Beechcraft Baron 58 - Engine Failure after Lift-Off and in Flight

BEECHCRAFT Baron 58
Serial TH 773 and After
Section III
Emergency Procedures
ENGINE FAILURE AFTER LIFT-OFF
AND IN FLIGHT
NOTE
The most
important aspect of engine failure is
the necessity to maintain lateral and direc-
tional control. If airspeed is below 81 kts, re-
duce
power on the operative engine as re-
quired to maintain control.
An immediate landing is advisable regardless of take-off
weight. Continued flight cannot be assured if take-off
weight exceeds the weight determined from the TAKE-OFF
WEIGHT graph. Higher
take-off weights will result in a loss
of
altitude while retracting the landing gear and feathering
the propeller. Continued flight requires immediate pilot re-
sponse to the following procedures.
1.
landing Gear and Flaps - UP
2.
Throttle (inoperative engine) - CLOSED
3. Propeller (inoperative engine) - FEATHER
4. Power (operative engine) - AS REQUIRED
5.
Airspeed-MAINTAINSPEEDATENGINEFAILURE(l00
KTS MAX.) UNTIL OBSTACLES ARE CLEARED.
After positive control of the airplane is established"
6. Secure inoperative engine:
a.
Mixture Control - IDLE CUT-OFF
b. Fuel Selector
- OFF
c.
Auxiliary Fuel Pump - OFF
d. Magneto/Start
Switch - OFF
e.
Alternator Switch - OFF
f.
Cowl Flap - CLOSED
7. Electrical Load - MONITOR
(Maximum loadof 1.0 on re-
maining engine)
October 1976
3-5