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on PFDs (OFF flag may flash
at end of test).
(6) Decision height......................................................... Set on both PFDs.
(7) MDA ......................................................................... Set as a barometric DH, in case
RA fails.
(8) Runway Course........................................................ Set on both PFDs, or armed
(cyan) by FMS.
(9) EFIS .....................................................................Check that no comparator flags are
displayed.
(10) CAS......................................................................Check that the following messages
are not displayed:
• AFCS MSGS FAIL warning
message,
• AP PITCH TRIM, EFIS
COMP INOP and EFIS
COMP MON caution
messages,
• FD 1 and 2 FAIL status
messages.
(11) Stabilizer and elevator position ............................Check valid on F/CTL synoptic page.
(12) Approach mode ....................................................... Arm
B. Before Landing:
(1) Autopilot ........................................................Disengage at an altitude not less than
80 feet AGL.
SUPPLEMENT 4A
Category II Operations
07−04A−01−4
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
6. ABNORMAL PROCEDURES
The abnormal procedures in Chapter 5 are applicable, except as modified by the following:
A. Single Engine Approach and Landing
(1) Approach .......................................................... Conduct under Category I operations.
B. Engine Failure During Final Approach
Continue approach if the following can be accomplished above 800 feet AGL:
(1) Autopilot ....................................................... Disconnect
(2) Operating engine.............................................. Increase thrust as required.
(3) FLIGHT SPOILER lever ..................................... Ensure retracted.
(4) FLAPS ..................................................................Select to 20° for landing.
(5) Airspeed ........................................................... Increase to VREF + 14 KIAS.
(6) Airplane ............................................................... Retrim
(7) Autopilot ....................................................... Re-engage
(8) Actual landing distance .................................... Increase by a factor of 1.55 (55%), for a
landing without the use of
reverse thrust.
(9) GPWS/FLAP OVRD switch
(if installed) ...........................................................Select to OVRD (to mute flap aural
warning).
At glideslope intercept:
(10) Airplane ............................................................... Retrim directionally as required.
If above 800 feet AGL and the above procedure can not be accomplished:
(11) Approach .......................................................... Conduct under Category I operations.
If below 800 feet AGL and non-visual:
(12) Go-Around........................................................... Initiate
After landing or during go-around at a safe altitude:
(13) Engine shutdown procedure........................ Accomplish If applicable, refer to
Chapter 5; ABNORMAL
PROCEDURES – POWER
PLANT – In-Flight Engine
Failure/Shutdown procedure.
SUPPLEMENT 4A
Category II Operations
07−04A−01−5
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
6. ABNORMAL PROCEDURES (CONT'D)
C. System Failures:
SYSTEM INDICATION
VHF NAV 1 or 2 ILS receiver, on applicable side, is inoperative.
ACTION
First failure during approach (of the two required units):
If above 500 feet AGL, on a stabilized approach:
(1) NAV SOURCE............................ Select X-SIDE.
(2) Approach ................................Continue to Category I minima, or
initiate go-around.
If below 500 feet AGL and non-visual:
Failure of cross-side NAV:
(1) Approach ................................Continue to Category I minima, or
initiate go-around.
Failure of on-side NAV:
(1) Go-around ..................................Initiate
SYSTEM INDICATION
PFD 1 or 2 Primary flight display, on applicable side, goes blank.
ACTION
Failure during approach:
(1) Display reversionary panel
selector switch ............................ Select to PFD.
Applicable MFD defaults
to primary flight display.
SYSTEM INDICATION
STAB CH 1 or 2 Horizontal stabilizer trim, on applicable side, is inoperative.
STAB CH 1 (2) INOP status message, displayed on EICAS.
　
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