ................................................................ AS REQUIRED NOTE 1. The wing anti-ice system must be selected ON, for final taxi prior to takeoff, if the OAT is 5°C (41°F) or below, unless Type II, III or IV anti-icing fluids have been applied. Single engine taxi operations are prohibited in these conditions. 2. L(R) WING A/ICE caution messages may be posted or L HEAT or R HEAT lights may go out during taxi but caution messages must be verified out and WING A/ICE ON or WING/COWL A/ICE ON advisory message and L HEAT and R HEAT lights must be verified on, prior to takeoff. If wing antiice is not required for takeoff it should be selected OFF just prior to takeoff. 3. To prevent wing contamination from reverse jet blast, operating the thrust reversers during taxi operations on wet and contaminated surfaces should be avoided. 4. The wing anti-ice system must be selected and confirmed ON for takeoff, when the OAT is 5°C (41°F) or below and: (a) Visible moisture in any form (such as clouds, fog or mist) is present below 400 feet AGL, or (b) The runway is wet or contaminated, or (c) In the presence of any precipitation (such as rain, snow, sleet or ice crystals). 5. If wing anti-ice is selected ON for takeoff, the cowl anti-ice must also be selected ON. 6. When Type II, III or IV anti-icing fluids have been applied, the wing anti-ice system must only be selected and confirmed ON just prior to thrust increase for takeoff. 7. The wing anti-ice system may be selected OFF only if it can be positively verified that all of the following conditions are met: (a) The runway to be used is not wet or contaminated, (b) There is no precipitation, and (c) There is no visible moisture in any form (such as clouds, fog, mist, rain, snow, sleet or ice crystals) below 400 feet AGL. 8. Refer to Chapter 6; SUPPLEMENTARY PROCEDURES – COLD WEATHER OPERATION – PHASE OF FLIGHT PROCEDURES.
1-82
June 2012
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
3.
Wing and cowl anti-ice ............................................................................(Cont’d) a) Wing anti-ice ...................................... Select WING switch to NORM WING A/ICE ON
ANTI-ICE WING
TEST
COWL
64.5 L HEAT R HEAT
NORM
ON
ON
L
R
DET WING
WSHLD/WIND OFF/ RESET
VIB
64.5 N2
VIB
PROBES OFF/ RESET
TEST
LOW HI
L
LOW
OFF O
HI
ON
R
OFF ON
L
R
604_ORM_01_118
STBY OFF
b) Cowl anti-ice............... Select COWL L and R switch/lights to turn on • If wing anti-ice is on - Check that the WING/COWL A/ICE ON advisory message is displayed NOTE 1. The engine cowl anti-ice system must be on when the OAT is 10°C (50°F) or below and visible moisture in any form is present (such as fog with visibility of one mile or less, rain, snow, sleet and ice crystals). 2. The engine cowl anti-ice system must also be on when the OAT is 10°C (50°F) or below when operating on runways, ramps, or taxiways where surface snow, ice, standing water or slush is present. COWL A/ICE ON
ANTI-ICE WING
If wings are on
L HEAT R HEAT
NORM
ON
ON
L
R
DET WING
WSHLD/WIND OFF/ RESET
PROBES OFF/ RESET
TEST
LOW HI
L
R
LOW
OFF O
HI
ON
L
OFF ON
R
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
WING/COWL A/ICE ON
604_ORM_01_119
STBY OFF
TEST
COWL
1-83
June 2012
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
4.
L and R WSHLD/WIND ....................................................................... HI OR LOW • Check the caution messages are removed Messages removed
ANTI-ICE WING L HEAT R HEAT
NORM
ON
ON
L
R
WING
WSHLD/WIND OFF/ RESET
PROBES OFF/ RESET
TEST
LOW HI
L
5.
R WSHLD HEAT R WINDOW HEAT L WSHLD HEAT L WINDOW HEAT
DET
LOW
OFF O
OFF
HI
ON
ON
R
L
R
604_ORM_01_120
STBY OFF
TEST
COWL
PROBES ............................................................................................................ ON a) L and R PROBES switches ............................................Select to ON • Check the caution messages are removed Messages removed
ANTI-ICE WING L HEAT R HEAT
NORM
ON
ON
L
R
WING
WSHLD/WIND OFF/ RESET
PROBES OFF/ RESET
TEST
LOW HI
L
6.
1-84
R PROBE HEAT OFF L PROBE HEAT OFF
DET
R
LOW
OFF
HI
ON O
L
OFF ON
R
604_ORM_01_121
STBY OFF
TEST
COWL
Cabin .........................................................................................................ADVISE • Not less than 1 minute prior to takeoff
June 2012
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
7.
Cockpit lighting ............................................................................ AS REQUIRED • Check EMER LTS switch selected to ARM
8.
External lights .............................................................................. AS REQUIRED • External lights and landing lights as required PASS
SIGNS
NO SMKG
EMER LTS
SEAT BELTS
O ON OFF AUTO
FDR EVENT
ON O OFF AUTO
IND LTS
MISC LTS BOARD
ON OFF ARM
OVHD
DOME
OFF
OFF
DIM
ON
ON
BRT B OFF
BRT
EXTERNAL LTS A/COLL WING-INSP BEACON OFF OFF OFF
OFF O ON
O ON
O ON
NOSE PLS OFF O S STDY
9.
O ON
RECOG TAXI LTS
RIGHT
OFF O ON
OFF
O ON
LANDING LTS LEFT
LOGO
PLS O OFF S STDY
OFF O ON
604_ORM_01_122
NAV
CAS.......................................................................................CHECK AND CLEAR • Check that the TO CONFIG OK advisory message is shown and no warning, caution or status messages are displayed • Check reverser advisory messages are displayed TO CONFIG OK L REV ARMED R REV ARMED 604_ORM_01_123
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
1-85
June 2012
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
10. Weather radar ................................................................................................... ON • Select weather radar (WX position) • Check weather radar mode indicators SEC
-1
NORM
+1
-2
+2
-3
+3
XFR
TILT
MAP WX TEST WX+T OFF TURB
TERR
BRG
STAB
WX
TFC NAV SOURCE
WX
RANGE
G+1
604_ORM_01_124
FORMAT
T+5.0
MFD
11. Transponder ................................................................................................... SET • Set ATC SEL to 1 if using flight director 1 • Set ATC SEL to 2 if using XFR mode on the FCP (flight director 2) STBY 2
AFCS SEL
RTU 2 INHIB
1-RTU-2
June 2012
ATC SEL
INHIBIT PUSH RTU 1 INHIB
1-86
2
1
FMS TUNE INHIB FMS TUNE
604_ORM_01_125
1
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
AFTER TAKEOFF CHECK 1.
LDG GEAR lever............................................................................................... UP • Check that the landing gear is retracted and all gear symbols indicate ‘UP’ HORN
- GEAR -
NOSE STEER ARMED
LDG G GEA GEAR
UP UP UP
MUTED OFF ANTI-SKID
TEST
UP
ARMED
DN
OFF
604_ORM_01_126
DN LCK REL MLG BAY OVHT TEST OVHT
FLAPS .................................................................................................................. 0 • Selection should be made at a safe altitude and airspeed • Check that the FLAPS indication displays 0 - GEAR -
FLAPS 0
0 STAB NU
20
- FLAPS -
30
30
45
45
- TRIM -
5.0
20 ND
LWD
AIL
RWD
RUDDER NL
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
0
UP UP UP
NR
604_ORM_01_127
2.
FAIL
1-87
June 2012
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
3.
Thrust reversers............................................................................................. OFF • Check advisory messages are removed Messages removed
GND SPOILERS
L REV ARMED R REV ARMED ARM AUTO DISARM
EMER STOW
OFF F
UNLK
UNLK
L
R
OFF F
THRUST REVERSER
CAS...................................................................................... CHECK AND CLEAR • Verify and analyze all messages, and clear (if any) • Monitor for messages during flight
APU
0.0
0.0
100
323
N1
EICAS Primary Page
5.
EICAS Status Page
604_ORM_01_129
4.
604_ORM_01_128
R ARMED
L ARMED
IGNITION ....................................................................................... AS REQUIRED NOTE 1. 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. 2. The engine cowl and wing anti-ice systems must be on when in icing conditions or when ice is indicated by the ice detection system.
6.
1-88
Wing and cowl anti-ice ................................................................ AS REQUIRED
June 2012
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
CLIMB CHECK 1.
Pressurization ...........................................................................................CHECK C ALT
1000
RATE
350
¨3
0.4
604_ORM_01_131
If the APU is supplying bleed air: 2.
Packs.............................................................. TRANSFER TO ENGINE BLEEDS NOTE 1. Bleed air extraction from the APU is not permitted above 15,000 feet. 2. On airplanes 5301 to 5630 NOT incorporating Service Bulletin 604-49-006 or 604-49-009: • Bleed air extraction from the APU is not permitted above 14,500 feet. Transfer to engine bleed as follows: a) b) c) d)
R - 10TH STAGE bleed ............................................. Open (Press in) 10 TH STAGE ISOL ............................................... Close (Press out) L - 10 TH STAGE bleed............................................. Open (Press in) APU LCV ................................................................ Close (Press out)
BLEED AIR NORM
14TH STAGE DUCT FAIL
OPEN
CLOSED L
DUCT MON
CLOSED ISOL
R
10TH STAGE DUCT FAIL
FAIL
OPEN
DUCT FAIL
CLOSED
OPEN
L
APU LCV
ISOL
R
C
D
B
A
CLOSED
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
DUCT FAIL
604_ORM_01_132
LOOP A LOOP B
TEST
1-89
June 2012
EXPANDED CHECKLIST OPERATIONS REFERENCE MANUAL
Climb thrust .................................................................................................... SET • FMS CDU - THRUST LIMIT page • N1 CLB displayed on the primary EICAS page
POS
BRT
THRUST LIMIT TO
TEXT DISPLAY
30% 4.0 CLB
90.8
2/4 APR
N1 90.8 CLB
95.5
VFTO
> CYOW
90.8 CRZ
39.1 / 39.1 / 45.2 --MODE-MCT
7747 /13700 FT
TGT
---.OAT
20°C
ENG BLEED
ENG BLEED
10TH/OFF
]
CYOW
97.2 --MODE-MCT
7747 /13700 FT ENG BLEED
N1 97.2 CRZ
VFTO
90.8 CRZ
APR
95.5 TGT
---.OAT
20°C
ENG BLEED
10TH/OFF 5/8 SM) Other SQ Squall DS Duststorm SS Sandstorm PO Dust/Sand Whirls VA Volcanic Ash FC Funnel Cloud + FC Tornado/Waterspout
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
APPENDIX-5 June 2012
APPENDIX OPERATIONS REFERENCE MANUAL
Aviation Routine Weather Report – METAR BKN008 OVC040 – The cloud layer at 800 feet is broken, covering from 5/8 to 7/8 of the observed sky. The next layer at 4000 feet is overcast covering, combined with the lower layer, 8/8 of the sky, as observed from the ground. Layers are reported based on the summation of the layer amounts as observed from the surface up. The layer amounts are reported in eighths of sky coverage (oktas) as follows: FEW – >0 to 2, SCT – 3 to 4, BKN – 5 to 7, OVC – 8. Only CB and TCU will be reported as cloud types in this area of the report. Where observed, other cloud types and their layer opacity's are reported in the remarks. Obscured sky is indicated by vertical visibility (VV) and is reported in hundreds of feet. In AWOS reports; cloud types are not identified, cloud layers are limited to 4 layers, and clear (CLR) will be reported when no layers exist below 10,000 feet. M05/M08 – Temperature is – 5°C, dew point is – 8°C. Temperature and dew point are reported to the nearest whole °C. Negative values will be preceded by the letter “M”. A2992 – The altimeter setting is 29.92 inches of mercury. The letter “A” prefixing the 4-digit number group indicates inches of mercury for station pressure. REFZRA – Freezing rain has been observed during the hour since the last report, but not at the time of the report. Recent weather since the last observation is reported, to include: freezing precipitation; moderate or heavy rain, snow, blowing snow, snow pellets, hail, or ice pellets; thunderstorm, sandstorm, or duststorm; volcanic ash; funnel cloud, tornado, and waterspout. WS RWY33 – Recent wind shear existed in the takeoff or landing path of Runway 33 below 1600 feet AGL. Recent wind shear information below 1600 feet AGL will be provided when reported by an aircraft on takeoff or landing. RMK SF5 SC3 – The lowest reported cloud layer type is stratus fractus, opaque over 5/8 of its coverage. The next layer type is stratocumulus, opaque over 3/8 of its coverage. Where observed, the cloud types and their opacities will be included in remarks. The remarks will include all elements augmented by human observers at AWOS sites. Funnel clouds, tornadoes, and waterspouts will be spelled out if “FC” or “+ FC” is in the present weather section. VIS 3/8 NW – Visibility is 3/8 statute mile to the northwest. Other supplementary remarks of operational significance may be included using standard abbreviations. SLP134 – The mean sea level pressure is 1013.4 hPa (mb). The mean sea level pressure, indicated in hectopascals, will always be the last field of the METAR report, prefixed with “SLP”.
APPENDIX-6 June 2012
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
APPENDIX OPERATIONS REFERENCE MANUAL
INTERNATIONAL AERODROME FORECAST – TAF International Aerodrome Forecast – TAF TAF CYXE 291045Z 291111 24010G25KT WS011/27050KT 3SM -SN BKN010 OVC040 TEMPO 1801 11/2SM SN BLSN BKN008 PROB30 2022 1/2SM SN VV005 FM0130Z 28010KT 5SM -SN BKN020 BECMG 0608 0000KT P6SM SKC RMK FCST BASED ON AUTO OBS NXT FCST BY 17Z TAF – Aerodrome Forecast in TAF Code This indicates the type of report. If the forecast is amended it will be indicated directly following the report type, i.e., “TAF AMD”. CYXE – Saskatoon, Saskatchewan As in the METAR, the issue day of the month and UTC time will be included in all reports. 291045Z – Report issued on the 29th day of the month, 1045 UTC As in the METAR, the issue day of the month and UTC time will be included in all reports. 291111 – Forecast covers the period from 1100Z on the 29th to 1100Z the following day. The forecast period contains the start day, UTC hour, and ending UTC hour. Within the forecast there may be further subdivisions by change groups which will include modified elements. 24010G25KT – Forecast surface wind is 240°T at 10 knots gusting to 25 knots. Wind is forecast in the TAF using criteria similar to that of the METAR. WSO11/27050K – There is a wind shear forecast to exist in the layer from the surface to 1100 feet AGL. The wind at that height is 270° True at 50 knots. Canada and the U.S. have adopted this format of forecasting low level non-convective wind shear. Low level wind shear forecasts shall be included whenever strong wind shear, which could adversely affect aircraft operation within 1500 feet AGL, can be adequately predicted. 3SM -SN – Forecast prevailing visibility is 3 statute miles in light snow. Prevailing visibility is forecast as per the METAR criteria. Visibilities greater than 6 SM are coded as “P6SM”. BKN010 OVC040 – Forecast cloud layers are broken at 1000 feet and overcast at 4000 feet. Cloud layers are forecast as per the METAR criteria. Only cumulonimbus (CB) cloud type will be identified in the forecast. It will be appended following the cloud layer height (BKN010CB).
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
APPENDIX-7 June 2012
APPENDIX OPERATIONS REFERENCE MANUAL
International Aerodrome Forecast – TAF TEMPO 1801 – The following weather elements are forecast to temporarily change between 1800 and 0100 UTC. There are a number of change group codes. Canada has adopted a unique format to delineate the hour grouping in the “FM” change group with the letter “Z” to avoid any confusion which may arise between hour and minute groupings. Elements identified after a change group code are those that are expected to change, while those not stated remain the same. The change groups are: FM0130Za change from a certain time in hours and minutes of the stated elements (0130Z). BECMG 0608a permanent but gradual change of the stated elements, occurring over the indicated period (0600 0800Z). TEMPO 1801a temporary fluctuation of the stated elements, occurring over the indicated period (1800 - 0100Z). PROB30 2022a probability (30% or 40% for PROB40) that a hazard to aviation will occur during the specified time. If a greater probability exists one of the other change groups will be used. 11/2SM -SN BLSN BKN008 – The prevailing visibility is forecast at 11/2 statute miles in light snow and moderate blowing snow with a broken cloud layer at 800 feet. PROB30 2022 – There is a 30% probability of the following events between 2000 and 2200Z. 11/2SM SN VV005 – The prevailing visibility is forecast at 1/2 statute mile in moderate snow which is the obscuring phenomena creating a vertical visibility of 500 feet. FM0130Z – A change of the following elements will occur beginning at 0130Z. 28010KT 5SM -SN BKN020 – The wind is forecast at 280° True at 10 knots with a prevailing visibility of 5 statute miles in light snow and a broken cloud layer at 2000 feet. BECMG 0608 – Between 0600 and 0800Z the following weather elements will gradually change to become as forecast. 0000KT P6SM SKC – The wind is forecast to be calm, the forecast visibility is greater than 6 SM (“P” for plus), and the sky will be clear (SKC). RMK FCST BASED ON AUTO OBS NXT FCST BY 17Z – The observation for this site is based primarily on AWOS sensor data. The next forecast for this site will be issued by 1700Z. This remark format is unique to Canadian TAFs. It brings to the attention of the users that the on-site observational data is AWOS based (this remark will still appear for sites where there is human augmentation of the observation) and Canada has staggered issue and update schedules for some TAFs.
APPENDIX-8 June 2012
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
APPENDIX OPERATIONS REFERENCE MANUAL
TEMPERATURE CONVERSION TABLE ISA -30°C
ISA -20°C
ISA -10°C
ISA +10°C
ISA +20°
°C
°F
°C
°F
°C
°F
°C
°F
°C
°F
°C
°F
°C
°F
0
-15.0
5.0
-5.0
23.0
5.0
41.0
15.0
59.0
25.0
77.0
35.0
95.0
45.0
113.0
1000
-17.0
1.4
-7.0
19.4
3.0
37.4
13.0
55.4
23.0
73.4
33.0
91.4
43.0
109.4
2000
-18.9
-2.1
-8.9
15.9
1.1
33.9
11.1
51.9
21.1
69.9
31.1
87.9
41.1
105.9
3000
-20.9
-5.7
-10.9
12.3
-0.9
30.3
9.1
48.3
19.1
66.3
29.1
84.3
39.1
102.3
4000
-22.9
-9.3
-12.9
8.7
-2.9
26.7
7.1
44.7
17.1
62.7
27.1
80.7
37.1
98.7
5000
-24.9
-12.8
-14.9
5.2
-4.9
23.2
5.1
41.2
15.1
59.2
25.1
77.2
35.1
95.2
6000
-26.9
-16.4
-16.9
1.6
-6.9
19.6
3.1
37.6
13.1
55.6
23.1
73.6
33.1
91.6
7000
-28.9
-20.0
-18.9
-2.0
-8.9
16.0
1.1
34.0
11.1
52.0
21.1
70.0
31.1
88.0
8000
-30.8
-23.5
-20.8
-5.5
-10.8
12.5
-0.8
30.5
9.2
48.5
19.2
66.5
29.2
84.5
9000
-32.8
-27.1
-22.8
-9.1
-12.8
8.9
-2.8
26.9
7.2
44.9
17.2
62.9
27.2
80.9
10000
-34.8
-30.7
-24.8
-12.7
-14.8
5.3
-4.8
23.3
5.2
41.3
15.2
59.3
25.2
77.3
11000
-36.8
-34.2
-26.8
-16.2
-16.8
1.8
-6.8
19.8
3.2
37.8
13.2
55.8
23.2
73.8
12000
-38.8
-37.8
-28.8
-19.8
-18.8
-1.8
-8.8
16.2
1.2
34.2
11.2
52.2
21.2
70.2
13000
-40.8
-41.4
-30.8
-23.4
-20.8
-5.4
-10.8
12.6
-0.8
30.6
9.2
48.6
19.2
66.6
14000
-42.7
-44.9
-32.7
-26.9
-22.7
-8.9
-12.7
9.1
-2.7
27.1
7.3
45.1
17.3
63.1
15000
-44.7
-48.5
-34.7
-30.5
-24.7
-12.5
-14.7
5.5
-4.7
23.5
5.3
41.5
15.3
59.5
16000
-46.7
-52.1
-36.7
-34.1
-26.7
-16.1
-16.7
1.9
-6.7
19.9
3.3
37.9
13.3
55.9
17000
-48.6
-55.6
-38.6
-37.6
-28.6
-19.6
-18.6
-1.6
-8.6
16.4
1.4
34.4
11.4
52.4
18000
-50.7
-59.2
-40.7
-41.2
-30.7
-23.2
-20.7
-5.2
-10.7
12.8
-0.7
30.8
9.3
48.8
19000
-52.7
-62.8
-42.7
-44.8
-32.7
-26.8
-22.7
-8.8
-12.7
9.2
-2.7
27.2
7.3
45.2
20000
-54.6
-66.3
-44.6
-48.3
-34.6
-30.3
-24.6
-12.3
-14.6
5.7
-4.6
23.7
5.4
41.7
21000
-56.6
-69.9
-46.6
-51.9
-36.6
-33.9
-26.6
-15.9
-16.6
2.1
-6.6
20.1
3.4
38.1
22000
-58.6
-73.5
-48.6
-55.5
-38.6
-37.5
-28.6
-19.5
-18.6
-1.5
-8.6
16.5
1.4
34.5
23000
-60.5
-77.0
-50.5
-59.0
-40.5
-41.0
-30.5
-23.0
-20.5
-5.0
-10.5
13.0
-0.5
31.0
24000
-62.5
-80.6
-52.5
-62.6
-42.5
-44.6
-32.5
-26.6
-22.5
-8.6
-12.5
9.4
-2.5
27.4
25000
-64.5
-84.2
-54.5
-66.2
-44.5
-48.2
-34.5
-30.2
-24.5
-12.2
-14.5
5.8
-4.5
23.8
26000
-66.5
-87.7
-56.5
-69.7
-46.5
-51.7
-36.5
-33.7
-26.5
-15.7
-16.5
2.3
-6.5
20.3
27000
-68.5
-91.3
-58.5
-73.3
-48.5
-55.3
-38.5
-37.3
-28.5
-19.3
-18.5
-1.3
-8.5
16.7
28000
-70.5
-94.9
-60.5
-76.9
-50.5
-58.9
-40.5
-40.9
-30.5
-22.9
-20.5
-4.9
-10.5
13.1
29000
-72.4
-98.4
-62.4
-80.4
-52.4
-62.4
-42.4
-44.4
-32.4
-26.4
-22.4
-8.4
-12.4
9.6
30000
-74.4 -102.0 -64.4
-84.0
-54.4
-66.0
-44.4
-48.0
-34.4
-30.0
-24.4
-12.0
-14.4
6.0
31000
-76.4 -105.6 -66.4
-87.6
-56.4
-69.6
-46.4
-51.6
-36.4
-33.6
-26.4
-15.6
-16.4
2.4
32000
-78.4 -109.1 -68.4
-91.1
-58.4
-73.1
-48.4
-55.1
-38.4
-37.1
-28.4
-19.1
-18.4
-1.1
33000
-80.4 -112.7 -70.4
-94.7
-60.4
-76.7
-50.4
-58.7
-40.4
-40.7
-30.4
-22.7
-20.4
-4.7
34000
-82.4 -116.3 -72.4
-98.3
-62.4
-80.3
-52.4
-62.3
-42.4
-44.3
-32.4
-26.3
-22.4
-8.3
35000
-84.3 -119.8 -74.3 -101.8 -64.3
-83.8
-54.3
-65.8
-44.3
-47.8
-34.3
-29.8
-24.3
-11.8
Altitude Feet
ISA
ISA +30°C
36000
-86.3 -123.4 -76.3 -105.4 -66.3
-87.4
-56.3
-69.4
-46.3
-51.4
-36.3
-33.4
-26.3
-15.4
37000
-86.5 -123.7 -76.5 -105.7 -66.5
-87.7
-56.5
-69.7
-46.5
-51.7
-36.5
-33.7
-26.5
-15.7
38000
-86.5 -123.7 -76.5 -105.7 -66.5
-87.7
-56.5
-69.7
-46.5
-51.7
-36.5
-33.7
-26.5
-15.7
39000
-86.5 -123.7 -76.5 -105.7 -66.5
-87.7
-56.5
-69.7
-46.5
-51.7
-36.5
-33.7
-26.5
-15.7
40000
-86.5 -123.7 -76.5 -105.7 -66.5
-87.7
-56.5
-69.7
-46.5
-51.7
-36.5
-33.7
-26.5
-15.7
41000
-86.5 -123.7 -76.5 -105.7 -66.5
-87.7
-56.5
-69.7
-46.5
-51.7
-36.5
-33.7
-26.5
-15.7
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
APPENDIX-9 June 2012
APPENDIX OPERATIONS REFERENCE MANUAL
CONVERSION FACTORS – TABLE MULTIPLY
BY
TO OBTAIN
Centimeter
0.3937
in
Centimeter2
0.155
in2
MULTIPLY
BY
TO OBTAIN
Km/hr
0.54 0.6214
knots mph
Knot
1.151 1.852
mph km/hr
kPa
0.145
psi
Liter
0.2642 0.22
USG Imperial gal
Centimeter3
0.061
in3
Cu ft3
0.0283
meter3
Ft
0.3048
meter
Ft2
0.0929
m2
Meter
3.281
ft
Gal, Imperial
1.2009 4.546
USG liter
Meter2
10.76
ft2
Meter3
35.3115
ft3
Gal, U.S.
3.7854 0.8327
liter Imperial gal Mile
5280 1.609 0.869
ft km nautical mile
Mph
1.609 0.869
km/hr knot
Nautical Mile
1.151 1.852
mile m
Pound (lb)
0.4536
kilogram
PSI
6.895
kPa
In
2.54
cm
In2
6.452
cm2
In3
16.387
cm3
Kilogram
2.205
lb
Kilometer
0.6214 0.54
mile nautical mile
APPENDIX-10 June 2012
FOR TRAINING PURPOSES ONLY Copyright © Bombardier Inc.
APPENDIX OPERATIONS REFERENCE MANUAL
DEFINITIONS GENERAL The following definitions are for terms commonly used throughout the manual. Items not commonly used will be defined in the respective sections where they apply.
AIRSPEEDS IAS CAS EAS TAS M MT V1 V1MBE V1MCG V2 VA VEF VFE VFTO VLE VLO VMO/MMO
VMCA
VMCG
VMCL VR VREF VS1G VSR
Indicated airspeed: Airspeed indicator reading corrected for instrument error. Values in this manual assume zero instrument error. Calibrated airspeed: Indicated airspeed corrected for static source position error. Equivalent airspeed: Calibrated airspeed corrected for compressibility. True airspeed: Equivalent airspeed corrected for density. Indicated Mach number: Machmeter reading corrected for instrument error. True Mach number: Machmeter reading corrected for both instrument and static source position errors. Takeoff decision speed (formerly designated as Critical engine failure recognition speed): The speed used as a reference at which, due to engine failure or other causes, the pilot may elect to stop or continue the takeoff. Maximum V1 for brake energy: The maximum speed on the ground from which a stop can be accomplished within the energy capabilities of the brakes. Minimum V1 limited by control on the ground:The takeoff decision speed following an engine failure at VMCG. V1 may not be less than V1MCG. Takeoff safety speed: Target climb speed to be attained at or before a height of 35 feet above the runway during a continued takeoff, following an engine failure. Design maneuvering speed: The maximum speed at which application of full available aileron, rudder or elevator will not overstress the airplane. Critical engine failure speed: The speed at which, if the critical engine fails, the engine failure is recognized at V1. Maximum flap extended speed: is the highest speed permissible with the wing flaps in a prescribed extended position. Final takeoff climb speed: The speed attained at the end of the flight path acceleration segment during a continued takeoff following an engine failure, and is the climb speed scheduled for the final takeoff climb. Maximum landing gear extended speed: The maximum speed at which the airplane can be safely flown with the landing gear extended. Maximum landing gear operating speed: The maximum speed at which the landing gear can be safely extended or retracted. Maximum Operating Limit Speed/Mach Number: The maximum operating limit speed (airspeed or Mach number) is the speed that may not be deliberately exceeded in any regime of flight (climb, cruise, or descent) unless a higher speed is authorized for flight test or pilot training operations. Minimum control speed, air: Minimum flight speed at which the airplane is controllable with a maximum of 5° bank, when the critical engine suddenly becomes inoperative, with the remaining engine at maximum takeoff thrust. Minimum control speed, ground: Minimum speed on the ground at which control can be maintained and the takeoff continued using aerodynamic controls alone, when the critical engine suddenly becomes inoperative, with the remaining engine at maximum takeoff thrust. Minimum control speed during landing approach: Minimum flight speed at which the airplane is controllable with a maximum of 5° bank, when the critical engine suddenly becomes inoperative, with the remaining engine at maximum takeoff power. Rotation speed: Speed at which rotation is initiated during takeoff. Approach speed: The landing reference speed at a height of 50 feet above the runway threshold in the normal landing configuration Stalling speed and pusher activation speed. Reference Stall Speed: The reference stall speed upon which all performance data is based.
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TEMPERATURE ISA
International Standard Atmospheric conditions.
OAT
Outside air temperature - The free air temperature, obtained either from in-flight temperature indications or ground meteorological sources.
SAT
Static air temperature (In-flight, SAT = OAT).
TAT
Total air temperature – Static air temperature plus adiabatic compression (ram) rise.
DISTANCES
Takeoff Distance
The takeoff distance is the longer of: The distance from the start of the takeoff roll to the point where the airplane attains a height of 35 feet above the takeoff surface, with a failure of the critical engine at VEF. 115% of the distance from the start of the takeoff roll to the point at which the airplane attains a height of 35 feet above the takeoff surface, with all engines operating.
Takeoff Run
The takeoff run is the longer of: The distance from the start of the takeoff roll to the mid point between lift-off and the point at which the airplane attains a height of 35 feet above the takeoff surface, with a failure of the critical engine at VEF. 115% of the distance from the start of the takeoff roll to the mid point between lift-off and the point at which the airplane attains a height of 35 feet above the takeoffsurface, with all engines operating.
Accelerate – Stop Distance
The accelerate, stop distance is the longer of (a.) and (b.) as defined below: The sum of the distances necessary to: Accelerate the airplane from a standing start to VEF with all engines operating; Accelerate the airplane from VEF to V1 assuming the critical engine fails at VEF; and Come to a full stop from the point reached at the end of the acceleration period prescribed in paragraph (a.) 2 above, assuming that the pilot does not apply any means of retarding the airplane until that point is reached; plus A distance equivalent to 2 seconds at constant V1. The sum of the distances necessary to: Accelerate the airplane from a standing start to V1 with all engines operating; Come to a full stop at the end of the period prescribed in paragraph (b.) 1 above, assuming that the pilot does not apply any means of retarding the airplane until that point is reached; plus A distance equivalent to 2 seconds at constant V1.
Clearway
An area beyond the runway, not less than 500 feet wide, centrally located about the extended centerline of the runway, and under the control of the airport authorities. The clearway is expressed in terms of a clearway plane, extending from the end of the runway with an upward slope not exceeding 1.25% above which no object nor any terrain protrudes. However, threshold lights may protrude above the plane if their height above the end of the runway is 26 inches or less and if they are located to each side of the runway.
Stopway
An area beyond the takeoff runway at least as wide as the runway and centered upon the extended centerline of the runway, able to support the airplane during an aborted takeoff without causing structural damage to the airplane, and designated by the airport authorities for use in decelerating the airplane during an aborted takeoff.
Actual Landing Distance
Actual landing distance is the distance from a 50 feet height at VREF with the flaps in the normal landing configuration, to a full stop on a smooth, dry, level, hard-surfaced runway and ISA temperature.
Landing Field Length
The performance charts in this chapter include factors for operational rules which require the use of 60% of the available runway in determining landing field length requirements. The required landing field length on a dry runway is the actual landing distance divided by 0.6. The landing field length required under wet runway conditions is equal to 115% of the dry runway landing field length.
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TAKEOFF PATH Takeoff Path
The takeoff path begins from a standing start and ends at 1500 feet above the takeoff surface or at the point where transition from takeoff to en route configuration is completed, whichever is higher.
Takeoff Flight Path
The takeoff flight path begins at the end of the takeoff distance and at a height of 35 feet above the takeoff surface, and ends at 1500 feet above the takeoff surface, or at the point where transition from takeoff to en route configuration is completed, whichever is higher. This is also known as the Gross Takeoff Flight Path.
Net Takeoff Flight Path
The net takeoff flight path is the gross takeoff flight path diminished by 0.8% climb gradient capability (or equivalent reduction in acceleration along that part of the takeoff flight path at which the airplane is accelerated in level flight). The net takeoff flight path must clear all obstacles in the takeoff area by at least 35 feet vertically.
CLIMB GRADIENT Climb Gradient
The ratio of the change in height, during a portion of a climb, to the horizontal distance traversed in the same time interval.
Gross Gradient
Climb gradient expressed as a percentage ratio, obtained using the following formula: (Change in height ÷ Horizontal distance traveled) x 100. The gradients shown on the charts are based on true (not pressure) rates of climb.
Net Gradient
The gross gradient reduced by the required margins.
First Segment
The first segment starts from the 35-foot height and extends to the point where the landing gear is fully retracted, at a constant V2 speed and flaps in the takeoff position.
Second Segment
The second segment starts at the point where the landing gear is fully retracted up to at least 400 feet above the runway, flown at V2 speed and flaps in the takeoff position.
Acceleration Segment
The acceleration segment is the part of the takeoff flight path that begins at the end of the second segment and extends horizontally over the distance required to retract flaps to zero, and accelerate to the final takeoff climb speed.
Final Segment
The final segment starts from the end of the acceleration segment and extends to the end of the takeoff flight path, flown at the final segment climb speed, flaps up.
MISCELLANEOUS APR
Automatic Performance Reserve: In the event of an engine failure during takeoff, the APR system, if operating, will increase the thrust rating of the remaining engine. The APR rating must be set manually in the event of a single-engine go-around.
Center of Gravity (C.G.)
The point at which the airplane would balance if suspended.The C.G. distance from the reference datum is found by dividing the total moment by the total weight of the airplane.
GW
Gross weight: The maximum weight to which the airplane is certificated.
MLW
Maximum landing weight: The maximum airplane weight approved for the landing touchdown at a maximum descent velocity of 10 feet per second.
MTOW
Maximum takeoff weight: The maximum airplane weight approved for the start of takeoff or for landing at a reduced descent velocity not to exceed 6 feet per second.
MZFW
Maximum zero fuel weight.
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FLIGHT PLAN EQUIPMENT SUFFIXES DEFINITION EQUIPMENT: The Challenger aircraft is equipped with the following components: Communication: • •
2 or 3 VHF transceivers 2 HF transceivers
Navigation and Approach Aids: • • • • • • • •
2 or 3 IRS 2 VHF navigation systems 2 DME receivers 2 ADF receivers 2 GPS sensors 2 or 3 FMS 2 ILS receivers 2 VOR receivers
SSR Equipment: • •
2 ATC transponders Mode A, C and S
The communication (COM), navigation (NAV), approach aid and SSR equipment on board and its serviceability must be inserted in the flight plan by adding the appropriate suffixes. The first suffixes will denote the COM, NAV, and approach aid equipment, followed by an oblique stroke, and another suffix to denote the SSR equipment. Each State of Registry develops its own rules regarding suffix codes but do base their rules, to some extent, upon the ICAO recommended codes. It is the operator’s responsibility to determine which codes to utilize in what airspace they intend to operate. Differences exist between States (countries) especially with regard to advanced navigation capability; therefore the operator must utilize that State’s suffix codes when operating totally within that State’s airspace. International flight operations use the ICAO suffixes. For navigation purpose, a reference to the appropriate State’s document must be made to fully comply with the Flight Planning requirement. The following tables are given as examples only. References: Transport Canada Aeronautical Information Manual (RAC section) FAA Aeronautical Information Manual (Chapter 5)
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EQUIPMENT SUFFIX TABLES CANADA & ICAO A
(Not allocated)
M
(Not allocated)
B
(Not allocated)
O
VOR
C
LORAN C
P
(Not allocated)
D
DME
Q
(Not allocated)
E
(Not allocated)
R
RNP type certification
F
ADF
T
TACAN
G
GNSS
U
UHF
H
HF RTF
V
VHF
I
INS
W
RVSM certification
J
Data Link
X
MNPS certification
K
MLS
Y
CMNPS certification
L
ILS
Z
Other equipment carried
UNITED STATES AREA NAVIGATION (RNAV) /Y
LORAN, VOR/DME, OR INS with no transponder
/C
LORAN, VOR/DME, OR INS, transponder with no Mode C
/I
LORAN, VOR/DME, OR INS transponder with Mode C
ADVANCED RNAV WITH TRANSPONDER AND WITH MODE C (If an aircraft is unable to operate with a transponder and/or Mode C, it will revert to the appropriate code listed above under Area Navigation.) /E
Flight Management System (FMS) with DME/DME and IRU position updating
/F
FMS with DME/DME position updating
/G
Global Navigation Satellite System (GNSS), including GPS or Wide Area Augmentation System (WAAS), with en route and terminal capability
/R
Required Navigational Performance (RNP). The aircraft meets the RNP type prescribed for the route segment(s), route(s), and/or area concerned.
Reduced Vertical Separation Minimum (RVSM). Prior to conducting RVSM operations within the U.S., the operator must obtain authorization from the FAA or from the responsible authority, as appropriate. /J
/E with RVSM
/K
/F with RVSM
/L
/G with RVSM
/Q
/R with RVSM
/W
RVSM
Example: Canadian Domestic FP
International ICAO FP
United States Domestic FP
CL604/SDGRWY/S
CL60/M-SDGRIHXW/S
CL604/L
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