# 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. section_id phase criticality section_title item_index item_id type tickable memory_item indent text response condition detail test normal Piper PA-34-200 Seneca — PA34-200T test 0 challenge yes no 0 Name_________________________________________ test normal Piper PA-34-200 Seneca — PA34-200T test 1 challenge yes no 0 Date _________________ test normal Piper PA-34-200 Seneca — PA34-200T test 2 challenge yes no 0 CFI___________________________________________ test normal Piper PA-34-200 Seneca — PA34-200T test 3 challenge yes no 0 Engine Model Number is ________________ test normal Piper PA-34-200 Seneca — PA34-200T test 4 challenge yes no 0 Rated Speed________________ test normal Piper PA-34-200 Seneca — PA34-200T test 5 challenge yes no 0 Engine Type: test normal Piper PA-34-200 Seneca — PA34-200T test 6 challenge yes no 0 Propeller Type: test normal Piper PA-34-200 Seneca — PA34-200T test 7 challenge yes no 0 Rated HP @SL_______________ test normal Piper PA-34-200 Seneca — PA34-200T test 8 challenge yes no 0 @12,000Ft___________________ test normal Piper PA-34-200 Seneca — PA34-200T test 9 challenge yes no 0 Engine Oil Capacity ___________ test normal Piper PA-34-200 Seneca — PA34-200T test 10 challenge yes no 0 Rated RPM__________________ test normal Piper PA-34-200 Seneca — PA34-200T test 11 challenge yes no 0 Minimum Fuel Grade_____________________ test normal Piper PA-34-200 Seneca — PA34-200T test 12 challenge yes no 0 Fuel Tank Configuration______________________ test normal Piper PA-34-200 Seneca — PA34-200T test 13 challenge yes no 0 Total Capacity __________________ test normal Piper PA-34-200 Seneca — PA34-200T test 14 challenge yes no 0 Usable_________________ test normal Piper PA-34-200 Seneca — PA34-200T test 15 challenge yes no 0 Maximum Takeoff Weight________________________ test normal Piper PA-34-200 Seneca — PA34-200T test 16 challenge yes no 0 Maximum Landing Weight________________________ test normal Piper PA-34-200 Seneca — PA34-200T test 17 challenge yes no 0 Maximum Zero Fuel Weight_______________________ test normal Piper PA-34-200 Seneca — PA34-200T test 18 challenge yes no 0 Maximum Baggage Compartments (Aft)__________ test normal Piper PA-34-200 Seneca — PA34-200T test 19 challenge yes no 0 (Forward)__________ test normal Piper PA-34-200 Seneca — PA34-200T test 20 challenge yes no 0 Green Arc is _____________ test normal Piper PA-34-200 Seneca — PA34-200T test 21 challenge yes no 0 to_____________ test normal Piper PA-34-200 Seneca — PA34-200T test 22 challenge yes no 0 Yellow Arc is ______________ test normal Piper PA-34-200 Seneca — PA34-200T test 23 challenge yes no 0 to____________ test normal Piper PA-34-200 Seneca — PA34-200T test 24 challenge yes no 0 White Arc is ______________ test normal Piper PA-34-200 Seneca — PA34-200T test 25 challenge yes no 0 to_____________ test normal Piper PA-34-200 Seneca — PA34-200T test 26 challenge yes no 0 What is the Blue Line? __________________ test normal Piper PA-34-200 Seneca — PA34-200T test 27 challenge yes no 0 Speed_______________ test normal Piper PA-34-200 Seneca — PA34-200T test 28 challenge yes no 0 Maximum Gear Extended Speed is______________ test normal Piper PA-34-200 Seneca — PA34-200T test 29 challenge yes no 0 Maximum Landing Gear Extending Speed is____________ test normal Piper PA-34-200 Seneca — PA34-200T test 30 challenge yes no 0 Maximum Landing Gear Retraction Speed is____________ test normal Piper PA-34-200 Seneca — PA34-200T test 31 challenge yes no 0 Maximum Flap Extension Speed at 10(________ test normal Piper PA-34-200 Seneca — PA34-200T test 32 challenge yes no 0 25(________ test normal Piper PA-34-200 Seneca — PA34-200T test 33 challenge yes no 0 40(________ test normal Piper PA-34-200 Seneca — PA34-200T test 34 challenge yes no 0 Air Minimum Control Speed (Vmc) _______________ test normal Piper PA-34-200 Seneca — PA34-200T test 35 challenge yes no 0 State the Basic Engine Failure Procedures test normal Piper PA-34-200 Seneca — PA34-200T test 36 challenge yes no 0 At what airspeed should the gear be manually lowered? _____________ test normal Piper PA-34-200 Seneca — PA34-200T test 37 challenge yes no 0 State the correct procedure for Cross Feeding. test normal Piper PA-34-200 Seneca — PA34-200T test 38 challenge yes no 0 State procedures for inadvertent spin recovery test normal Piper PA-34-200 Seneca — PA34-200T test 39 challenge yes no 0 Cranking of the starter should be limited to _______________sec. test normal Piper PA-34-200 Seneca — PA34-200T test 40 challenge yes no 0 “Overboost” annunciator lights will illuminate at ___________”Hg test normal Piper PA-34-200 Seneca — PA34-200T test 41 challenge yes no 0 The maximum demonstrated crosswind component is ______________ KTS. test normal Piper PA-34-200 Seneca — PA34-200T test 42 challenge yes no 0 The intentional engine inoperative speed is _______________KIAS test normal Piper PA-34-200 Seneca — PA34-200T test 43 challenge yes no 0 Use Enclosure 1 to determine the Accelerate Stop distance. test normal Piper PA-34-200 Seneca — PA34-200T test 44 challenge yes no 0 Given: 80( F 4570 Lbs 4500 ft Pressure Alt ________ Ft test normal Piper PA-34-200 Seneca — PA34-200T test 45 challenge yes no 0 Use Enclosure 2 to determine the Take-off distance over a 50 ft obstacle. test normal Piper PA-34-200 Seneca — PA34-200T test 46 challenge yes no 0 Given: 70( F, 7000 Ft. Pressure Alt, 4,100 Lbs Takeoff Wt., 15 Kt HW test normal Piper PA-34-200 Seneca — PA34-200T test 47 challenge yes no 0 ___________________ Ft test normal Piper PA-34-200 Seneca — PA34-200T test 48 challenge yes no 0 Use Enclosure 3 to determine the Rate of Climb (2 engines, and single engine). test normal Piper PA-34-200 Seneca — PA34-200T test 49 challenge yes no 0 Given: 80( F, 2500 Ft. Pressure Alt., 4570 Lbs. test normal Piper PA-34-200 Seneca — PA34-200T test 50 challenge yes no 0 __________, ___________Feet per Minute test normal Piper PA-34-200 Seneca — PA34-200T test 51 challenge yes no 0 Use Enclosure 4 to determine the landing distance. test normal Piper PA-34-200 Seneca — PA34-200T test 52 challenge yes no 0 Given:80( F, 5,000 Ft Pressure Alt,4,000 lbs landing weight, 5 kts HW. test normal Piper PA-34-200 Seneca — PA34-200T test 53 challenge yes no 0 Determine the weight and balance for the following conditions. test normal Piper PA-34-200 Seneca — PA34-200T test 54 challenge yes no 0 Pilot and Front Pax 385 lbs test normal Piper PA-34-200 Seneca — PA34-200T test 55 challenge yes no 0 Rear Pax (facing aft seats) 170 lbs test normal Piper PA-34-200 Seneca — PA34-200T test 56 challenge yes no 0 Aft Baggage 100 lbs test normal Piper PA-34-200 Seneca — PA34-200T test 57 challenge yes no 0 Full Fuel with optional fuel tanks test normal Piper PA-34-200 Seneca — PA34-200T test 58 challenge yes no 0 Is the Aircraft within limits? Yes No test normal Piper PA-34-200 Seneca — PA34-200T test 59 challenge yes no 0 Approximately how long would you have to fly at 75%, 23.6 GPH fuel burn in order land within limits?_____________