UH 60 PPC EXAM LATEST VERSION REAL EXAM QUESTIONS WITH 100% CORRECT ANSWERS
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UH 60 PPC
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UH 60 PPC
UH 60 PPC EXAM LATEST VERSION REAL EXAM QUESTIONS WITH 100% CORRECT ANSWERS
Cruise Torque - Answer-CRUISE TORQUE is simply the torque required to maintain your desired cruise airspeed for your given weight and configuration.
Continuous Torque Available - Answer-is the most torque the engines c...
UH 60 PPC EXAM LATEST VERSION
REAL EXAM QUESTIONS WITH 100%
CORRECT ANSWERS
Cruise Torque - Answer-CRUISE TORQUE is simply the torque required to maintain
your desired cruise airspeed for your given weight and configuration.
Continuous Torque Available - Answer-is the most torque the engines can produce
continually and remain out of the 30 minute engine operating limitations. This is the
MCP line in the cruise charts in chapter 7 of the -10. The aircraft will be at the top of one
or more of the continuous ranges: 1) TGT - 793 2) Eng oil temp 135 C. As the name
implies, there is no time limit on maintaining this torque.
Cruise Fuel Flow - Answer-This is the predicted fuel flow (burn rate) that the aircraft
should have at cruise torque.
MAX RANGE IAS / TORQUE (dual enqine) - Answer-This is defined as the speed which
yields the maximum nautical miles per pound of fuel for a specific configuration, weight,
and altitude.
MAX ENDURANCE IAS / TORQUE (dual enqine) - Answer-This is defined as the speed
which yields the minimum fuelflow attainable for a specific configuration, weight, and
altitude. Simply stated, MAX ENDURANCE IAS/TORQUE will give you the most
HOURS of flight time per pound of fuel.
CRITICAL TORQUE - Answer-Critical Torque is the dual engine torque value, which
when exceeded, may not allow the aircraft to maintain % RPM R within normal limits
under single-engine operations in the same flight conditions.
MAX ALLOWABLE GWT & OPTIMUM AIRSPEED AT MAX ALLOWABLE GWT (dual
enqine) - Answer-This will provide the aircrew with an airspeed value to fly as quickly as
possible to the destination, while remaining out of any 30-minute limits or the lowest
possible TGT.
MAX R/C IAS / TORQUE - Answer-This is the airspeed that allows the aircraft to climb
from one altitude to a higher altitude in the least amount of time. Airspeed is corrected
for pitot static system error at rates of climb Greater and less than 1400 FPM.
MAX ALT MSL - Answer-This is the maximum altitude the aircraft can fly at MAX
ENDURANCE IAS for its given weight, configuration, and ETF/ATF.
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