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Above 14,000 feet 265 1.5
NORMAL PROCEDURES
Approach and Landing
Vol. 1 04−08−2
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
1. APPROACH AND LANDING (CONT'D)
D. Precision (ILS/PAR) Approach
Precision approaches utilizing the autopilot and/or the flight director are essentially the same.
Approaching the fix (or beacon), when performing a full approach (with procedure
turn), or coming from a hold:
NOTE
When performing an ILS autopilot-coupled approach, ensure that both
flight directors are displayed.
(1) Airspeed ...............................................Flaps 20° speed
+ 20 KIAS
Fix outbound:
(2) Flaps.............................................................20 degrees
For straight-in approach (radar vectored):
(1) Flaps.............................................................20 degrees
(2) Airspeed ...............................................Flaps 20° speed
+ 20 KIAS
NOTE
When performing a straight-in approach, assume the initial approach
configuration (as in 1 and 2 above), at a distance of 12 miles away from
the airport.
Cleared for the approach; Fix inbound (for a full approach), or when on the localizer
intercept heading (for a straight-in approach):
(3) FCP mode ............................................................APPR
(4) Mode annunciations ..............................................Verify
• LOC 1 (2) and GS armed – white indications on both PFDs.
• LOC 1 (2) – green indications on both PFDs.
When 1 dot below the glideslope:
(5) LDG GEAR lever ...................................................... Set to DN.
(6) Flaps.............................................................30 degrees
At glideslope capture (indicated by green GS annunciation on both PFDs):
(7) Flaps.............................................................45 degrees
(8) Airspeed ................................................VREF + 10 KIAS
(9) Before landing check...................................... Complete
(10) Preselect ALT........................................................... Set to missed approach altitude.
At 1,500 feet AGL:
(11) Airspeed ....................................................VREF + WIND Wind correction is half steady
state plus all gust. Maximum
correction is + 20 KIAS.
NORMAL PROCEDURES
Approach and Landing
Vol. 1 04−08−3
REV 66, Feb 01/07
▼
CL−604 Operating Manual
PSP 604−6
1. APPROACH AND LANDING (CONT'D)
D. Precision (ILS/PAR) Approach (Cont’d)
At the final approach fix (FAF):
(12) Fix name, altitude and flags .............................Recheck correct fix name, at correct
altitude and no flags in view.
At decision height (DH) or decision altitude (DA) and landing is feasible:
(13) Autopilot (if used) ......................................... Disconnect at no less than 80 feet AGL.
CAUTION
PFD negative barometric altitude is indicated by a yellow NEG flag
within the barometric altitude window.
NORMAL PROCEDURES
Approach and Landing
Vol. 1 04−08−4
REV 66, Feb 01/07
▼
CL−604 Operating Manual
PSP 604−6
1. APPROACH AND LANDING (CONT'D)
D. Precision (ILS/PAR) Approach (Cont’d)
NORMAL PROCEDURES
Approach and Landing
Vol. 1 04−08−5
REV 66, Feb 01/07
Precision (ILS/PAR) Approach
Figure 04−08−1
CL−604 Operating Manual
PSP 604−6
1. APPROACH AND LANDING (CONT'D)
E. Non-Precision Approach
When approaching the fix (or beacon):
(1) Airspeed .................................................Flaps 0° speed
+ 30 KIAS
When at fix outbound or when abeam the approach fix for straight-in approach (radar
vectored):
(2) Flaps.............................................................20 degrees
(3) Airspeed ...............................................Flaps 20° speed
+ 20 KIAS
When tracking procedure turn altitude:
(4) Preselect altitude ...................................................... Set to the final approach fix (FAF)
altitude. Verify that ALTS
white indication is on (armed).
When established inbound:
(5) FCP mode ...............................................................FLC
(6) FLC........................................................ Set as required
(7) Thrust levers.........................................................Adjust to maintain the desired rate of
descent.
At approximately 3 miles before FAF:
(8) LDG GEAR lever ...................................................... Set to DN.
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庞巴迪挑战者604操作手册 Operating Manual 1(99)
