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(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.
(5) GPWS, STEEP APPROACH
switch/light .........................................................Press in Check ON light on.
When 1.5 dots below the glideslope:
(6) LDG GEAR lever ...................................................... Set to DN.
(7) Flaps.............................................................30 degrees
SUPPLEMENTARY PROCEDURES
Steep Approaches up to 5.5 Degrees
Vol. 1 06−26−4
REV 70, Jun 08/07
▼
CL−604 Operating Manual
PSP 604−6
5. NORMAL PROCEDURES (CONT'D)
B. Precision (ILS/PAR) Approach (Cont’d)
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
Steep Approaches up to 5.5 Degrees
Vol. 1 06−26−5
REV 70, Jun 08/07
▼
CL−604 Operating Manual
PSP 604−6
5. NORMAL PROCEDURES (CONT'D)
B. Precision (ILS/PAR) Approach (Cont’d)
SUPPLEMENTARY PROCEDURES
Steep Approaches up to 5.5 Degrees
Vol. 1 06−26−6
REV 70, Jun 08/07
Precision (ILS/PAR) Approaches up to 5.5 Degrees
Figure 06−26−1
CL−604 Operating Manual
PSP 604−6
5. NORMAL PROCEDURES (CONT'D)
C. In Range Check
(1) GPWS, STEEP APPROACH
switch/light .........................................................Press in Check ON light on.
D. Before Landing Check
NOTE
The airplane should be fully configured for landing and slowed to VREF prior
to glideslope intercept.
E. Go-Around
(1) GPWS, STEEP APPROACH
switch/light .......................................................Press out Check ON light out.
F. After Landing Check
(1) GPWS, STEEP APPROACH
switch/light .......................................................Press out Check ON light out.
SUPPLEMENTARY PROCEDURES
Steep Approaches up to 5.5 Degrees
Vol. 1 06−26−7
REV 70, Jun 08/07
CL−604 Operating Manual
PSP 604−6
6. ABNORMAL PROCEDURES
The abnormal procedures in Chapter 5 are applicable, except as modified by the following:
Discontinue steep approach landing and divert to the nearest suitable airport if any procedure
necessitates:
• an approach speed greater than VREF,
• a landing with flaps other than 45 degrees or
• an increase in actual landing distance by a factor greater than 1.50 (50%).
• a landing with any of the systems inoperative as listed in the system limitations of this
supplement.
A. Engine Failure During Approach
(1) Operating engine.............................................. Increase thrust as required.
(2) FLIGHT SPOILER lever .......................................Select to RETRACT.
Check EICAS indicates
spoilers retracted.
(3) FLAPS ..................................................................Select to 20°.
(4) Airspeed ........................................................... Increase to VREF (Flaps 45°) + 14 KIAS.
　
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