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1.55 (55%) 1.50 (50%)
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 8-13
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15
FLIGHT CONTROLS
MALFUNCTIONS
Stabilizer Trim Malfunction
........Stabilizer cannot be trimmed to desired position.
........STAB CH 1 INOP status message not displayed.
(1) STAB TRIM DISC........................... PRESS, HOLD & RELEASE
(2) STAB TRIM CH 2 ......................................................... ENGAGE
NOTE
Do not engage STAB TRIM CH 1.
(3) MACH TRIM ................................................................. ENGAGE
END
MACH TRIM
MACH TRIM
With at least one STAB TRIM channel engaged:
(1) MACH TRIM ................................................................. ENGAGE
NOTE
With a Mach trim failure, do not exceed 250 KIAS (0.7 M),
unless the autopilot is engaged and functioning normally.
END
Aileron/Rudder Trim Runaway
(1) Rudder (or aileron) ...............................................OVERPOWER
(2) Affected trim ................................................................NEUTRAL
NOTE
Use of autopilot may alleviate trim problem.
END
ABNORM 8-14
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15
FLIGHT CONTROLS
MALFUNCTIONS
AILERON PCU
AILERON PCU
At a safe altitude:
(1) ROLL DISC .......................................................PULL and TURN
NOTE
1. The pilot with the operative aileron will be required
to maintain a roll control input to offset the effects
of the aileron PCU malfunction.
2. If the right aileron control circuit is inoperative, the
autopilot system is inoperative.
(2) Land at the nearest suitable airport.
NOTE
Controllability is reduced. Select longest runway available
with minimum turbulence and crosswind.
Prior to landing:
(3) GPWS/FLAP OVRD (if installed)....................................... OVRD
(4) Landing flaps .......................................................................... 20°
(5) Approach speed ...........................................................VREF + 14
minimum.
(6) Actual landing distance ............................................. INCREASE
as applicable by factor given below:
WITHOUT THRUST
REVERSERS
WITH THRUST
REVERSERS
1.55 (55%) 1.50 (50%)
END
ABNORM 8-15
REV 74, Nov 07/08
QUICK REFERENCE HANDBOOK
PSP 604-15
FLIGHT CONTROLS
MALFUNCTIONS
ELEVATOR SPLIT
ELEVATOR SPLIT
(1) Elevator controls................................................MOVE SLOWLY
and monitor position on EICAS to identify malfunctioning
elevator surface.
If control response is such that intended flight path cannot be
maintained:
At a safe altitude:
(2) Elevator controls..........................................................RELEASE
(3) PITCH DISC handle ..........................................PULL and TURN
(4) Jammed side ............................................................... Determine
If left side, do not re-engage autopilot.
Right side jammed:
Yes
(5) STALL PROT, PUSHER
(either left or right) ........................................................ OFF
NOTE
Stick shaker on operative control column, operates at
a lower intensity.
No
(5) Land at the nearest suitable airport.
NOTE
Controllability is reduced. Select the longest runway
available with minimum turbulence and crosswind.
Prior to landing:
(6) GPWS/FLAP OVRD (if installed)....................................... OVRD
(7) Landing flaps .......................................................................... 20°
(8) Approach speed ...........................................................VREF + 14
minimum.
(9) Actual landing distance ............................................. INCREASE
as applicable by factor given below:
WITHOUT THRUST
REVERSERS
WITH THRUST
REVERSERS
1.55 (55%) 1.50 (50%)
END
ABNORM 8-16
REV 74, Nov 07/08
QUICK REFERENCE HANDBOOK
PSP 604-15
FLIGHT CONTROLS
MALFUNCTIONS
CONTENTS PAGE
• FUEL IMBALANCE ..................................................ABNORM 9−2
• L (R) ENG SOV ........................................................ABNORM 9−3
　
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