Piper PA-34-200 Seneca — PA34-200T test
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Piper PA-34-200 Seneca — PA34-200T test
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Name_________________________________________
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Date _________________
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CFI___________________________________________
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Engine Model Number is ________________
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Rated Speed________________
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Engine Type:
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Propeller Type:
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Rated HP @SL_______________
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@12,000Ft___________________
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Engine Oil Capacity ___________
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Rated RPM__________________
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Minimum Fuel Grade_____________________
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Fuel Tank Configuration______________________
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Total Capacity __________________
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Usable_________________
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Maximum Takeoff Weight________________________
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Maximum Landing Weight________________________
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Maximum Zero Fuel Weight_______________________
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Maximum Baggage Compartments (Aft)__________
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(Forward)__________
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Green Arc is _____________
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to_____________
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Yellow Arc is ______________
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to____________
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White Arc is ______________
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to_____________
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What is the Blue Line? __________________
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Speed_______________
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Maximum Gear Extended Speed is______________
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Maximum Landing Gear Extending Speed is____________
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Maximum Landing Gear Retraction Speed is____________
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Maximum Flap Extension Speed at 10(________
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25(________
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40(________
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Air Minimum Control Speed (Vmc) _______________
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State the Basic Engine Failure Procedures
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At what airspeed should the gear be manually lowered? _____________
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State the correct procedure for Cross Feeding.
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State procedures for inadvertent spin recovery
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Cranking of the starter should be limited to _______________sec.
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“Overboost” annunciator lights will illuminate at ___________”Hg
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The maximum demonstrated crosswind component is ______________ KTS.
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The intentional engine inoperative speed is _______________KIAS
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Use Enclosure 1 to determine the Accelerate Stop distance.
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Given: 80( F 4570 Lbs 4500 ft Pressure Alt ________ Ft
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Use Enclosure 2 to determine the Take-off distance over a 50 ft obstacle.
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Given: 70( F, 7000 Ft. Pressure Alt, 4,100 Lbs Takeoff Wt., 15 Kt HW
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___________________ Ft
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Use Enclosure 3 to determine the Rate of Climb (2 engines, and single engine).
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Given: 80( F, 2500 Ft. Pressure Alt., 4570 Lbs.
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__________, ___________Feet per Minute
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Use Enclosure 4 to determine the landing distance.
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Given:80( F, 5,000 Ft Pressure Alt,4,000 lbs landing weight, 5 kts HW.
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Determine the weight and balance for the following conditions.
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Pilot and Front Pax 385 lbs
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Rear Pax (facing aft seats) 170 lbs
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Aft Baggage 100 lbs
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Full Fuel with optional fuel tanks
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Is the Aircraft within limits? Yes No
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Approximately how long would you have to fly at 75%, 23.6 GPH fuel burn in order land within limits?_____________