Learjet 35A - Page 210

ENGINE OVERSPEED
Affected engine:
1. Thrust Lever - Retard.
'CAUTION I~
Do not set affected engine FUEL CMPTR switch OFF.
The fuel computer provides additional overspeed pro-
tection which may be beneficial.
2. If engine does not respond to thrust lever movement - shutdown
engine.
Refer to ENGINE SHUTDOWN IN FUGHT procedure, this I
section.
ENGINE SHUTDOWN IN FUGHT
Affected Engine:
1. ENG SYNC Switch - OFF.
2. Thrust Lever - CUTOFF.
The engine fuel and hydraulic pumps will continue to
operate
with a windmilling engine. Prolonged operation
without fluid available to the pumps may cause damage.
Therefore, the
FIRE PULL or ENG FIRE PULL T-Han-
die should not be pulled unless a fuel or hydraulic leak is
suspected.
3.
Rudder Trim - As required.
4. Yaw Damper - Engage.
5. AIR IGN Switch - OFF.
6. START-GEN Switch - OFF.
7. Electrical Load - Reduce.
'CAUTION I~
During single-engine operation, the COOL-FAN switch
should be placed to OFF to prevent overloading the op-
erating generator.
8.
BLEED AIR Switch - OFF.
9. CROSSFLOW Switch - OPEN. Monitor fuel balance. Crossflowas
required.
-~ During single-engine operation, maintain slip indicator
~, ball centered.
10. Refer to ENGINE AIRSTARTS, Section III or SINGLE-ENGINE
LANDING, this section.
FAA APPROVED 4-30-76
REISSUED 2-25-81, CHANGE 12
4-13