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(7) Approach speed ...........................................................VREF + 14
minimum.
(8) Actual landing distance ............................................. INCREASE
as applicable, by factor given below:
WITHOUT THRUST
REVERSERS
WITH THRUST
REVERSERS
1.55 (55%) 1.50 (50%)
NOTE
After touchdown, use nose wheel steering and, if
necessary, differential braking to maintain directional
control, as the airplane will turn in the direction of the
jammed rudder.
END
EMER 10-4
REV 74, Nov 07/08
QUICK REFERENCE HANDBOOK
PSP 604-15 FLIGHT CONTROLS
Stabilizer Trim Runaway
........Abnormal/uncommanded change in pitch attitude.
........Stabilizer trim changes without pilot input.
........Higher or lower than normal and increasing or decreasing pitch control forces.
(1) Control column ...........................................ASSUME CONTROL
and override runaway.
(2) Both STAB TRIM DISC ................................ PRESS, HOLD and
RELEASE
(3) Control .....................................................TRANSFER TO PILOT
(4) STAB CH1 and CH2 HSTCU cbs
(2F8 and 4B8) ................................................................... OPEN
(5) Airspeed .........................................................................ADJUST
NOTE
1. If a pull force is required, increase airspeed. If a
push force is required, decrease airspeed.
2. Do not exceed VMO/MMO or minimum
maneuvering speed as appropriate.
3. Flight spoilers will reduce airspeed and provide
nose up pitch.
4. Reducing thrust will reduce airspeed and provide
nose up pitch.
5. Autopilot, stabilizer trim and Mach trim are not
available.
(6) Land immediately at the nearest suitable airport.
Prior to landing:
(7) GPWS/FLAP OVRD (if installed)....................................... OVRD
CAUTION
Selection of Flaps 20 will increase
nose down pitching moment slightly,
and therefore should be selected just
prior to approach in the event of a full
nose down stabilizer position. Selection
of Flaps 20 significantly reduces
landing field length compared to
Flaps 0.
If control forces are excessive, some
relief may be gained by adjusting
airspeed or flap position. Reduced flap
settings generally reduce pull forces.
Increased flap settings generally
reduce push forces.
EMER 10-5
REV 66, Feb 01/07
▼
QUICK REFERENCE HANDBOOK
PSP 604-15 FLIGHT CONTROLS
Stabilizer Trim Runaway (Cont’d)
(8) Recommended landing flaps.................................................. 20°
(9) Final approach speed.............................................VREF + ΔVREF
for applicable flap setting.
(10) Actual landing distance ............................................. INCREASE
as applicable by factor given below:
Flaps
Setting
(Degrees)
Δ VREF
(KTS)
ALD Factor
Without Thrust
Reversers
With Thrust
Reversers
0 30 1.80 (80%) 1.75 (75%)
20 14 1.55 (55%) 1.50 (50%)
30 7 1.40 (40%) 1.35 (35%)
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.
WARNING
In the event of a go-around, increasing
thrust will increase nose down forces.
Increase thrust slowly to avoid
excessive pitch force.
END
EMER 10-6
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15 FLIGHT CONTROLS
CONTENTS PAGE
Fuel
• Low Fuel Warning ........................................................ EMER 11−2
EMER 11-1
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15 FUEL EMERGENCY
Low Fuel Warning
...........Fuel quantity readouts (amber) when either wing tank is below 230 kg (500 lb), or
...........Total fuel quantity is less than 460 kg (1,000 lb).
(1) Airplane attitude ...................................................... 5° NOSE UP
maximum.
(2) Fuel balance....................................................................CHECK
(3) Land at the nearest suitable airport.
NOTE
Do not attempt go-around. The minimum fuel quantity for
go-around is 230 kg (500 lb) per wing (with the airplane
level), and assuming a maximum airplane climb attitude of
10° nose up.
END
EMER 11-2
　
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