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ALT/HDG/IAS/PIT/ROL/LOC/GS annunciations on PFDs.
ACTION
Failure during approach:
(1) Go-around ..................................Initiate
(2) Applicable procedure..........Accomplish Refer to Chapter 5;
ABNORMAL
PROCEDURES –
INSTRUMENTS
SYSTEM.
SUPPLEMENT 4B
Category II Operations
07−04B−01−7
REV 75, Feb 17/09
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
6. ABNORMAL PROCEDURES (CONT'D)
C. System Failures: (Cont’d)
SYSTEM INDICATION
ADC 1 or 2 Erratic PFD data or ADC FAIL annunciation, and ALT/IAS annunciation
on PFDs.
ACTION
First failure during approach (of the two required units):
If above 500 feet AGL, on a stabilized approach:
(1) ADC............................................ Select 1 or 2.
(2) Approach ................................Continue to Category I minima, or
initiate go-around.
If below 500 feet AGL and non-visual:
Failure of cross-side ADC:
(1) Approach ................................Continue to Category I minima, or
initiate go-around.
Failure of on-side ADC:
(1) Go-around ..................................Initiate
SUPPLEMENT 4B
Category II Operations
07−04B−01−8
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
FD 1 or 2 Flight director, on applicable side is inoperative. FD 1 (2) FAIL 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
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
SUPPLEMENT 4B
Category II Operations
07−04B−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
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 4B
Category II Operations
07−04B−01−10
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
　
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