Piper PA-34-200 Seneca — PA34-200T test
NOT FOR FLIGHT — source fidelity: unreviewed | operational review: none | completeness: full
Source: Piper/PA-34-200 Seneca/PA34-200T test.txt
Rights: licensed
Checklist hash: c86ad29edd90ea3b7c68d0642428577564a161ee90e450dbeb3cb8456f62bd2f
Verify against the aircraft's own approved documentation before use.
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PIPER PA-34-200 SENECA — PA34-200T TEST
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[ ] 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?_____________