3-42 Developed for Training Purposes Leerjet 35/36
February 1998
CAE SimuFlite
Thrust Reversers
Aeronca Thrust Reversers
Operational procedures in the AFM Supplement are manda-
tory.
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Do not attempt to deploy thrust reversers in flight.
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Do not use thrust reversers to back up the aircraft.
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Do not pull thrust reverser CBs while in flight except as
specified in Emergency and/or Abnormal Procedures.
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Do not deploy drag chute (if installed) while using reverse
thrust.
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Thrust reversers are limited to ground operations on
paved surfaces.
Maximum reverse thrust usable at 60 KIAS or above is limited
to fan speed (N1) equal to takeoff power setting. At 60 KIAS,
smoothly and deliberately return the thrust reverser levers to
the reverse idle/deploy position.
S/Ns 35-001 to 153 and 36-001 to 038 with P/N 210 1142-1
fuel computers: Minimum turbine speed (N2) above 40,000 ft
is 86% RPM when the N2 placard is installed on the instrument
panel. Otherwise, turbine speed (N2) is limited by the fuel com-
puter (turbine speed may be slightly less than 86%).
CAUTION: If full reverse power is maintained below 60 KIAS,
reingestion of exhaust gases in the engine may occur.
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