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(58) IRS reversionary selectors........................................................................ As required
(59) FMS 3 selector (if installed) ...................................................................... As required
(60) LANDING GEAR MANUAL RELEASE handle ................................................Stowed
(61) ADG handle .....................................................................................................Stowed
(62) ADG AUTO DEPLOY CONTROL switch...........................................................LAMP
E. Before Start Check
(1) Gravity crossflow check ............................................................................... Complete
(2) Windshield/window heat test ....................................................................... Complete
(3) Wing overheat detection system test........................................................... Complete
(4) Pressurization controls .......................................................................................... Set
(5) Altimeters............................................................................................................... Set
(6) EFIS..................................................................................................Set for departure
(7) CAS .................................................................................................................. Check
(8) Brakes and anti-skid system check ............................................................. Complete
(9) FMS ....................................................................................................................... Set
(10) FMS messages................................................................................................. Check
(11) Radios/Navaids.................................................................................Set for departure
(12) Take-off data.......................................................................................................... Set
(13) Take-off briefing........................................................................................... Complete
F. Start Check
(1) Passenger door ..................................................................................... Check closed
(2) Fuel quantity and balance................................................................................. Check
(3) BEACON switch (if installed) ................................................................................. ON
(4) L and R BOOST PUMP switch/lights..................................................................... ON
(5) BLEED AIR switch/lights........................................................................... Set for start
NORMAL PROCEDURES
Consolidated Checklists
04−20−4
REV 75, Feb 17/09
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. CONSOLIDATED CHECKLISTS (CONT'D)
F. Start Check (Cont’d)
(6) IGNITION, A (B) switch/light ................................................................................ARM
On airplanes 5301 to 5330 NOT incorporating SB 604–21–002:
(7) L and R PACK switch/lights ................................................................................. OFF
(8) Engines............................................................................................................START
G. APU Assisted Engine Start Procedure
With the APU operating:
(1) APU LCV switch/light............................................................................. Check OPEN
(2) L (R) ENG START switch/light........................................................................... Press
When N2 reaches 20% RPM and ITT is below 120°C:
(3) Left or right thrust lever.....................................................................Advance to IDLE
(4) Engine instruments ..........................................................................................Monitor
(5) Fuel system check valve operation (first flight of the
day).................................................................................................................... Verify
(6) L and R BOOST PUMP switch/lights..................................................................... ON
If the other engine is to be started using APU bleed air:
(7) Thrust lever (of operating engine)........................................................ Check at IDLE
(8) 10th stage bleed air pressure ........................................................................... Check
(9) L (R) ENG START switch/light........................................................................... Press
When N2 reaches 20% RPM and ITT is below 120°C:
(10) Thrust lever (of starting engine)........................................................Advance to IDLE
　
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