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limited by climb requirements is 21,800 kg (48,061 lb).
Example: ANTI-ICE OFF
Associated Conditions:
Temperature = 27°C
Airport pressure altitude = 4,000 ft
Wing and cowl anti-ice = Off
10th stage bleeds = Closed
As shown in the example (Figure 06−24−14, Anti-ice Off), the maximum landing weight
limited by climb requirements is 23,000 kg (50,706 lb).
SUPPLEMENTARY PROCEDURES
Operation with Systems Inoperative
Vol. 1 06−24−21
REV 71, Oct 31/07
CL−604 Operating Manual
PSP 604−6
8. PERFORMANCE (CONT'D)
DFM0708_013
SUPPLEMENTARY PROCEDURES
Operation with Systems Inoperative
Vol. 1 06−24−22
REV 71, Oct 31/07
Landing Weight Limited by Climb Requirements
Figure 06−24−14
CL−604 Operating Manual
PSP 604−6
1. GENERAL
These supplementary procedures must be used when conducting approaches above
3.5 degrees, but below 4.5 degrees.
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
Manual.
The effect of these supplementary procedures on the basic Operating Manual is given below.
2. INTRODUCTION
The general information in Chapter 1 is applicable.
3. OPERATING LIMITATIONS
The operating limitations in Chapter 2 are applicable, except as modified by the following:
A. Operating Limitations
(1) APPROACHES
On airplanes NOT incorporating Service Bulletin 604–34–055:
Operations with a glidepath angle exceeding the maximum shown in area A of
Figure 06−25−1 are prohibited.
On airplanes incorporating Service Bulletin 604–34–055:
Operations with a glidepath angle exceeding the maximum shown in area B of
Figure 06−25−1 are prohibited.
B. Systems Limitations
(1) AUTOMATIC FLIGHT CONTROL SYSTEM
The minimum autopilot use height for precision approaches (ILS) with a glidepath angle
that exceeds 3.5 degrees is 160 feet AGL.
SUPPLEMENTARY PROCEDURES
Approaches below 4.5 Degrees
Vol. 1 06−25−1
REV 75, Feb 17/09
CL−604 Operating Manual
PSP 604−6
3. OPERATING LIMITATIONS (CONT'D)
DFM0711_001
SUPPLEMENTARY PROCEDURES
Approaches below 4.5 Degrees
Vol. 1 06−25−2
REV 75, Feb 17/09
Approach Glidepath Angle Operating Limit
Figure 06−25−1
CL−604 Operating Manual
PSP 604−6
4. EMERGENCY PROCEDURES
The emergency procedures in Chapter 3 are applicable.
5. NORMAL PROCEDURES
The normal procedures in Chapter 4 are applicable, except as modified by the following;
A. Before Start Check
On airplanes incorporating Service Bulletin 604–34–055:
(1) GPWS, STEEP APPROACH
switch/light .......................................................Press out Check ON light out.
B. 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.
For operations in area B of Figure 06−25−1:
(5) GPWS, STEEP APPROACH
switch/light .........................................................Press in Check ON light on.
SUPPLEMENTARY PROCEDURES
Approaches below 4.5 Degrees
Vol. 1 06−25−3
REV 75, Feb 17/09
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CL−604 Operating Manual
　
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