N123AX Piper Saratoga II HP (PA-32R-301) Checklist (v23 - Revision 3 April 2011) AIRSPEEDS FOR SAFE OPERATIONS. Best Rate of Climb (gear up, flaps up)

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1 N123AX Piper Saratoga II HP (PA-32R-301) Checklist (v23 - Revision 3 April 2011) AIRSPEEDS FOR SAFE OPERATIS Best Rate of Climb (gear down, flaps up) Best Rate of Climb (gear up, flaps up) Turbulent Air Operating Speed Maximum Flap Speed Downwind Speed (10 ) Base Leg Speed (25 ) Landing Final Approach Speed (Full ) Maximum Demonstrated Crosswind Velocity 85 KIAS 93 KIAS 134 KIAS 111 KIAS 100 KIAS 90 KIAS 80 KIAS 17 KTS PREFLIGHT CHECK COCKPIT Fuel Strainer Control Wheel Gear Handle Parking Brake Radio Master Switch All Switches Magneto Switches Fuel Gauges Fuel Selector Annunciator Panel Primary Flight Controls Trim Pitot & Static System Windows Required Papers and POH Tow Bar and Baggage Baggage door-rear drain & for water & sediment release restraints down set IDLE / quantity SET LOWEST TANK extend proper operation neutral drain clean on board stow properly - secure close and secure RIGHT WING Surface Condition Flap and hinges Aileron and hinges Static wicks Wing tip and lights Fuel Tank Fuel Quantity gauge clear of ice, frost, snow - secure supply visually secure cap

2 Fuel Tank Vent Fuel Tank sumps Tie down and chock Main gear strut Tire Brake block and disc Fresh air inlet clear drain and for water, sediment and proper fuel remove proper Inflation (4.5 ±.5 in) NOSE SECTI Baggage door General condition Cowling Windshield Propeller and spinner Air Inlets Engine baffle seals Chock Nose gear strut Nose gear doors Nose gear tire Landing light Oil Dipstick Oil filler cap close and secure secure clean clear remove proper Inflation (3.25 ±.25 in) secure quantity (9 Quarts Min) properly seated secure LEFT WING Surface Condition Fresh air inlet Fuel Tank sump Tie down and chock Main gear strut Tire Brake block and disc Fuel Tank Vent Fuel Quantity gauge Fuel Tank Stall warning vanes Pitot head Wing tip and lights Aileron and hinges Flap and hinges Static wicks clear of ice, frost, snow drain and for water, sediment and proper fuel remove proper Inflation (4.5 ±.5 in) clear supply visually secure cap remove cover holes clear - secure

3 FUSELAGE Antennas Static vents Empennage Stabilator and trim tab Tie down clear clear of ice, frost, snow remove MISCELLANEOUS Battery master switch Interior lighting Pitot heat switch Exterior lighting switches Pitot Stall warning horn All lighting switches Pitot heat switch Battery master switch Passengers Doors Seats Seat belts and harness retract and and - warm board closed and secure adjusted & locked fasten/adjust/ inertia reel BEFORE STARTING ENGINE Fire Extinguisher Altimeter & Instruments Alternator Switch Circuit Breakers Alternate Air Propeller Alternate Static Annunciator Panel CHECKED UP CHECKED IN CLOSED MAX RPM closed NORMAL START COLD ENGINE Alternator Switch Magneto Switches Electric Fuel Pomp Propeller Area Fuel Pomp Start 1/2inch OPEN PRIME then IDLE CUT- CLEAR MAX 15 SEC RICH 1000 rpm

4 HOT START Alternator Switch Magneto Switches Electric Fuel Pomp Propeller Area Fuel Pomp Start 1/2inch OPEN IDLE CUT- CLEAR MAX 15 SEC RICH 1000 rpm FLOODED START Alternator Switch Magneto Switches Electric Fuel Pomp Propeller Area Start FULL OPEN IDLE CUT- CLEAR MAX 15 SEC RICH 1000 rpm AFTER START Oil Pressure GREEN SECTOR Nav & Strobe Light AS REQUIRED Radio Master Switch Marker Lights CHECKED Autopilot TEST Gyro lining up Fuel Selector SET FULLEST TANK Aux Vacuum Pump AUX light on increase electrical load of approx 15 amps on ammeter Ammeter CHECK increased charge Aux Vacuum Pump - AUX light off TAXI Parking Brake Propeller Brakes Steering Flight Instruments Take-Off Briefing RELEASE full INCREASE apply slowly CHECKED REVIEWED

5 GROUND CHECK Parking Brake Propeller Electric Fuel Pomp Magnetos Vacuum Oil Temperature Oil Pressure Propeller Alternate Air Electric Fuel Pomp Fuel flow Compass Gyro SET full INCREASE 2000 rpm max drop 175 RPM max diff 50 RPM inch Hg RICH exercise then full INCREASE max 500 RPM drop & close READ IDLE - then 1000 rpm RESET BEFORE TAKE- Alternator Switch Magneto Switches Flight Instruments Engine gauges Propeller Elevator Trim Rudder Trim Flight Controls Doors Cabin Fan Landing Light Pilot Heat Altimeter Transponder Verify Verify Verify set set set set slightly aft set to the right free & correct closed and latched AS REQUIRED SET / CHECKED AS REQUIRED

6 NORMAL TAKE Trim Rotate Landing Gear Power Settings retracted set 84 to 88 KIAS depending on weight UP 110 KIAS max when straight away landing on runway not possible Full / 2700 RPM SHORT FIELD, OBSTACLE CLEARANCE 25 Trim slightly aft of neutral full power prior to brake release Rotate 69 to 72 KIAS depending on weight After breaking ground, accelerate to 74 to 77 KIAS depending on aircraft weight Landing Gear UP 110 KIAS max Accelerate to climb speed retract slowly CLIMB After 500ft AGL MAP reduce to 25 MAP RPM reduce to 2500 RPM rich side of 75% 6 divisions (150 F) rich of peak for engine cooling Best Rate (3600lbs Gear DOWN flaps up) Best Rate (3600lbs Gear UP flaps up) En route Electric Fuel Pomp 85 KIAS 93 KIAS 105 KIAS at desired altitude CRUISE Power Settings 65% (cf. power setting table) Peak EGT Keep CHT below 400 F Oil Temp between 165 F and 220 F DESCENT Power Settings as required richer as required Avoid Fast Cooling of the Engine. Strive for 50 F per minute

7 APPROACH AND LANDING Fuel Selector Landing Gear App, Set Up & Briefing Altimeter (Transition Level) Power Settings FULLEST TANK set down 132 KIAS max set 110 knots max PERFORMED SET 19 MAP / 2100 RPM Try to maintain at least 15 MAP during approach BEFORE LANDING Auto Pilot Propeller Landing Gear Landing Light Speed Full RICH MAX RPM DOWN / 3 GREENS AS REQUIRED 80 KIAS AFTER LANDING No Essential Avionics Landing Light Pilot Heater Trim UP AS REQUIRED TAKE- SHUT DOWN Radio Master Switch Electric Switches Magneto switches Alternator switch closed idle cut-off

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13 N123AX Piper Saratoga II HP (PA-32R-301) Emergency Checklist (v23 - Revision 3 April 2011) AIRSPEEDS FOR SAFE OPERATIS Stall Speeds 3600 lbs (Gear Up, 0 Flap) 67 KIAS 3600 lbs (Gear Up, 40 Flap) 63 KIAS Maneuvering Speeds 3600 lbs 134 KIAS 2230 lbs 105 KIAS Never Exceed Speed 191 KIAS Power Off Glide Speed 3600 lbs (Gear Up, 0 Flap) 83 KIAS ENGINE FIRE DURING START Starter Electric fuel pump Fuel selector Abandon if fire continues crank Engine idle cut off open ENGINE POWER LOSS DURING TAKE If sufficient runway remains for a normal landing, leave gear DOWN land straight ahead If area ahead is rough or if it is necessary to clear obstructions: Gear Selector Switch UP If sufficient altitude has been gained to attempt a restart: Airspeed MAINTAIN SAFE Fuel Selector SWITCH to TANK CTAINING FUEL CHECK CHECK RICH Alternate Air OPEN If power is NOT regained, proceed with power off landing.

14 ENGINE POWER LOSS IN FLIGHT If at low altitude: Airspeed Prepare for power off landing MAINTAIN 83 KIAS Minimum If altitude permits: Fuel Selector Alternate Air Engine Gauges SWITCH to TANK CTAINING FUEL RICH OPEN CHECK for INDICATI of CAUSE of POWER LOSS If no fuel pressure is indicated, tank selector position to be sure it is on a tank containing fuel. When Power is Restored: Alternate Air If power is not restored, prepare for power off landing. CLOSE adjust as necessary POWER LANDING - Trim for 83 KIAS - Locate suitable field - Establish spiral pattern ft. above field at downwind position for normal landing - When field can easily be reached extend full flaps for shortest landing - Touchdowns should be made at lowest possible airspeed with full flaps. When committed to landing: Landing Gear Selector Magnetos Alternator Switch Fuel Selector Seat Belts and Harness Cabin doors DOWN AS DESIRED CLOSE IDLE CUT- tight unlatch and open NOTE: If master switch is, the landing gear cannot be retracted.

15 FIRE IN FLIGHT Source of Fire Electrical Fire (Smoke in Cabin) Alternator Switch Vents Cabin Heat Land as soon as practicable Engine Fire Fuel Selector Heater and defroster Proceed with POWER LANDING procedure CHECK OPEN CLOSED IDLE CUT- CHECK LOSS OF OIL PRESSURE - Land as soon as possible and investigate cause - Prepare of power off landing LOSS OF FUEL FLOW Fuel Selector on tank containing usable fuel Land as soon as practicable ENGINE DRIVEN FUEL PUMP FAILURE retard reset as required CAUTI: if normal engine operation and fuel flow is not immediately reestablished, the electric fuel pump should be turned. The lack of a fuel flow indication while the electric fuel pump is on could indicate a leak in the fuel system or fuel exhaustion. If fuel system leak is verified, switch fuel selector to off.

16 HIGH OIL TEMPERATURE - Land at nearest airport and investigate the problem - Prepare for power off landing ELECTRICAL FAILURES ALT annunciator is illuminated Ammeter If Ammeter shows Zero: ALT Switch Reduce electrical load to minimum ALT circuit breaker ALT Switch If power not restored ALT Switch to verify inop alt and reset as required If alternator output cannot be restored, reduce electrical loads and land as soon as practical. The battery is the only remaining source of electrical power. ELECTRICAL OVERLOAD (ALTERNATOR OVER 20 AMPS ABOVE KNOWN ELECTRICAL LOAD) ALT Switch BAT Switch If alternator loads are reduced Electrical load reduce to minimum Land as soon as practical If alternator loads are not reduced ALT Switch BAT Switch as required Land as soon as practical. Anticipate complete electrical failure.

17 PROPELLER OVERSPEED Oil Pressure Propeller Control Airspeed RETARD CHECK FULL DECREASE RPM then SET if any CTROL AVAILABLE REDUCE AS REQUIRED to REMAIN BELOW 2700 RPM EMERGENCY LANDING GEAR EXTENTI Prior to emergency extension procedure: ALTR Switch Circuit Breakers Day/Night dimming switch (in daytime) Gear Indicator Bulbs CHECK CHECK CHECK day by depressing Annunc. test If landing gear does NOT down and locked: Airspeed Landing Gear Selector Switch REDUCE BELOW 90 KIAS GEAR DOWN POSITI If landing gear still does not down and locked: Emergency Gear knob PULL, while fish tailing airplane (under normal conditions will take approx. 10 seconds to be down and locked) If all electrical power has been lost, the landing gear must be extended using the above procedures. The gear position indicator lights will not illuminate SPIN RECOVERY Rudder Control Wheel Ailerons FULL OPPOSITE to DIRECTI of ROTATI FULL FORWARD NEUTRAL IDLE When rotation stops: Rudder Control Wheel NEUTRAL REGAIN LEVEL FLIGHT ATTITUDE AS REQUIRED

18 OPEN DOOR Airspeed Cabin Vents Storm Window If door latch is open If Side Latch Open REDUCE TO 90 KIAS CLOSE OPEN LATCH PULL on ARMREST while Latching ENGINE ROUGHNESS Alternate Air Fuel Selector Engine Gauges Magneto Switch ADJUST for maximum smoothness OPEN SWITCH TANKS CHECK and proceed accordingly L then R, then BOTH If operation is satisfactory on either one, continue on that magneto at reduced power, with full RICH mixture, to a landing at the first available airport. If roughness persists, prepare for a precautionary landing. LOSS OF ENGINE DRIVEN VACUUM (SUCTI) PUMP If vacuum pressure falls below 4.8 In. Hg. (and/or VAC annunciator) Auxiliary Vacuum Switch Verify vacuum system suction 4.8 to 5.2 In. Hg. Compass error may exceed 10 Monitor electrical load. If required turn off non essential electrical equipment Land at the earliest opportunity to have primary system repaired