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PSP 604−6
5. NORMAL PROCEDURES (CONT'D)
B. Precision (ILS/PAR) Approach (Cont’d)
When 1.5 dots below the glideslope:
(6) LDG GEAR lever ...................................................... Set to DN.
(7) Flaps.............................................................30 degrees
When 1 dot below the glideslope:
(8) Flaps.............................................................45 degrees
(9) Airspeed ................................................................. VREF
NOTE
1. The airplane should be fully configured for landing and slowed
to VREF prior to glideslope intercept.
2. Operations in icing conditions may result in the N2 being
displayed in the cautionary (amber) range (below 78% N2 ). In
this condition, the wing and cowl anti-ice systems should be
monitored. If an abnormal condition occurs, it may not be
possible to complete the approach when the associated
procedure is followed.
(10) Before landing check...................................... Complete
(11) Preselect ALT........................................................... Set to missed approach altitude.
At 1,500 feet AGL:
(12) Airspeed ....................................................VREF + WIND Wind correction is half steady
state plus all gust. Maximum
correction is + 20 KIAS.
At the final approach fix (FAF):
(13) 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:
(14) Autopilot (if used) ......................................... Disconnect at no less than 160 feet AGL.
CAUTION
PFD negative barometric altitude is indicated by a yellow NEG flag
within the barometric altitude window.
SUPPLEMENTARY PROCEDURES
Approaches below 4.5 Degrees
Vol. 1 06−25−4
REV 75, Feb 17/09
▼
CL−604 Operating Manual
PSP 604−6
5. NORMAL PROCEDURES (CONT'D)
B. Precision (ILS/PAR) Approach (Cont’d)
SUPPLEMENTARY PROCEDURES
Approaches below 4.5 Degrees
Vol. 1 06−25−5
REV 75, Feb 17/09
Precision (ILS/PAR) Approaches below 4.5 Degrees
Figure 06−25−2
CL−604 Operating Manual
PSP 604−6
5. NORMAL PROCEDURES (CONT'D)
C. In Range Check
For operations in area B of Figure 06−25−1:
(1) GPWS, STEEP APPROACH
switch/light .........................................................Press in Check ON light on.
D. Before Landing Check
NOTE
1. For approaches at angles above 4.0 degrees, the airplane should be
fully configured for landing and slowed to VREF prior to glideslope
intercept.
2. Intermittent operation at idle when wing anti-ice and/or cowl anti-ice is
ON is acceptable during final approach provided no associated EICAS
caution messages are annunciated.
E. Go-Around
For operations in area B of Figure 06−25−1:
(1) GPWS, STEEP APPROACH
switch/light .......................................................Press out Check ON light out.
F. After Landing Check
On airplanes incorporating Service Bulletin 604–34–055:
(1) GPWS, STEEP APPROACH
switch/light .......................................................Press out Check ON light out.
6. ABNORMAL PROCEDURES
The abnormal procedures in Chapter 5 are applicable, except as modified by the following:
A. Flaps Failure
The following applies, in addition to the existing flap failure procedure:
If flaps fail at 0 degrees, divert to a suitable landing field with a glidepath angle of 3.5 degrees
or less.
END
7. SUPPLEMENTARY PROCEDURES
The supplementary procedures in Chapter 6 are applicable.
8. PERFORMANCE
The performance data in Chapter 6 of the Airplane Flight Manual are applicable.
SUPPLEMENTARY PROCEDURES
Approaches below 4.5 Degrees
Vol. 1 06−25−6
REV 75, Feb 17/09
CL−604 Operating Manual
PSP 604−6
NOTE
These supplementary procedures are only applicable to airplanes
incorporating Service Bulletin 604−34−055.
These supplementary procedures are NOT applicable to FAA
registered airplanes.
These supplementary procedures do not constitute approval to
conduct Steep Approach operations.
1. GENERAL
These supplementary procedures must be used when conducting steep approach landings from
4.5 degrees to 5.5 degrees, inclusive.
These data complement or supersede data contained in the basic Operating Manual. These
supplementary procedures must, therefore, be used in conjunction with the basic Operating
　
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