Piper PA-34-200 Seneca — PA34-200T test
Piper PA-34-200 Seneca · standard normal
NOT FOR FLIGHT
NOT REVIEWED — nobody has checked this against a source document · never used in an aircraft
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Piper PA-34-200 Seneca — PA34-200T test test
Name_________________________________________ Date _________________ CFI___________________________________________ Engine Model Number is ________________ Rated Speed________________ Engine Type: Propeller Type: Rated HP @SL_______________ @12,000Ft___________________ Engine Oil Capacity ___________ Rated RPM__________________ Minimum Fuel Grade_____________________ Fuel Tank Configuration______________________ Total Capacity __________________ Usable_________________ Maximum Takeoff Weight________________________ Maximum Landing Weight________________________ Maximum Zero Fuel Weight_______________________ Maximum Baggage Compartments (Aft)__________ (Forward)__________ Green Arc is _____________ to_____________ Yellow Arc is ______________ to____________ White Arc is ______________ to_____________ What is the Blue Line? __________________ Speed_______________ Maximum Gear Extended Speed is______________ Maximum Landing Gear Extending Speed is____________ Maximum Landing Gear Retraction Speed is____________ Maximum Flap Extension Speed at 10(________ 25(________ 40(________ Air Minimum Control Speed (Vmc) _______________ State the Basic Engine Failure Procedures At what airspeed should the gear be manually lowered? _____________ State the correct procedure for Cross Feeding. State procedures for inadvertent spin recovery Cranking of the starter should be limited to _______________sec. “Overboost” annunciator lights will illuminate at ___________”Hg The maximum demonstrated crosswind component is ______________ KTS. The intentional engine inoperative speed is _______________KIAS Use Enclosure 1 to determine the Accelerate Stop distance. Given: 80( F 4570 Lbs 4500 ft Pressure Alt ________ Ft Use Enclosure 2 to determine the Take-off distance over a 50 ft obstacle. Given: 70( F, 7000 Ft. Pressure Alt, 4,100 Lbs Takeoff Wt., 15 Kt HW ___________________ Ft Use Enclosure 3 to determine the Rate of Climb (2 engines, and single engine). Given: 80( F, 2500 Ft. Pressure Alt., 4570 Lbs. __________, ___________Feet per Minute Use Enclosure 4 to determine the landing distance. Given:80( F, 5,000 Ft Pressure Alt,4,000 lbs landing weight, 5 kts HW. Determine the weight and balance for the following conditions. Pilot and Front Pax 385 lbs Rear Pax (facing aft seats) 170 lbs Aft Baggage 100 lbs Full Fuel with optional fuel tanks Is the Aircraft within limits? Yes No Approximately how long would you have to fly at 75%, 23.6 GPH fuel burn in order land within limits?_____________