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FD 1 or 2 Flight director, on applicable side is inoperative. FD 1 (2) FAIL status
message displayed on EICAS.
ACTION
Continue approach, if the following is accomplished above
500 feet AGL:
(1) Autopilot...............................Disengage
(2) AFCS SEL 1 (2).......................... Select to operative AFCS
channel.
(3) FDs ...........................................Engage
(4) Autopilot....................................Engage
(5) Approach ................................Continue to Category II minima.
If below 500 feet AGL, on a stabilized approach:
(1) Autopilot...............................Disengage
(2) Manual control .........................Resume
(3) Approach ................................Continue to Category I minima, or
initiate go-around.
If below 200 feet AGL and non-visual:
(1) Go-around ..................................Initiate
SUPPLEMENTARY PROCEDURES
Category II Operation
Vol. 1 06−10A−8
REV 66, Feb 01/07
▼
CL−604 Operating Manual
PSP 604−6
6. ABNORMAL PROCEDURES (CONT'D)
C. System Failures (Cont’d)
SYSTEM INDICATION
AFCS PITCH
TRIM
Autopilot pitch trim failure; AP PITCH TRIM caution message displayed
on EICAS.
ACTION
During coupled approach:
If above 200 feet AGL, on a stabilized approach:
(1) Autopilot...............................Disengage Retrim, then re-engage.
If caution message goes out:
(2) Approach ................................Continue
If caution message persists:
(2) Manual control .........................Resume
(3) Approach ................................Continue to Category I minima.
If below 200 feet AGL and non-visual:
(1) Go-around ..................................Initiate
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 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 Stab
Trim switch.
If unable to disconnect autopilot, expect higher than normal control feel
force loads during landing.
SUPPLEMENTARY PROCEDURES
Category II Operation
Vol. 1 06−10A−9
REV 66, Feb 01/07
▼
CL−604 Operating Manual
PSP 604−6
6. ABNORMAL PROCEDURES (CONT'D)
C. System Failures (Cont’d)
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
SYSTEM INDICATION
HYDRAULICS Any hydraulic system(s) failure(s) annunciated as caution messages
displayed on EICAS; Refer to 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.
END
SUPPLEMENTARY PROCEDURES
Category II Operation
Vol. 1 06−10A−10
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
7. PERFORMANCE
The performance data in Chapter 6 of the Airplane Flight Manual 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
　
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