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Yes
(1) EICAS Primary Display Failure
or EICAS Secondary Display
Failure Procedure .........................................ACCOMPLISH
(See Page ABNORM 15–2)
− END −
No
Primary flight display (PFD) is affected:
Yes
(1) Primary Flight Display Failure
Procedure .....................................................ACCOMPLISH
(See Page ABNORM 12–2)
− END −
No
Multifunction display (MFD) is affected:
(1) No further action required.
END
ABNORM 2-7
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15
AIR-CONDITIONING AND
PRESSURIZATION
ABNORM 2-8
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15
AIR-CONDITIONING AND
PRESSURIZATION
THIS PAGE INTENTIONALLY LEFT BLANK
CONTENTS PAGE
• AP TRIM IS LWD (RWD, ND, NU) ...........................ABNORM 3−2
• AP PITCH TRIM .......................................................ABNORM 3−3
• YAW DAMPER .........................................................ABNORM 3−4
• Single Flight Director Failed [FD 1 (2) FAIL
Status Msg] ...............................................................ABNORM 3−5
NOTE
Autopilot disconnect warnings are indicated by “Cavalry
Charge” aural and flashing red AP message on the primary
flight display.
ABNORM 3-1
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15
AUTOMATIC FLIGHT
CONTROL SYSTEM
AP TRIM IS LWD (RWD) (ND) (NU)
AP TRIM IS LWD (RWD) (ND) (NU)
(1) Autopilot operation ......................................................MONITOR
Retrim as required.
NOTE
Anticipate out of trim situation when disconnecting or
changing autopilot.
Caution message persists:
Yes
(2) Autopilot........................................................DISCONNECT
(3) AFCS SEL 1 (2)......................................................SELECT
operative channel.
(4) Autopilot................................................................ ENGAGE
and monitor operation. Retrim as required.
Caution message persists:
Yes
(5) Autopilot ............................................... DISCONNECT
Assume manual control.
− END −
No
(2) No further action required.
END
ABNORM 3-2
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15
AUTOMATIC FLIGHT
CONTROL SYSTEM
AP PITCH TRIM
AP PITCH TRIM
Pilot advisory that autopilot pitch trim has not been able to keep
up with trim change.
NOTE
Anticipate elevator out of trim situation when disconnecting
the autopilot.
(1) Autopilot ...............................................................DISCONNECT
Retrim as required.
(2) AFCS SEL 1 (2)..............................................................SELECT
operative channel.
(3) FDs and autopilot ......................................................... ENGAGE
and monitor operation. Retrim as required.
AP PITCH TRIM caution message persists:
Yes
(4) Autopilot........................................................DISCONNECT
Assume manual control.
− END −
No
(4) No further action required.
END
ABNORM 3-3
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15
AUTOMATIC FLIGHT
CONTROL SYSTEM
YAW DAMPER
YAW DAMPER
(1) YD1 and YD2 ............................................................... ENGAGE
YAW DAMPER caution message persists:
Yes
(2) YAW DAMPER.............................................DISCONNECT
(3) FLAPS .........................................................AS REQUIRED
Land with flaps at 20°, commensurate with the
controllability of the airplane.
No
Landing with FLAPS at 20 degrees:
Yes
Prior to landing:
(2) GPWS/FLAP OVRD
(if installed) ................................................................ OVRD
(3) Approach speed ...................................................VREF + 14
minimum.
(4) Actual landing distance...........................................Increase
as applicable by factor given below:
WITHOUT THRUST
REVERSERS
WITH THRUST
REVERSERS
1.55 (55%) 1.50 (50%)
Select the runway available with minimum crosswind.
− END −
No
(2) No further action required.
END
ABNORM 3-4
REV 67, Mar 19/07
QUICK REFERENCE HANDBOOK
PSP 604-15
AUTOMATIC FLIGHT
CONTROL SYSTEM
Single Flight Director Failed
NOTE
Anticipate elevator out of trim situation when autopilot is
　
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