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Figure 04−08−3
CL−604 Operating Manual
PSP 604−6
1. APPROACH AND LANDING (CONT'D)
G. Standard Visual Approach
Enter the downwind leg according to the prescribed regulatory procedures.
(1) Downwind altitude ..........................................1,500 feet
(2) Flaps.............................................................20 degrees
(3) Airspeed ...............................................Flaps 20° speed
+ 20 KIAS
(4) Thrust .......................................................... As required to maintain the downwind
airspeed.
(5) LDG GEAR lever ...................................................... Set to DN, prior to turning towards
the base leg.
Turning base:
(6) Descent ............................................................... Initiate
(7) Flaps.............................................................30 degrees
(8) Airspeed ...............................................Flaps 30° speed
+ 10 KIAS
(9) Rate of descent ..............................Approximately –700
fpm
At 500 to 700 feet altitude, initiate turn to final:
(10) Flaps.............................................................45 degrees
NOTE
The autopilot, if used, should be disconnected no later than 320 feet
AGL.
(11) Airspeed ....................................................VREF + WIND Wind correction is half steady
state plus all gust. Maximum
correction is + 20 KIAS.
(12) Before landing check...................................... Complete
At 50 feet AGL:
(13) Thrust levers.........................................................Select to IDLE.
NORMAL PROCEDURES
Approach and Landing
Vol. 1 04−08−11
REV 66, Feb 01/07
▼
CL−604 Operating Manual
PSP 604−6
1. APPROACH AND LANDING (CONT'D)
G. Standard Visual Approach (Cont’d)
NORMAL PROCEDURES
Approach and Landing
Vol. 1 04−08−12
REV 66, Feb 01/07
Standard Visual Approach
Figure 04−08−4
CL−604 Operating Manual
PSP 604−6
1. APPROACH AND LANDING (CONT'D)
H. Before Landing Check
(1) IGNITION, CONT switch/light...................... As required
NOTE
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.
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:
(2) ANTI-ICE, WING switch .......................................Select as required.
(3) ANTI-ICE, COWL L and R
switch/lights ..........................................................Select as required.
If wing anti-ice is selected ON and WING L HEAT or R HEAT light goes out or
WING A/ICE ON or WING/COWL A/ICE ON advisory message goes out:
(4) Thrust ............................................................... Increase until the following come on:
• WING A/ICE ON or
WING/COWL A/ICE ON
advisory message.
• WING L HEAT and R HEAT
lights.
If WING A/ICE ON or WING/COWL A/ICE ON advisory message remains out or
WING L HEAT or R HEAT light remains out:
(5) Leave icing conditions.
(6) Cabin ................................................................... Advise not less than five minutes prior
to landing.
(7) PASS SIGNS, NO SMKG switch..........................Select to ON.
(8) PASS SIGNS, SEAT BLTS switch .......................Select to ON.
(9) LDG GEAR lever ...................................................... Set to DN. Check that three green
DN indications are displayed,
indicating that the landing gear
is down and locked.
NORMAL PROCEDURES
Approach and Landing
Vol. 1 04−08−13
REV 68, Apr 16/07
▼
CL−604 Operating Manual
PSP 604−6
1. APPROACH AND LANDING (CONT'D)
H. Before Landing Check (Cont’d)
(10) Brake and anti-skid system ..................................Check
(a) ANTI-SKID, ARMED switch..........................Check selected to armed.
(b) ANTI-SKID, TEST switch.............................. Select to TEST momentarily, and
check the following:
• A/SKID IN TEST advisory
message on.
After approximately 3 seconds
check:
• A/SKID IN TEST advisory
message out.
NOTE
Anti-skid system is inoperative if the A/SKID IN TEST
advisory message does not come on during test.
Anti-skid system is inoperative if A/SKID INBD (OUTBD)
　
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