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ACTION
Single channel failure:
(1) Approach ................................Continue
Dual channel failure
(STAB TRIM caution message on: autopilot may disengage):
(1) Go-around ..................................Initiate
Dual channel failure during final approach (in stabilized trim condition):
(1) Approach ................................Continue to Category I minima.
SUPPLEMENT 4A
Category II Operations
07−04A−01−6
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
RADIO
ALTIMETER
False radio altimeter height on PFDs, and RA annunciation on PFDs.
ACTION
Failure (of 2nd radio altimeter) 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
IRS Erratic PFD data or ATT annunciation, and HDG/ROL/PIT annunciation
on PFDs.
ACTION
First failure during the approach (AP will disconnect):
If above 500 feet AGL, on a stabilized approach:
(1) Manual control .........................Resume
(2) IRS source.................................. Select an operative IRS. (if IRS
3 is installed, AP will be
available).
(3) Approach ................................Continue to Category I minima, if
only one IRS available.
If below 500 feet AGL and non-visual:
(1) Manual control .........................Resume
(2) Go-around ..................................Initiate
SYSTEM INDICATION
EFIS Comparator EFIS COMP INOP (EFIS comparator failure) caution message or EFIS
COMP MON caution message displayed on EICAS and any of the
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 4A
Category II Operations
07−04A−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 4A
Category II Operations
07−04A−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
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庞巴迪挑战者604飞机飞行手册CL604 Airplane Flight Manual 2(75)
