曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

(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
　
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：龐巴迪挑戰(zhàn)者604飛機飛行手冊CL604 Airplane Flight Manual 2(79)