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HYDRAULICS Any hydraulic system(s) failure(s) annunciated as caution messages
displayed on EICAS (See Chapter 5; ABNORMAL PROCEDURES –
HYDRAULIC POWER).
ACTION
Failure during approach:
If above 200 feet AGL, on a stabilized approach:
(1) Applicable procedure..........Accomplish Refer to Chapter 5;
ABNORMAL
PROCEDURES –
HYDRAULIC POWER.
(2) Approach ................................Continue to Category I minima, or
initiate go-around.
If below 200 feet AGL and non-visual:
(1) Go-around ..................................Initiate
SYSTEM INDICATION
MAIN
GENERATOR
Generator failure; GEN 1 (2) OFF caution message displayed on EICAS
ACTION
NOTE
AP will disconnect if AFCS 2 is active.
YD 1 or YD 2 may disengage.
(1) Approach ................................Continue to Category I minima, or
initiate go-around.
SUPPLEMENT 4B
Category II Operations
07−04B−01−11
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
7. PERFORMANCE
The performance data in Chapter 6 are applicable, except as modified by the following:
A. Maximum Landing Weight Limited By Climb Requirements – Approach Flaps
20°/Landing Flaps 45°
The maximum landing weight limited by climb requirements for varying conditions of airport
pressure altitude and temperature for the flaps 20° approach climb configuration and a
subsequent landing flaps 45° configuration, are given in Figure 07−04B−1. The chart
incorporates all applicable anti-icing and 10th stage bleeds combinations.
NOTE
If ice accumulation is suspected on unprotected surfaces, then reduce
the maximum landing weight values derived from Figure 07−04B−1 by
800 kg (1,764 lb).
Example: ANTI-ICE ON
Associated Conditions:
Temperature = −8°C
Airport pressure altitude = 4,000 ft
Cowl anti-ice = On
10th stage bleeds = Closed
As shown in the example Figure 07−04B−1, Anti-ice On), the maximum landing weight limited
by climb requirements is 24,100 kg (53,131 lb). The landing weight in this case is greater than
the maximum approved landing weight (Refer to Chapter 2; LIMITATIONS – STRUCTURAL
WEIGHT) and is not considered limiting.
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 07−04B−1, Anti-ice Off), the maximum landing weight limited
by climb requirements is 23,700 kg (52,250 lb). The landing weight in this case is greater than
the maximum approved landing weight (Refer to Chapter 2; LIMITATIONS – STRUCTURAL
WEIGHT) and is not considered limiting.
SUPPLEMENT 4B
Category II Operations
07−04B−01−12
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
DFM0704B_001 ldg_watlim_405_ha_Cll.uni
SUPPLEMENT 4B
Category II Operations
07−04B−01−13
REV 66, Feb 01/07
Landing Weight Limited by Climb Requirements − Approach Flaps 20°/Landing Flaps 45°
Figure 07−04B−1
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
SUPPLEMENT 4B
Category II Operations
07−04B−01−14
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
GENERAL 07−05−01−1
INTRODUCTION 07−05−01−1
LIMITATIONS 07−05−01−1
EMERGENCY PROCEDURES 07−05−01−1
NORMAL PROCEDURES 07−05−01−1
High Speed Flight 07−05−01−1
Intentional Stalls 07−05−01−2
Gross Climb Performance 07−05−01−12
ABNORMAL PROCEDURES 07−05−01−16
PERFORMANCE 07−05−01−16
LIST OF ILLUSTRATIONS
Figure 07−05−1 Stick Shaker Speed (KIAS) − Flaps 0°, Landing Gear Up 07−05−01−4
Figure 07−05−2 Stick Shaker Speed (KIAS) − Flaps 20°, Landing Gear Up 07−05−01−5
Figure 07−05−3 Stick Shaker Speed (KIAS) − Flaps 30°, Landing Gear Up 07−05−01−6
Figure 07−05−4 Stick Shaker Speed (KIAS) − Flaps 45°, Landing Gear
Down 07−05−01−7
Figure 07−05−5 Stick Pusher Speed (KIAS) − Flaps 0°, Landing Gear Up 07−05−01−8
　
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