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After touchdown:
(3) FLIGHT SPOILER lever ...............................................MAX
− END −
No
(2) No further action required.
END
ABNORM 8-9
REV 74, Nov 07/08
QUICK REFERENCE HANDBOOK
PSP 604-15
FLIGHT CONTROLS
MALFUNCTIONS
GND SPLRS
GND SPLRS
On ground:
Yes
NOTE
GND SPLRS caution message may come on at taxi
speeds above 16 knots.
(1) Airplane ......................................................................STOP
(2) Ground spoilers pre-flight
check ............................................................ACCOMPLISH
Ground spoilers are unserviceable if message
persists.
− END −
No
During flight:
(1) GND SPOILERS ............................................................DISARM
GND SPLRS caution message persists:
Yes
Prior to landing:
(2) GPWS/FLAP OVRD
(if installed) ................................................................ OVRD
(3) Landing flaps .................................................................. 20°
(4) Approach speed ...................................................VREF + 14
minimum.
(5) Actual landing distance...................................... INCREASE
as applicable by factor given below:
WITHOUT THRUST
REVERSERS
WITH THRUST
REVERSERS
1.60 (60%) 1.55 (55%)
NOTE
Landing distance factors for failed ground spoilers are
based upon serviceable flight spoilers.
No
After touchdown:
(2) GND SPOILERS ..................................................................ARM
(3) FLIGHT SPOILER lever .......................................................MAX
END
ABNORM 8-10
REV 74, Nov 07/08
QUICK REFERENCE HANDBOOK
PSP 604-15
FLIGHT CONTROLS
MALFUNCTIONS
STAB TRIM
STAB TRIM
MACH TRIM
(1) STAB TRIM DISC........................... PRESS, HOLD & RELEASE
(2) STAB TRIM CH 1 and CH 2......................................... ENGAGE
STAB TRIM caution message persists:
Yes
(3) STAB TRIM, CH 2 ................................................ ENGAGE
STAB TRIM caution message still persists:
Yes
NOTE
1. Minimize changes to airspeed and
configuration to minimize control forces or
autopilot servo loads.
2. Disregard MACH TRIM caution message.
No
(3) MACH TRIM ................................................................. ENGAGE
− END −
ABNORM 8-11
REV 74, Nov 07/08
▼
QUICK REFERENCE HANDBOOK
PSP 604-15
FLIGHT CONTROLS
MALFUNCTIONS
STAB TRIM (Cont’d)
Autopilot is engaged:
Yes
(4) Autopilot.................................................LEAVE ENGAGED
as long as needed to reduce workload.
AP TRIM IS ND (NU) caution message is displayed:
Yes
(5) Airspeed .........................................................ADJUST
as required to keep autopilot engaged as long
as possible.
NOTE
1. If AP TRIM IS ND is displayed, decrease
airspeed. If AP TRIM IS NU is displayed,
increase airspeed.
2. AP TRIM IS ND (NU) caution message
will go out if the airspeed is adjusted.
AP TRIM IS ND (NU) caution message persists:
Yes
NOTE
Anticipate an out-of-trim condition with autopilot
disengagement.
(6) Autopilot........................................ DISCONNECT
No
Prior to landing:
Failure occurred with flaps at 45°:
Yes
(7) Landing flaps ................................................ LEAVE AT 45°
CAUTION
Do not jettison fuel if trim runaway
is in nose down direction.
Fuel jettison will cause the CG to
move forward requiring a larger
pull force to counter and causing
any push force to be reduced.
Consider use of fuel jettison in the
event of a nose-up trim runaway
condition.
A landing may be made with fuel
in the tail tank.
− END −
ABNORM 8-12
REV 74, Nov 07/08
▼
QUICK REFERENCE HANDBOOK
PSP 604-15
FLIGHT CONTROLS
MALFUNCTIONS
STAB TRIM (Cont’d)
No
(7) GPWS/FLAP OVRD (if installed)....................................... OVRD
(8) Landing flaps .......................................................................... 20°
(9) Approach speed ...........................................................VREF + 14
minimum.
(10) Actual landing distance ............................................. INCREASE
as applicable by factor given below:
WITHOUT THRUST
REVERSERS
WITH THRUST
REVERSERS
　
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