Vso 61. Vs1 63. Vr 70. Vx 76. Vxse 78. Vy 89. Vyse. 89 (blue line) Vmc. 61 (radial redline) Vsse 76. Va 134) Vno 163

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1 PA34-200T Piper Seneca II Normal procedures V-speeds Knots Vso 6 Vs 63 Vr 70 Vx 76 Vxse 78 Vy 89 Vyse Vmc 89 (blue line) 6 (radial redline) Vsse 76 Va 2-36(@4507lbs 34) Vno 63 Vfe 38 (0*)/2(25*)/07(40*) Vle 29 Vlr 07 Vlo 29 Vne 95 Nose gear 3 psi Main gear 55 psi

2 PREFLIGHT INSIDE CABIN PA34-200T Piper Seneca II Normal procedures Landing gear control Down Avionics Master switch Gear lights Fuel quantity Lights lift detectors & pitot heat Master switch Magnetos Three green no red As required Open Mixtures Idle cut off Trim Flaps Flight controls Pitot and static system Neutral Down Free and correct Drain Cross feed drains Drain

3 PA34-200T Piper Seneca - PREFLIGHT OUTSIDE CABIN Cross feed drains Right wing flap & aileron Closed Right main gear Right strut and tire Right wing tip Right leading edge Right engine nacelle Right propeller Proper inflation oil Open And secure Fuel drains Nose section Nose gear Nose strut and tire Landing light Windshield Left wing engine nacelle & landing gear Pitot tube Stall warning vanes Rear door Left static vent Dorsal fin air scoop Empennage Drain door secure No leaks Proper inflation Clean movement Latched Clear Clear Stabilator Free and secure Right static vent Antennas Clear Navigation and landing lights

4 PA34-200T Piper Seneca II Normal procedures BEFORE STARTING ENGINES Seats Seatbelts and harnesses Parking brake Circuit breakers Avionics switch Alternate air Anti-collision lights (fin) Alternators Adjusted Fastened As desired In Open STARTING ENGINES Fuel selectors Mixtures Full rich Throttles Propellers Master switch Magnetos (L) Aux fuel pumps Full forward Full forward Prime (L) 4 to 5 seconds at 60 F Throttle (L) Starter (L) When engine starts & tach over 500 rpm: Starter Throttle Auxiliary fuel pump Oil pressure (L) Mixture (L) Half Engage Release 000 RPM Low if necessary for smooth operation Lean REPEAT FOR RIGHT ENGINE Alternators normal indications Gyro pressure

5 TAXIING PA34-200T Piper Seneca II Normal procedures Avionics power switch Fuel selectors Parking brake Brakes Flaps Instruments Heater and defroster Auto pilot Cross feed Release Up BEFORE TAKE OFF Parking brake Flight controls Auto pilot Trim Manifold pressure lines Mixtures Propellers Throttles Propellers Throttles Propellers Propellers Alternate air Magnetos Alternator output Gyro pressure gauge Engine gauges Icing equipment Throttles Fuel selectors Set Free and correct operation For take off Drain Forward Forward 000 RPM feathering RPM maximum drop 900 RPM Exercise governor Forward and then off 50 RPM drop max, 50 RPM max diff. left and right if needed 000 RPM

6 TAXIING Alternators Annunciator panel Flight instruments Wing flaps Doors - Front and back Auxiliary fuel pumps Briefing Press to test Set 0 for normal, 25 short field T.O. Latched Complete Transponder Alt Lights Pitot heat Set - Recog, nav as needed As required 2

7 PA34-200T Piper Seneca II Normal procedures NORMAL TAKEOFF Mixture Full rich 39 / FULL RPM Rotate 70 Kias Pitch 89 Kias (blue line) Gear Up (out of usable runway) 3.5 /2450 RPM (pattern altitude) As required SHORT FIELD TAKEOFF Mixture Brakes Release brakes Control yoke Pitch Clear of obstacles Gear Full rich Hold 39 /2450 RPM Accelerate to 66 Kias Rotate firmly to 7 Kias through 50 feet 76 Kias (Vx) 89 Kias (blue line) Up (out of usable runway) 3.5 /2450 RPM (pattern altitude) As required

8 CLIMB PA34-200T Piper Seneca II Normal procedures 3.5 /2450 RPM Pitch Best rate Cruise climb Best angle 89 Kias 02 Kias 76 Kias As required CRUISE Mixtures Engine gauges Lights 3.5 /2450 RPM (or per performance chart) Lean for cruise Closed or as required Monitor As Required DESCENT Mixtures Icing equipment Lights Enrich with descent Cruise setting Closed As desired BEFORE LANDING Fuel selectors Auxiliary fuel pumps Mixtures Propellers Landing gear Door seals Heater Set Fall forward Down As desired

9 CLIMB Auto pilot 2

10 PA34-200T Piper Seneca II Normal procedures NORMAL LANDING/ PATTERN VFR DOWNWIND Gear down before landing check Down (29 Kias) 20 /Full RPM BASE Flaps 25 Airspeed 05 Kias GUMPS FINAL Flaps 40 Airspeed 90 Kias SHORT FIELD LANDING FINAL Flaps 40 Airspeed 78 Kias TOUCHDOWN Flaps Control yoke Brakes Up Back pressure Apply gently GO AROUND Throttles 39 Flaps/gear/flaps/flaps Clean Open

11 AFTER LANDING PA34-200T Piper Seneca II Normal procedures Flaps Alternate air Heater Transponder Timer Up Open Fan 2 min, then Standby Start, 3 min cool down SHUTDOWN Avionics, lights, fans Mixtures Magnetos Master Alternators Idle cut-off Closed Record time

12 PA34-200T Piper Seneca II Emergency procedures ENGINE FAILURE: TAKEOFF (ON TAKE OFF ROLL) Throttles Brakes and rudder Closed Apply to control aircraft If inadequate runway remains: Master Fuel selector ENGINE FAILURE (IN FLIGHT) IF GEAR DOWN ON CLIMBOUT Rudder Throttles Pitch Identify, Verify, Feather, Mixture Maintain heading Retard to stop turn 89 Knots (blue line) Return to land ABOVE 66 KNOTS Mixtures, props, throttles Gear, flaps Identify Verify (inop throttle) Fix SET Up, as desired Dead foot, dead engine Retard Troubleshooting flow OR Feather Engine securing checklist

13 PA34-200T Piper Seneca II Emergency procedures TROUBLESHOOT / AIR START Fuel selector Aux fuel pump Throttle Open /4 Propeller Mixture Magnetos Starter Throttle Forward Rich Engage until windmilling Low until engine warms If engine does not start, prime as needed Alternator ENGINE SECURING PROCEDURE Throttle (verify inop) Prop (verify inop) Mixture (verify inop) Aux pumps Magnetos (verify inop) Alternator (verify inop) Electrical load Fuel selector (verify inop) Retard Feather (before reaching 800 RPM) Idle cutoff Close (inop) Reduce SINGLE ENGINE LANDING Prop (inop) Feather When runway is assured Gear Down Flaps Extend, 25 Airspeed 9 Kias

14 PA3200T Piper Seneca II Emergency procedures SINGLE ENGINE GO-AROUND (not advised) Mixtures Propellers Throttles Flaps Gear Airspeed (op engine) Forward Forward 39 MP Up Up 89 Kias (blue line) Open ENGINE FIRE INFLIGHT Fuel selector (inop engine) Throttle (inop engine) Propeller (inop engine) Mixture (inop engine) Heater Defroster Flight Close Feather Idle cut off Land immediately ON GROUND (ENGINE NOT STARTED) Mixture Throttle Starter Attempt to suck flames into engine. If fire continues, attempt to extinguish, if extinguishing externally: Fuel selectors Mixtures Idle cut off Open Crank engine Idle cut off

15 PA34-200T Piper Seneca II Emergency procedures EMERGENCY DESCENT Throttles Propellers Mixtures Gear Airspeed Closed Forward Adjust Down 29 Kias SINGLE ENGINE FUEL MANAGEMENT If using fuel from same side as op engine: Fuel selector (op engine) Fuel selector (inop engine) Aux fuel pumps If using fuel from opposite side of op engine: Fuel selector (op engine) Fuel selector (inop engine) Aux fuel pumps Crossfeed *Cross feed in level flight only ** Does not cross feed with full fuel on same side as op engine. Vapor return fuel flow will be vented overboard. ENGINE FAILURE IN ICING CONDITIONS Select alternate air and attempt restart. If unable to restart engine: Prop (inop) Airspeed Electrical load Feather Blue line or above Reduce Land as soon as practicable. Maintain at least blue line on final. Do not extend gear or flaps until runway is assured. Flaps on final Extend, 25

16 PA34-200T Piper Seneca II Emergency procedures ALTERNATOR FAILURE IN ICING CONDITIONS Over-voltage relay Circuit breakers Reset and reset If unable to restore alternator: Avionics Windshield heat, except Nav com and transponder Gear may require free fall extension prior to landing ENGINE DRIVEN FUEL PUMP FAILURE Throttle Aux fuel pump Throttle Retard Unlatch, on high 75% power or less If normal Engine operation and fuel flow are not reestablished, auxiliary fuel pump should be turned off. Lack of fuel flow while on high setting may indicate fuel leak or fuel exhaustion. Auxiliary fuel pumps should only be used for fuel vapor suppression(low) or emergency use(high). High setting during normal engine operation may cause power loss. GEAR UNSAFE WARNING Red light indicates gear in transit. Recycle gear if indication continues. Light will illuminate when gear horn sounds at low throttle settings.

17 PA34-200T Piper Seneca II Emergency procedures MANUAL GEAR EXTENSION before extending gear manually: Circuit breakers Master switch Alternators Nav lights In (daytime) To extend, re-position clip downward and clear of knob and proceed as follows: Airspeed Gear selector Emergency gear extension knob Indicator lights 85 Kias max Down Pull 3 Green Leave emergency gear extension knob out ELECTRICAL FAILURES ALT annunciation light illuminated: Ammeters Determine inop alternator If both alternators inop, reduce electrical load. Turn OFF both switches then on one at a time to observe ammeters. Determine alternator showing least amps and turn it s switch off. Electrical loads Re-establish up to 60 Amps If one ammeter shows zero output, cycle its switch off, then on. If power is not restored check circuit breakers and reset once if required. If alternator remains inop, reduce electrical load and continue flight. Compass error may exceed 0 with both alternators inop.

18 PA34-200T Piper Seneca II Emergency procedures GYRO PRESSURE FAILURES Pressure bellow 4.5 Hg RPM Increase to 2575 Altitude Descend to maintain 4.5 Hg Use electric turn coordinator to monitor pressure instruments performance HEATER OVERHEAT Unit will automatically shut off. Do not attempt to restart in flight.

19 PA34-200T Piper Seneca II Manuevers STEEP TURNS Airspeed 24 /2500 RPM Above Va Clearing turns Select visual reference Roll into 45 or 50 turn, add 2 MP SLOW FLIGHT Clearing turns Select visual references Props Gear, flaps Pitch Recover 5 /Full RPM Forward Open Gear down, full flaps 70 Kias (minimum) or selected airspeed To maintain altitude (approx 2 MP) Pitch/power/positive rate/flaps/gear/flaps/flaps

20 PA34-200T Piper Seneca II Manuevers POWER-ON STALL Clearing turns Select visual reference Props Gear Airspeed 5 /2450 RPM Forward Open or as required Down (flaps up) Slow to 80 Kias 27 Pitch Identify Stall Recover For stall Call out horn, buffet, stall Reduce Pitch for 89 KTS POWER-OFF STALL Clearing turns Select visual reference Configure for Slow Flight Pitch 89 KTS Idle When Stabilized Identify Stall Recover Call out horn, buffet, stall Set throttle to T in throttle, reduce pitch Gear up, flaps 25 deg Set power 39, pitch 89 kts, Flaps up at + rate of climb

21 PA34-200T Piper Seneca II Manuevers Vmc DEMO Clearing turns Select visual references Props Mixture Gear, flaps Inoperative engines cowl flap 5 /2450 RPM Forward Rich Up Closed Retard left (inop) side Advance right (op) side Pitch Up to obtain 66 Kias (Vmc) Feed in rudder to maintain directional control First indication of stall or loss of directional control: Retard op throttle Pitch 89 Kias (blue line) At blue line, 38 (op-throttle) DRAG DEMO Clearing turns Airspeed Left throttle Right prop 5 /2450 RPM 89 Kias (Blue line) Retard Forward Right throttle 38 VSI Gear VSI Flaps VSI Note reading Down Note reading Down Note reading Left prop Simulate feather (throttle 2 )

22 Vmc DEMO VSI Flaps/gear/flaps/flaps VSI Note reading Clean up in stages Note reading after each step 2