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counteract the yaw and roll from asymmetrical
thrust. The control forces, particularly on the
rudder, may be high. The pitch attitude for VYSE
will have to be lowered from that of VY.
Figure 12-11. Engine failure on takeoff, landing gear down.
If Engine Failure Occurs at
or Before Lift-off, Abort the
Takeoff.
If Failure of Engine Occurs After Lift-off:
1. Maintain Directional Control
2. Close Both Throttles
Figure 12-12. Engine failure on takeoff, inadequate climb performance.
Liftoff
Engine Failure
Descend at VYSE
Land Under Control
On or Off Runway
Over Run Area
Ch 12.qxd 5/7/04 9:54 AM Page 12-19
At least 5° of bank should be used, if necessary,
to stop the yaw and maintain directional control.
This initial bank input is held only momentarily,
just long enough to establish or ensure directional
control. Climb performance suffers when
bank angles exceed approximately 2 or 3°, but
obtaining and maintaining VYSE and directional
control are paramount. Trim should be adjusted
to lower the control forces.
• CONFIGURATION—The memory items from
the “engine failure after takeoff” checklist
[Figure 12-14] should be promptly executed to
configure the airplane for climb. The specific
procedures to follow will be found in the
AFM/POH and checklist for the particular airplane.
Most will direct the pilot to assume VYSE,
set takeoff power, retract the flaps and landing
gear, identify, verify, and feather the failed
engine. (On some airplanes, the landing gear is
to be retracted before the flaps.)
The “identify” step is for the pilot to initially
identify the failed engine. Confirmation on the
engine gauges may or may not be possible,
depending upon the failure mode. Identification
should be primarily through the control inputs
required to maintain straight flight, not the
engine gauges. The “verify” step directs the pilot
to retard the throttle of the engine thought to have
failed. No change in performance when the suspected
throttle is retarded is verification that the
correct engine has been identified as failed. The
corresponding propeller control should be
brought fully aft to feather the engine.
• CLIMB—As soon as directional control is established
and the airplane configured for climb, the
bank angle should be reduced to that producing
best climb performance. Without specific
guidance for zero sideslip, a bank of 2° and
one-third to one-half ball deflection on the
slip/skid indicator is suggested. VYSE is maintained
with pitch control. As turning flight
reduces climb performance, climb should be
made straight ahead, or with shallow turns to
avoid obstacles, to an altitude of at least 400
feet AGL before attempting a return to
the airport.
Obstruction Clearance
Altitude or Above
At 500' or Obstruction Clearance Altitude:
7. Engine Failure Checklist
Circle and Land
3. Drag - Reduce - Gear, Flaps
4. Identify - Inoperative Engine
5. Verify - Inoperative Engine
6. Feather - Inoperative Engine
If Failure of Engine Occurs After Liftoff:
1. Maintain Directional Control - VYSE,
Heading, Bank into Operating Engine
2. Power - Increase or Set for Takeoff
Figure 12-13. Landing gear up—adequate climb performance.
Figure 12-14.Typical “engine failure after takeoff” emergency
checklist.
12-20
ENGINE FAILURE AFTER TAKEOFF
Airspeed . . . . . . . . . . . . . . . . . . . Maintain VYSE
Mixtures . . . . . . . . . . . . . . . . . . . RICH
Propellers . . . . . . . . . . . . . . . . . .HIGH RPM
Throttles . . . . . . . . . . . . . . . . . . . FULL POWER
Flaps . . . . . . . . . . . . . . . . . . . . . . . UP
Landing Gear . . . . . . . . . . . . . . . UP
Identify . . . . . . . . . . . . . . . . . . . . Determine failed
engine
Verify Close throttle of
failed engine
Propeller . . . . . . . . . . . . . . . . . . . FEATHER
Trim T abs . . . . . . . . . . . . . . . . . . . ADJUST
Failed Engine . . . . . . . . . . . . . . . SECURE
As soon as practical . . . . . . . . . . LAND
Bold - faced items require immediate action and
are to be accomplished fro m mem ory.
. . . . . . . . . . . . . . . . . . . . . . . .
Ch 12.qxd 5/7/04 9:55 AM Page 12-20
12-21
• CHECKLIST—Having accomplished the
memory items from the “engine failure after
takeoff” checklist, the printed copy should be
reviewed as time permits. The “securing failed
engine” checklist [Figure 12-15] should then be
　
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