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(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 4B
Category II Operations
07−04B−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.
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 4B
Category II Operations
07−04B−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
　
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