Miscellaneous Quiz / DA20 Operating Limits (All)

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Score 0/87 Timer 10:00
InquiryLimitation
Main landing gear tire pressure (psi)
Max. ramp weight (lbs)
Max. crosswind component student dual (kts)
Max. OAT (degrees C) operation w/ partial winterization kit
DA20 max. demonstrated crosswind component (kts)
Max. rpm drop difference between magnetos
Positive limit load factor (flaps CRUISE)
Voltmeter lower limit red arc (volts)
Fuel pressure lower limit red line (psi)
Min. rpm drop during magneto check
Forced landing final approach airspeed (flaps LDG)
Max. permissible continuous bhp
Min. rpm for in-flight (area) idle beyond gliding range of a runway
Max. time for oil pressure to reach 10 psi after start
Force propeller to windmill if stopped and starter is inop
Fuel tank capacity (US gal.)
V FE (flaps LDG) (Max. Airspeed with flaps extended)
Max. tailwind component (kts)
Max. CHT (degrees F)
V NO (Max. structural cruising speed)
Min. engine-out airspeed to sustain windmilling prop
Aft CG limit (1764 lbs)
Max. oil temperature (degrees F)
V S0 (Stall speed in LDG configuration)
V X (flaps CRUISE) (Best angle of climb)
Min. oil pressure (psi)
Min. oil temp for full power operation if oil pressure norm
Max. rpm after start until oil temp indication registers
Forced landing final approach airspeed (flaps CRUISE)
InquiryLimitation
V NE (Never exceed airspeed)
Max. total wind student dual (kts)
Oil temperature normal operating range (degrees F)
Tachometer normal operating range (rpm)
CHT caution range (degrees F)
V Y (flaps CRUISE) (Best rate of climb)
Voltmeter caution range yellow arc (volts)
Min. CHT (degrees F) takeoff & descent
Fuel pressure upper limit red line (psi)
Nose gear tire pressure (psi)
Usable fuel (US gal.)
Min. oil quantity (US qts)
Max. oil pressure for full power operation if OAT < 0 degrees C
Voltmeter upper limit red line (volts)
Max. continuous starter operation
CHT normal operating range (degrees F)
Max. oil quantity (US qts)
V X (flaps T/O) (Best angle of climb)
Max. oil pressure (psi)
Max. crosswind component student solo (kts)
Min. permissible static rpm (full throttle runup)
Min. oil temperature (degrees F)
V Y (flaps T/O) (Best rate of climb)
V R (Rotate Speed)
Min. OAT (degrees C) cabin heat not req for 10 min. before T/O
Max. landing weight (lbs)
Min. idle mixture rise leaned to peak (runup/shutdown)
Max. permissible continuous rpm
Aft CG limit (at or below 1653 lbs)
InquiryLimitation
Min. rpm during engine runup idle check
Maximum airplane structural temperature (degrees C)
Negative limit load factor (flaps CRUISE)
Forward CG limit (1764 lbs)
Lift-off airspeed
Forward CG limit (at or below 1653 lbs)
Best glide airspeed (1764 lbs) (L/D Max)
Normal landing final approach airspeed
No-Flap landing final approach airspeed
Max. cumulative starter op. before cooling 3-5min.
Max. OAT (degrees C) operation w/ full winterization kit
Min. rpm operations with fuel pump off
Forced landing final approach airspeed (flaps T/O)
Positive limit load factor (flaps T/O or LDG)
Max. takeoff weight (lbs)
Voltmeter green arc (volts)
Max. total wind student solo (kts)
Max. weight in baggage compartment (lbs)
Approved fuel grade
Maximum permissible bank angle for steep turns
V A (1764 lbs) (No full or abrupt control inputs above V A or overstress conditions will occur.)
Oil pressure normal operating range (psi)
Max. time for CHT below 300 degrees F in descent (minutes)
Min. oil temp. to begin an area SFL at Area Idle (degrees F)
Max. rpm drop during magneto check
Negative limit load factor (flaps T/O or LDG)
V FE (flaps T/O) (Max. Airspeed with flaps extended)
Propeller approx. minimum ground clearance (inches)
V S1 (Stall speed in CRUISE configuration)

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Created Mar 28, 2010ReportNominate
Tags:limit, limitation, operating

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