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DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
6. ABNORMAL PROCEDURES (CONT'D)
C. System Failures: (Cont’d)
SYSTEM INDICATION
AUTOPILOT
DISCONNECT
Autopilot fails to disengage when intentionally disconnected.
ACTION
Autopilot fails to disconnect using AP/SP DISC switch on control wheel
during approach to landing:
(1) Autopilot.............................. Disconnect using AP ENG switch on
FCP, or AP DISC switch
on FCP, or TOGA
switch, or AP/SP DISC
switch on other control
wheel.
(2) Airplane .........................................Trim manually using stabilizer
trim switch.
If unable to disconnect autopilot, expect higher than normal control feel
force loads during landing.
SYSTEM INDICATION
ILS LOCALIZER
or GLIDESLOPE
ILS deviation error is greater than Category II “window”. Flashing
localizer or glideslope scale and pointer.
ACTION
Failure during approach:
If above 200 feet AGL, on a stabilized approach:
(1) Approach ................................Continue to Category I minima, or
initiate go-around.
If below 200 feet AGL and non-visual:
(1) Go-around ..................................Initiate
SUPPLEMENT 4
Category II Operations
07−04−01−9
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
6. ABNORMAL PROCEDURES (CONT'D)
C. System Failures: (Cont’d)
SYSTEM INDICATION
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.
7. PERFORMANCE
The performance data in Chapter 6 are applicable.
SUPPLEMENT 4
Category II Operations
07−04−01−10
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
GENERAL 07−04A−01−1
INTRODUCTION 07−04A−01−1
LIMITATIONS 07−04A−01−2
EMERGENCY PROCEDURES 07−04A−01−3
Autopilot Failure 07−04A−01−3
NORMAL PROCEDURES 07−04A−01−4
Prior to Approach 07−04A−01−4
Before Landing 07−04A−01−4
ABNORMAL PROCEDURES 07−04A−01−5
Single Engine Approach and Landing 07−04A−01−5
Engine Failure During Final Approach 07−04A−01−5
System Failures 07−04A−01−6
PERFORMANCE 07−04A−01−12
Maximum Landing Weight Limited By Climb Requirements – Approach Flaps
20°/Landing Flaps 45° 07−04A−01−12
LIST OF ILLUSTRATIONS
Figure 07−04A−1 Landing Weight Limited by Climb Requirements −
Approach Flaps 20°/Landing Flaps 45° 07−04A−01−13
SUPPLEMENT 4A
Category II Operations
07−04A−00−1
REV 66, Feb 01/07
07−04A−00−1
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
TABLE OF CONTENTS
Page
TABLE OF CONTENTS
SUPPLEMENT 4A
Category II Operations
07−04A−00−2
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
NOTE
This Airplane Flight Manual Supplement is only applicable to
airplanes on the German Registry.
NOTE
This Airplane Flight Manual Supplement does not constitute
operational approval to conduct Category II operations. Such
authorization must be obtained by the operator from the
appropriate authorities.
1. GENERAL
The CL 600−2B16 (CL–604) airplane has been shown to meet the airworthiness requirements for
Category II Operations contained in Appendix 1 of AC 120−29 and JAR AWO, Subpart 2.
　
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