# Piper PA-34-200 Seneca — PA34-200T test

> **NOT FOR FLIGHT** — source fidelity: unreviewed | operational review: none | completeness: full

## Piper PA-34-200 Seneca — PA34-200T 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?_____________

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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.