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(9) Thrust levers ..............................................................................................SHUT OFF
(10) Fuel system crossflow valve operation
(last flight of the day) ........................................................................................ Check
(11) Passenger signs .................................................................................................. OFF
(12) ANTI-ICE, WING switch....................................................................................... OFF
(13) ANTI-ICE COWL switch/lights ............................................................................. OFF
(14) WSHLD/WIND L and R switches......................................................................... OFF
NORMAL PROCEDURES
Consolidated Checklists
04−20−10
REV 75, Feb 17/09
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. CONSOLIDATED CHECKLISTS (CONT'D)
V. Shutdown Check (Cont’d)
(15) BEACON switch (if installed) ............................................................................... OFF
(16) NOSE STEER switch........................................................................................... OFF
W. Securing Check
(1) Parking brake............................................................................................ As required
(2) IRS selectors ....................................................................................................... OFF
(3) THRUST REVERSER, L and R switches ............................................................ OFF
(4) External lights ...................................................................................................... OFF
(5) EMER LTS switch................................................................................................ OFF
(6) Hydraulic pump switches ..................................................................................... OFF
(7) APU GEN switch..................................................................................... OFF/RESET
If external power is in use:
(7) External AC.............................................................................................................Off
(8) APU .............................................................................................................Shutdown
(9) L and R PACK switch/lights ................................................................................. OFF
(10) 10TH STAGE ISOL switch/light ................................................................... Press out
(11) 14TH STAGE, L and R switch/lights.............................................................CLOSED
(12) BATT MASTER switch......................................................................................... OFF
(13) MISC LTS switches ............................................................................................. OFF
(14) Oil master chip detector indicators
(last flight of the day) ........................................................................................ Check
NORMAL PROCEDURES
Consolidated Checklists
04−20−11
REV 75, Feb 17/09
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
NORMAL PROCEDURES
Consolidated Checklists
04−20−12
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
1. SEVERE TURBULENCE PENETRATION
A. Autopilot
The autopilot should be disconnected.
B. Airspeed
Turbulence penetration speed is 280 KIAS or 0.75 MI, whichever is lower.
Severe turbulence may cause large and rapid variations in airspeed. Do not chase airspeed.
C. Attitude
Maintain wings level with desired pitch attitude. Use the PFD attitude indicator as the primary
instrument. In extreme windshear, large attitude changes may occur. Do not use sudden or
large control inputs.
D. Stabilizer
Maintain control of the airplane with elevators. After establishing the trim setting for
penetration speed, avoid using the stabilizer trim for controlling attitude.
E. Altitude
The penetration altitude should be an altitude which provides adequate maneuvering
margins. Large altitude variations are possible in severe turbulence. Sacrifice altitude to
maintain desired attitude and airspeed. Refer to Chapter 6; PERFORMANCE – GENERAL –
Flight Capabilities – Maneuvering Capabilities.
F. Thrust
Make initial thrust setting for target airspeed. Change thrust only in case of extreme airspeed
changes.
G. Thunderstorms
Continuous engine ignition must be used during the following:
• Flight through moderate or heavier intensity rain;
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庞巴迪挑战者604飞机飞行手册CL604 Airplane Flight Manual 1(122)
