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At the established downwind:
(1) Circling MDA .................................................... Maintain
(2) Flaps.............................................................30 degrees
(3) Airspeed ...............................................Flaps 30° speed
+ 10 KIAS
When abeam the runway threshold:
(4) Start .....................................................Time for 15 to 30
seconds, plus or
minus wind
correction.
After the desired timing has elapsed, start the turn towards the base leg:
(5) Descent ............................................................... Initiate
NOTE
The autopilot, if used, should be disconnected no later than 1,000 AGL.
Approaching 400 feet, start turn towards final, and when landing is assured:
(6) Flaps.............................................................45 degrees
(7) Airspeed ............................................. VREF + 1/2 GUST Maximum correction is
+10 KIAS.
CAUTION
PFD negative barometric altitude is indicated by a yellow NEG flag
within the barometric altitude window.
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) Landing gear lever.................................................... Set to DN, prior to turning towards
the base leg.
Turning base:
(6) Descent ............................................................... Initiate
(7) Flaps.............................................................30 degrees
SUPPLEMENTARY PROCEDURES
CAA (UK) Registry Operation
Vol. 1 06−23−4
REV 66, Feb 01/07
▼
CL−604 Operating Manual
PSP 604−6
5. NORMAL PROCEDURES (CONT'D)
(8) Airspeed ...............................................Flaps 30° speed
+ 10 KIAS
(9) Rate of descent ..............................Approximately –700
fpm
NOTE
The autopilot, if used, should be disconnected no later than 1,000
feet AGL.
At 500 to 700 feet altitude, initiate turn to final:
(10) Flaps.............................................................45 degrees
(11) Airspeed ............................................ VREF + 1/2 GUST Maximum correction is +10
KIAS.
(12) Before landing check...................................... Complete
At 50 feet AGL:
(13) Thrust levers.........................................................Select to IDLE.
6. ABNORMAL PROCEDURES
The abnormal procedures in Chapter 5 are applicable.
7. SUPPLEMENTARY PROCEDURES
The supplementary procedures in Chapter 6 are applicable, except as modified by the following:
A. Automatic Flight Control System
INSTRUMENT APPROACHES
Autopilot procedures for instrument approaches are essentially the same. The autopilot must
not be used, however, at altitudes below 1,000 feet AGL except when on an ILS approach,
where the minimum allowable altitude for the operation of the autopilot is 80 feet AGL.
During approaches, descent is initiated by using the vertical speed mode, by selecting the
VS switch which will automatically maintain the referenced vertical speed. When desired, the
reference vertical speed can be changed by using the Speed/Pitch wheel adjacent to the VS
switch.
The preselect altitude is set to the procedure turn altitude (if applicable), when tracking
outbound from the fix. Maintaining headings and turns are accomplished in the heading mode
by pressing the HDG switch, and rotating the heading select knob to the desired heading(s). If
so desired, the half bank mode may be used in conjunction with the heading select mode.
When cleared for the approach on the inbound leg to the fix, or when on the localizer
intercept heading for a straight-in approach, select the approach mode by pressing the APPR
switch. The flight control computer then arms for glideslope capture if on a front course
approach, captures the glideslope (as annunciated by green GS on the PFDs) and maintains
flight on the glide path. The half bank mode (if previously selected) will be automatically
cleared in this instance.
At this point, the preselect altitude should be set to the missed approach altitude, to prepare
for a possible overshoot.
SUPPLEMENTARY PROCEDURES
CAA (UK) Registry Operation
Vol. 1 06−23−5
REV 66, Feb 01/07
　
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