3-56 Developed for Training Purposes Leerjet 35/36
February 1998
CAE SimuFlite
Fuel
When using aviation gasoline (50% or more by volume), restrict
airplane flights to below 15,000 ft. Both electric standby boost
pumps must be on and operating when using aviation gasoline.
Aviation gasoline, MIL-D-5572D, Grades 80/87, 100/130 and
115/145 not in excess of 500 gallons per 100 hours of opera-
tion per engine may be used an emergency fuel and may be
mixed in any proportion with various listed kerosene-base fuels
as long as the rate usage of aviation gasoline does not exceed
500 gallons per 100 hours of operation per engine.
Maximum tip tank fuel for landing is 925 lbs each tip.
Jet A, Jet A-1, and Jet B conforming to ASTM ES-2-74 (Emer-
gency Standard Specification for Aviation Turbine Fuels) may
be used as temporary fuels until further notice.
Powerplant
Starting. . . . . . . . . . . . . . . . . . . . . . 860°C ITT FOR 1 SECOND
Takeoff . . . . . . . . . . . . . . . . . . . .870°C ITT FOR 30 SECONDS
. . . . . . . . . . . . . . . . .860°C ITT FOR 5 MINUTES
. . . . . . . . . . . . . . . . . . . .832°C ITT (UNLIMITED)
Maximum Continuous . . . . . . . . . . . . . 832°C ITT OR 100% N
1
Overspeed . . . . . . . . . . . . . . 103% N1 OR N2 FOR 1 MINUTE
. . . . . . . . . . . . .105% N
1 OR N2 FOR 5 SECONDS
If 105° N
1 or N2 is exceeded, remove engine.
CAUTION: During landings in turbulent air conditions with
the yaw damper off, the airplane may exhibit undesirable lat-
eral-directional (Dutch-roll) characteristics. These character-
istics improve as the wing/tip fuel is consumed. See Before
Landing procedure in AFM Section II and increase airspeed
as required.
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