NSA Master Checklist Seminoles Fuel Injected Rev 12

FUEL QUANTITY ................................... CHECK *Call line service for fuel if need (507)508-0323 OIL .................................... CHECK 6-8 QUARTS COCKPIT INSPECTION AIRCRAFT PARKING BRAKE ........................................ SET REQUIRED DOCUMENTS ...................... VERIFY *Airworthiness certificate should be visible to all passengers. HOBBS/TACH TIME ...............................VERIFY *Must match with the ramp out sheet. If not, call dispatch (507) 508-0706 FLIGHT CONTROLS ...............................CHECK *For ease and continuity PARKING BRAKE ....................................... SET *Parking brake is set by pushing on the toe brakes and pulling the parking brake knob out. PITOT/STATIC ....................................... DRAIN *Do not cover holes on buttons CIRCUIT BREAKERS .......................... CHECK IN ALTERNATE STATIC SOURCE ............... CLOSED MAGNETO SWITCHES ............................... OFF FUEL PUMPS............................................. OFF LANDING GEAR LEVER ......................... DOWN THROTTLES .............................................. IDLE MIXTURES..........................................CUT-OFF COWL FLAPS .......................................... OPEN TRIMS ............................................... NEUTRAL FUEL SELECTORS ....................................... ON ELECTRICAL SWITCHES ............................. OFF BATTERY MASTER SWITCH ........................ ON *Battery master will be left on as little as possible to prevent draining the battery. INTERIOR LIGHTING (NIGHT FLIGHT)….CHECK FUEL GUAGES ...................................... CHECK *Verify fuel tank visually LANDING GEAR LIGHTS .................... 3 GREEN PITOT HEAT............................................... ON *Limit pitot heat on the ground to no more than 3 minutes. EXTERNAL LIGHTS .................................... ON *Exit aircraft to verify operation of all lights and pitot heat. Remove aircraft blankets at this time and stow in baggage compartment. PITOT HEAT........................................... CHECK EXTERNAL LIGHTS ................................. CHECK *Enter aircraft PITOT HEAT SWITCH ................................ OFF ALL LIGHTING SWITCHES ......................... OFF BATTERY MASTER SWITCH....................... OFF EMERGENCY EXIT ...............................SECURE FLAPS.................................................. SET 40° WINDOWS/WINDSHIELD ...................... CLEAN BAGGAGE .......................................... SECURE EMPTY SEATBELTS .............................. FASTEN TOW BAR/CHOCKS..............................SECURE *Towbar and chocks need to be secured in its specifically designed holder or underneath the straps. BAGGAGE DOOR ............................... CLOSED RIGHT WING FUEL SUMPS .........................................DRAIN *If any contaminants are found, dump waste fuel into red containers along fence and take another sample. WING SURFACES ..................... CHECK/CLEAN *Ice, frost, and snow must be removed before attempting flight. If ice/frost is found on the wing, call Line Service for de-icing (507) 508-0323 FLAPS/HINGES ..................................... CHECK *Pushrods should have some wiggle AILERON AND HINGES ......................... CHECK *Pushrods should have some wiggle STATIC WICKS ...................................... CHECK *IFR flights not allowed without all nine static wicks present WING TIPS AND LIGHTS ....................... CHECK LEADING EDGE..................................... CHECK SCUPPER DRAIN................................... CLEAR FUEL VENT ............................................ CLEAR TIE DOWN/CHOCK............................ REMOVE FUEL TANK......................... CHECK QUANTITY NACALLE FUEL FILLER CAP……CHECK/SECURE OIL QUANTITY/CAP ................. CHECK/SECURE PROP AND SPINNER............................. CHECK ALTERNATOR BELT ............................... CHECK FRESH AIR INLET ................................... CLEAR COWLING INTERIOR ............................. CHECK *Using a flashlight, look for loose/broken wires, baffle seals, and any foreign material such as metal shavings or bird feathers. GEAR WELL AND DOORS ..................... CHECK *Check for any obstructions that would prevent the gear from fully retracting. GEAR LINE AND SWITCHES .................. CHECK CRANKCASE BREATHER TUBE ...............CLEAR MAIN GEAR STRUT ...................... APROX 2.6” *If the strut is not long enough, it requires more nitrogen the aircraft should be downed *If a puddle is found by the landing gear it can be an indication of a hydraulic fluid leak and should be inspected by maintenance. TIRE/BRAKEPAD/DISC........................... CHECK *Check for any erosion or deflation that would result in degraded braking action. DOOR HINGES...................................... CHECK NOSE SECTION GENERAL CONDITION .......................... CHECK WINDSHIELD ........................................ CLEAR BATTERY VENTS ................................... CLEAR LANDING LIGHT ................................... CHECK AIR INLETS ............................................CLEAR HEATER INLET/EXHAUST .......................CLEAR CHOCKS ........................................... REMOVE NOSE GEAR STRUT ..................... APROX. 2.7” *If the strut is not long enough, it requires more nitrogen the aircraft should be downed *If a puddle is found by the landing gear it can be an indication of a hydraulic fluid leak and should be inspected by maintenance. NOSE WHEEL TIRE................................ CHECK GEAR WELL AND DOORS ..................... CHECK GEAR LINE AND SWITCHES .................. CHECK LEFT WING WING SURFACES...................... CHECK/CLEAN *Ice, frost, and snow must be removed before attempting flight. If ice/frost is found on the wing, call Line Service for de-icing. (507) 508-0323 NOSE GEAR MIRROR............................ CLEAN LEADING EDGE..................................... CHECK MAIN GEAR STRUT ...................... APROX 2.6” *If the strut is not long enough, it requires more nitrogen the aircraft should be downed. *If a puddle is found by the landing gear it can be an indication of a hydraulic fluid leak and should be inspected by maintenance. TIRE/BRAKEPAD/DISC .......................... CHECK *Check for any erosion or deflation that would result in degraded braking action. TIE DOWN/CHOCK ............................REMOVE GEAR WELL AND DOORS ..................... CHECK *Check for any obstructions that would prevent the gear from fully retracting. GEAR LINES AND SWITCHES ................ CHECK CRANKCASE BREATHER TUBE .............. CLEAR COWLING INTERIOR............................. CHECK *Using a flashlight, look for loose/broken wires, baffle seals, and any foreign material such as metal shavings or bird feathers. ENGINE COMPARTMENT ..................... CHECK FUEL TANK ......................... CHECK QUANTITY NACALLE FUEL FILLER CAP……CHECK/SECURE OIL QUANTITY/CAP ................ CHECK/SECURE PROP AND SPINNER ............................ CHECK ALTERNATOR BELT............................... CHECK FRESH AIR INLET ................................... CLEAR SCUPPER DRAIN.................................... CLEAR FUEL VENT ............................................ CLEAR STALL WARNING VANES ...................... CHECK TEMP PROBE ....................................... CHECK PITOT MAST ......................... UNOBSTRUCTED WING TIPS AND LIGHTS ....................... CHECK AILERON AND HINGES ......................... CHECK *Pushrods should have some wiggle FLAPS AND HINGES ............................. CHECK *Pushrods should have some wiggle NSA Master Checklist Seminoles Fuel Injected Rev 12 pg 8 NSA Master Checklist Seminoles Fuel Injected Rev 12 pg 7 STATIC WICKS ...................................... CHECK *Flight in IFR conditions is not allowed without all nine static wicks. FUSELAGE/EMPENNAGE GENERAL CONDITION .......................... CHECK EMERGENCY EXIT ................................ CHECK FRESH AIR INLET .................................. CHECK SURFACE CONDITION .......................... CLEAR ANTENNAS .......................................... CHECK RUDDER............................................... CHECK STABILATOR......................................... CHECK ANTISERVO TAB................................... CHECK STATIC WICKS ...................................... CHECK *Flight in IFR conditions is not allowed without all nine static wicks. TIE DOWN .................... REMOVE AND CHECK *Black paint should be on the bottom of the tie down. If the paint is scraped, it can be an indication of a tail strike and should be inspected by maintenance. UNDERBELLY........................................ CHECK BAGGAGE DOOR ........ CLOSED AND LATCHED CABIN DOOR........................................ CHECK BEFORE STARTING ENGINE CHECKLIST FLAPS............................................ .. RETRACT PASSENGER BRIEFING................... COMPLETE *See below FLIGHT PLANNING .....................COMPLETED CABIN DOOR.................................... LATCHED SEATS ................................................ LOCKED SEAT BELTS ......................................... FASTEN PARKING BRAKE ....................................... SET *Parking brake is set by pushing on the toe brakes and pulling the parking brake knob out. LANDING GEAR LEVER ......................... DOWN THROTTLES .............................................. IDLE PROPELLERS .......................... FULL INCREASE *If the propellors are feathered on the ground do not attempt to start the engine. MIXTURE .................................. IDLE CUT OFF FRICTION HANDLE ........................ AS DESIRED ALT AIR ............................................... CLOSED COWL FLAPS ........................................... OPEN STABILIATOR & RUDDER TRIM ................... SET FUEL SELECTORS........................................ ON L/R ALTERNATOR SWITCHES ..................... ON E-BATT .................................................... ARM E-VOLTS……………………………………..VERIFY 23.3 *If E-volts are less than 23.3, the voltage can be checked again at the end of the GROUND CHECK. E-volts must not be less than 23.3 prior to flight. *E-Battery usage should be kept to as little as possible to avoid draining the battery. AVIONICS/ELECTR SWITCHES ................... OFF FIN STROBE ............................................... ON *Strobe lights must go on before mags as the strobe light is your warning to others your mags are on, and they should not approach the aircraft. CABIN HEAT .............................................. OFF CIRCUIT BREAKERS .......................... CHECK IN *PASSENGER BRIEF HOW/WHEN TO USE SEATBELTS HOW TO OPEN/CLOSE THE DOOR LOCATION/USE OF EMERGENCY EXITS LOCATION/USE OF EMERGENCY EQUIPMENT AID IN TRAFFIC SCANNING STERILE COCKPIT FOR TAXI/TAKEOFF/LANDING NORMAL START CHECKLIST- COLD ENGINE OIL TEMP BELOW 140°F BATTERY MASTER SWITCH ........................ ON GEAR POSITION INDICATIONS ........... 3 GREEN CAS/PFD MESSAGES .............................CHECK THROTTLE...............................1/4 INCH OPEN PROPELLERS ........................... FULL INCREASE *FUEL PUMP............................................... ON MAG TAGS .................................................OFF *LEFT/RIGHT MAGNETOS ..........................ON *MIXTURE....................PRIME THEN CUT OFF *Priming the engine is done by advancing the mixture to full until fuel flow stabilizes or reaches 3.5 GPH *PROP AREA...................................... CLEAR *STARTER .......................................ENGAGED *No more than 10 sec at a time *Wait 20 seconds between attempts. *No more than 5 start attempts allowed. *If the engine does not start after two attempts with priming, perform flooded engine start procedures. *MIXTURE.................................... ADVANCE *Advance mixture after the engine starts *THROTTLE .................. ADJUST TO 1000RPM *OIL PSI................................................ CHECK *VOLTS/AMPS .................................... CHECK * FUEL PUMP ...................................... ... OFF *FUEL PRESSURE ................................. CHECK REPEAT (*) STEPS FOR SECOND ENGINE NORMAL START CHECKLIST- HOT ENGINE OIL TEMP 140°F OR ABOVE BATTERY MASTER SWITCH ........................ ON GEAR POSITION INDICATIONS........... 3 GREEN CAS/PFD MESSAGES............................. CHECK THROTTLES ............................. 1/2 INCH OPEN PROPELLERS ............................ FULL INCREASE *MIXTURE......................................... CUT-OFF *FUEL PUMP ............................................... ON MAG TAGS .................................................OFF *LEFT/RIGHT MAGNETOS ........................... ON *PROP AREA......................................... CLEAR *STARTER .......................................ENGAGED *No more than 10 sec at a time *Wait 20 seconds between attempts. *No more than 5 start attempts allowed. *If the engine does not start after two attempts with priming, perform flooded engine start procedures. *MIXTURE....................................... ADVANCE *Advance mixture after the engine starts *THROTTLE ...................ADJUST TO LOW RPM *OIL PSI................................................ CHECK * VOLTS/AMPS...................................... CHECK *FUEL PUMP............................................. OFF *FUEL PRESSURE ................................. CHECK IF ENGINE DOES NOT START, ADD A SMALL AMOUNT OF PRIME AND REPEAT THE ABOVE. REPEAT (*) STEPS FOR SECOND ENGINE FLOODED ENGINE START BATTERY MASTER SWITCH ........................ ON GEAR POSITION INDICATIONS........... 3 GREEN CAS/PFD MESSAGES ............................ CHECK THROTTLE ..................................... OPEN FULL PROPELLERS........................... FULL FORWARD MIXTURE .................................. IDLE CUT-OFF *FUEL PUMP ............................................ OFF *LEFT/RIGHT MAGNETOS .......................... ON *PROP AREA.........................................CLEAR *STARTER ....................................... ENGAGED *No more than 10 sec at a time *Wait 20 seconds between attempts. *No more than 5 start attempts allowed. *MIXTURE.......................................ADVANCE *THROTTLE ..................................... …RETARD *OIL PSI................................................ CHECK *VOLTS/AMPS ..................................... CHECK * FUEL PUMP ....................................... .... OFF *FUEL PRESSURE ................................. CHECK REPEAT (*) STEPS FOR SECOND ENGINE NSA Master Checklist Seminoles Fuel Injected Rev 12 pg 9 NSA Master Checklist Seminoles Fuel Injected Rev 12 pg 10 EXTERNAL POWER START BATTERY.................................................... OFF ALTERNATORS .......................................... OFF EXTERNAL POWER ............................. PLUG IN GEAR POSITION INDICATIONS............3 GREEN CAS/PFD MESSAGES .............................CHECK THROTTLE ...............................1/4 INCH OPEN PROPELLERS............................ FULL INCREASE *FUEL PUMP.............................................. ON MAG TAGS ................................................. OFF *MAGNETOS.............................................. ON *MIXTURE .................... PRIME- IDLE CUT OFF *PROP AREA ......................................... CLEAR *STARTER ......................................... ENGAGE *No more than 10 sec at a time *Wait 20 seconds between attempts. *No more than 5 start attempts allowed. *If the engine does not start after two attempts with priming, perform flooded engine start procedures. *MIXTURE ...................................... ADVANCE *Advance mixture after the engine starts *OIL PSI ............................................... CHECK REPEAT (*) STEPS FOR SECOND ENGINE THROTTLE ................. LOWEST POSSIBLE RPM BATTERY MASTER ..... ................................ ON EXTERNAL POWER ..................... DISCONNECT ALTERNATOR ............................................. ON *VOLTS/AMPS .................................... CHECK *Do not attempt flight if there is no indication of alternator output. *FUEL PUMP............................................ OFF *FUEL PRESSURE ................................. CHECK BEFORE TAXI CHECKLIST BATTERY MASTER SWITCH ........................ ON FUEL SELECTORS...... ON,X-FEED FOR 30 SECS AVION MASTER SWITCH............................ ON CIRCUIT BREAKERS .......................... CHECK IN MFD.................CHECK DATABASE CURRENCY *Flight into IFR conditions is not authorized when database is expired FUEL TOTALIZER ............... SYNC OR MANUAL CAS/PFD MESSAGES ............................ CHECK MSG SOFTKEY...................................... CHECK TRAFFIC ................... TEST/VERIFY ADSB IS ON ANNUNCIATOR TEST............................ CHECK STANDBY INSTRUMENTS ..................... CHECK LIGHTS ...................................... AS REQUIRED *PIC will consider exterior lights in accordance with 91.205 for nighttime and low visibility operations to preserve night vision CABIN HEAT/DEFROST .............. AS REQUIRED AUTOPILOT TEST .................... SELF/MANUAL *Autopilot and disengages can be tested manually by setting the Heading (HDG) and Vertical Speed (VS), then moving the heading bug and pushing the Nose Up/Nose Down buttons to see if the yoke moves in the correct direction. *Avoid allowing the controls to go full deflection when performing manual test. TRIM ............................................... NEUTRAL FUEL SELECTORS ............................ VERIFY ON RADIOS ..................................................... SET ATIS/AWOS........................................ OBTAIN ALTIMETER ............................................... SET *If local altimeter setting not received, set field elevation. STANDBY ALTIMETER ............................... SET GPS/NAV/BUGS/AUTO PILOT ................... SET MIXTURE ................................................LEAN *Leaning for ground operations is done by leaning until RPM begins to decrease and enrichening to peak RPM. MFD SET .......................... AIRPORT DIAGRAM TAXI CLEARANCE ............................... OBTAIN *If at a towered airport, obtain IFR clearance as well TRANSPONDER ......................... . …..ALT/1200 TAXI BRIEF ................................ …..COMPLETE *See next page *TAXI BRIEF RUNWAY IN USE RUNWAY LENGTH/REQUIRED ROUTE TO RUNWAY AND RUNUP LOCATION OF HOTSPOTS WHO WILL BE PIC POSITIVE EXCHANGE OF FLIGHT CONTROLS TAXI CHECKLIST TAXI AREA ............................................. CLEAR PARKING BRAKE................................ RELEASE THROTTLE .........................ADVANCE SLOWLY BRAKES/STEERING ............................... CHECK FLIGHT INSTRUMENTS ......................... CHECK INSTRUMENT COCKPIT CHECK ...... COMPLETE RUN UP/GROUND CHECKLIST BRAKES .......................................... SET/HOLD MIXTURE........................................ FULL RICH PROPELLERS ........................... FULL INCREASE ENGINE INSTRUMENTS ........................ CHECK THROTTLE ...................................... 1500 RPM PROPELLERS ......................... FEATHER CHECK *The feather check is done by moving the prop lever all the way to the feather position then immediately back to full forward. Do not allow the RPM to drop more than 500rpm. THROTTLE ...................................... 2000 RPM ENGINE GAUGES ............................. IN LIMITS MAGNETOS.......................................... CHECK *MAX DROP 175RPM, MAX DIFF. 50RPM *Magneto check is done by turning one magneto off and checking to see if all EGT’s rise together. If an EGT were to rise slowly or decrease, it is possibly an indication of a bad or fouled spark plug. *A fouled spark plug can be corrected by leaning the mixture at high rpm to burn off the excess carbon build up. Perform magneto check again after attempting to correct for fouling. *If EGT drops to 0 then aircraft will be downed. ALT AIR .................................. CHECK (~75 RPM) *Avoid prolonged ground operations with the alternate air source as the air is unfiltered. THROTTLE ........................................ 2200RPM PROPELLERS..........................EXERCISE 3 TIMES *Exercising the propellers is done by pulling back on the prop lever until the beginning of resistance andthen returning to full forward. This allows fresh/warm oil into the prop hub. *MAX DROP 300RPM GOVENOR CHECK ......................................FFOD *Governor check is performed by reducing the propeller control until a drop of 100 or 200 rpm is noted, then advancing the throttle to get a slight increase in manifold pressure. RPM should remain the same when throttle is increased. THROTTLE ...................... IDLE (550 TO 650 RPM) RPM/OIL PRESSURE ................................ CHECK FUEL PUMPS ................................................ ON THROTTLE ......................................... 1000 RPM ALTERNATE STATIC ................................. CHECK *Alternate static is checked by opening the alternate static port underneath the panel on the pilot side and noting an increase on the VSI. Alternate static should be closed prior to take off. If no change is observed on VSI, open door or window and perform test again. FRICTION HANDLE ..................................... SET IFR CLEARANCE ................................... ACQUIRE *Consider weather and traffic for determining if a ground or airbourne clearance is appropriate. TAKE OFF BREIFING ......................... COMPLETE IF E VOLTS INDICTIONS LESS THAN 23.3 VOLTS DURING BEFORE STARTING ENGINE CHECKLIST E-BATT .................................................... ARM AVION MASTER SWITCH .......................... OFF ALTERNATORS .......................................... OFF BATT MASTER .......................................... OFF E VOLTS INDICATION… .......... 23.3 VOLTS MIN IF E VOLTS LESS THAN 23.3, DETERMINE CAUSE AND CORRECT ISSUE PRIOR TO FLIGHT. NSA Master Checklist Seminoles Fuel Injected Rev 12 pg 12 NSA Master Checklist Seminoles Fuel Injected Rev 12 pg 11 IF E VOLTS GREATER THAN OR EQUAL TO 23.3 VOLTS: BATT MASTER SWITCH .............................. ON ALTERNATORS ........................................ ..ON AVION MASTER SWITCH ......................... ..ON BEFORE TAKE OFF CHECKLIST FLIGHT CONTROLS .......... FREE AND CORRECT FLIGHT INSTRUMENTS .................. CHECK/SET ENGINE INSTRUMENTS ....................... CHECK FUEL QUANTITY ........................... SUFFICIENT PROPELLERS........................... FULL INCREASE MIXTURE......................................... FULL RICH *If density altitude on the ground is 5000ft or greater, lean to peak RPM. ALT AIR……………………………………………..CLOSED COWL FLAPS .......................................... OPEN FLAPS ........................................................ SET TRIM ......................................................... SET FUEL SELECTORS ........................................ ON CAS/PFD MESSAGES ............................ CHECK TRANSPONDER .................. CODE/ALT VERIFY DEPARTURE BRIEFING.................. COMPLETE *Initial heading/altitude/departure out of pattern ELECTRIC FUEL PUMPS ............. ................ ON PITOT HEAT............................... AS REQUIRED *Limit pitot heat on the ground to no more than 3 minutes. LANDING LIGHT ......................................... ON STROBE LIGHTS ................................. FULL ON NAV LIGHTS .............................. AS REQUIRED DOOR/WINDOW ................................ CLOSED TIME OFF ............................................... NOTE AUTOPILOT ................................ DISCONNECT TAKE OFF CLEARANCE ....................... OBTAIN FINAL APPROACH ....................... AREA CLEAR PARKING BRAKE................................RELEASE CLIMB CHECKLIST - ABOVE 1000’ AGL LANDING GEAR ............... ..........................UP FLAPS............................... VERIFY RETRACTED MIXTURE ........................................ FULL RICH ELECTRIC FUEL PUMPS .............................. ON COWL FLAPS ..............................AS REQUIRED CRUISE POWER .................. 25”MP 2500 RPM CRUISE CLIMB AIRSPEED .................. 105 KIAS *Climbs should be done at cruise climb as it results in cooler engine temperatures and better forward visibility. AUTO PILOT...................................... ENGAGE DEPARTURE AREA................................. CLEAR PRE-MANUEVER CHECKLIST MIXTURE .................................................. SET ELECTRIC FUEL PUMP ................................ ON FUEL SELECTORS........................................ ON ALL LIGHTS ................................................ ON ALTITUDE....................................... MIN. SAFE CLEARING TURNS ......................... COMPLETE *Performed by two 90⁰ turns or one 180⁰ turn to look for traffic, obstacles, and to become more visible to other traffic. The proper scanning technique is to break the area into sections and look in each section for 5-7 seconds. RADIO CALL .................................. COMPLETE POST MANUEVER CHECKLIST LANDING/RECOG LIGHT ........................... OFF ELECTRIC FUEL PUMPS ............................. OFF FUEL SELECTORS........................................ ON ENGINE GUAGES ................................. CHECK *Consider an appropriate time to conduct approach and landing checklist CRUISE CHECKLIST CRUISE POWER ......................................... SET PROPELLERS ..................................... RPM SET COWL FLAPS ............................ AS REQUIRED *Cowl flaps should be closed during cruise to reduce drag and increase airspeed. If CHT’s reach 400⁰F, then cowl flaps should be opened to cool the engine down. TRIM......................................... AS REQUIRED MIXTURE.......................................... ADJUST *Mixture should be leaned anytime above density altitude 5000 ft to best performance or 100⁰F Rich of Peak. Once mixture is set, monitor EGT gauges for any changes. LANDING/RECOG LIGHT............................OFF FUEL PUMPS .............................................OFF *Consider an appropriate time to conduct approach and landing checklist APPROACH AND LANDING CHECKLIST WEATHER .......................................... OBTAIN INSTRUMENTS ................................... ...... SET RADIOS ..................................................... SET ENVIRONMENT ..................................... BRIEF *Runway of intended use, patten entry, or approach brief SEATS/SEATBELTS ............... LOCKED/FASTEN FUEL PUMPS ............................................. ON FUEL SELECTORS ....................................... ON COWL FLAPS ...................................... CLOSED *Cowl flaps should be closed when operating at reduced power settings such as descent to keep engine warm. HEATER ............................. OFF/AS REQUIRED *When turning off the heater, it is required to allow the heater to cool off by leaving the air intake open 15 seconds in the air or by activating the fan for 2 minutes on the ground. GEAR (BELOW 140 KIAS) .................... DOWN GEAR POSITION INDICATOR ............. 3 GREEN NOSE GEAR ........................... VERIFY MIRROR MIXTURES ...................................... FULL RICH PROPELLER ............................FULL INCREASE ALT AIR .................................... AS REQUIRED AUTOPILOT ............................... DISCONNECT GO AROUND CHECKLIST (DUAL ENGINE) MIXTURES…………………………………….FULL RICH PROPELLERS………………………….FULL INCREASE THROTTLE……………………………………FULL OPEN CONTROL WHEEL………….. …..BACK PRESSURE TO OBTAIN + CLIMB FLAPS………………………………………………….……UP GEAR……………………………………………………..…UP COWL FLAPS…………………………...AS REQUIRED AFTER LANDING CHECKLIST RADIO CALL ............................ REPORT CLEAR FLAPS ............................................... RETRACT COWL FLAPS .......................................... OPEN ALT AIR……………………………………………..CLOSED ELECTRIC FUEL PUMPS ............................. OFF STROBE LIGHT ........................................... FIN LANDING LIGHT ........................ AS REQUIRED *Lights should be kept at a minimum at all times on the ground to protect night vision. Additional lights will be used if required for night or low-visibility operations or as preferred by PIC. PITOT HEAT............................................... OFF CABIN HEAT ........................... OFF/FAN (2MIN) *When turning off the heater, it is required to allow the heater to cool off by leaving the air intake open 15 seconds in the air or by activating the fan for 2 minutes on the ground. TRANSPONDER ............................... ALT/1200 FLIGHT PLAN ...................................... CLOSED MIXTURE………………………………………TAXI LEAN MFD ................................. AIRPORT DIAGRAM TAXI CLEARANCE ............................... OBTAIN NSA Master Checklist Seminoles Fuel Injected Rev 12 pg 13 NSA Master Checklist Seminoles Fuel Injected Rev 12 pg 14 ENGINE SHUTDOWN CHECKLIST PARKING BRAKE........................................ SET VENT FAN/HEATER/DEFROST ................... OFF THROTTLE .......................................1000 RPM AVION MASTER ........................................ OFF EMER BATT ............................................... OFF ALTERNATORS .......................................... OFF FUEL PUMPS............................................. OFF ELECTRICAL EQUIPMENT .......................... OFF THROTTLE ................................................ IDLE MIXTURE .................................. IDLE CUT-OFF MAGNETOS .............................................. OFF INTERIOR/EXTEROR LIGHTS ..................... OFF BATTERY MASTER ..................................... OFF STANDBY INST ............... VERIFY SHUT DOWN *Do not push any buttons on the standby instrument as this will cause it to remain on. Verify that the instrument indicates it is in the shutdown process. PARKING BRAKE ............................... RELEASE POST FLIGHT INSPECTION HOBBS/TACH .....................................RECORD *Send a photo of the tach and hobbs time to dispatch at (507)508-0706 CABIN INTERIOR .................................. CLEAN MIXTURE .......................................... CUT OFF MASTER SWITCHES ................................... OFF MAGNETOS ............................................... OFF MAG TAGS .................................................ON WINDOW........................................... CLOSED DOOR .................................................... CLOSED RIGHT WING CONDITION… .................. CHECK *Check for signs of birdstrike *Check for signs of propstrike *f there is a birdstrike the aircraft must be downed right away *A kit is located behind the pilot seat and must be filled out and accompanied by a safety report CHOCKS ............................................. INSERT NOSE SECTION CONDITION..................CHECK *Check for signs of propstrike PROP BLANKETS ....................................... ON ENGINE BLANKETS .................................... ON *Blankets will be used when average ambient temperature is below 40˚ F LEFT WING CONDITION ....................... CHECK *Check for signs of birdstrike FUSELAGE/EMPANNAGE… ................... CHECK *Check for signs of tailstrike TIE DOWN ........................... AS NECCESSARY DISCREPENCIES/SQUAWKS ............... REPORT This page is intentionally left blank NSA Master Checklist Seminoles Fuel Injected Rev 12 pg 15 NSA Master Checklist Seminoles Fuel Injected Rev 12 pg 16 Actions to Take ENGINE FAILURE – TAKEOFF Sudden yawing motion, low manifold pressure, low RPM If sufficient runway remains for a complete stop .............................................. .... Land............................................... Straight Ahead Directional Control..................................Maintain ..................................................... ............................................... If gear is in transit or UP and the decision is made to continue Directional Control ................................Maintain Airspeed…………………………….At least Vyse (88kts) Mixture .................................................. Full Rich Propellers ........................................ Full Increase Throttles ...............................................Full Open .............................................................. ............................................................... Fuel Selectors................................................. On ................................................... Inop Engine ................................. Identify/Verify *Identification of the failed engine can by done by noting a reduction in MP, RPM, CHT, and EGT or by determining which foot is not applying rudder pressure while maintaining desired heading. *Verification of failed engine is done by reducing throttle of suspected failed engine and noting the absence of engine or aircraft response. Throttle (inop) ............................................. Close Propeller (inop) ....................................... Feather Mixture (inop) .......................................... Cut-Off Bank ................................. 2˚-3˚ into Oper Engine Climb Speed ...................................... Vyse (88kts) Cowl Flaps (inop)...................................... Closed Magnetos (inop) ............................................Off Fuel Pump (inop) ...........................................Off Alternator (inop) ............................................Off Fuel Selector (inop) ........................................Off LAND AS SOON AS PRACTICAL Indications Smoke, smell, heat in the cabin, high CHT/EGT/oil temperatures, visible flames Actions to Take AFFECTED ENGINE Fuel Selector ............................................... Off Throttle ................................................... Close Propeller ............................................. Feather Mixture ................................................ Cut-off Cowl flaps .............................................. .Open Affected engine………………..Secure (Pg 19) *If fire persists, begin emergency descent (Pg 15) LAND AS SOON AS POSSIBLE ENGINE FIRE – IN FLIGHT Indications Smoke, heat, flames coming from panel, heat in the cabin Actions to Take Emergency Battery ........................ Verify Arm Battery Master......................................... .Off Alternators .............................................. ..Off Vents .................................................... ..Close Cabin Heat ................................................ .Off *If the fire persists, locate and use portable fire extinguisher located behind and between two front seats. *The fire extinguisher uses halon, which will remove the oxygen from the area to put out the fire. *Landing gear must be lowered manually LAND AS SOON AS POSSIBLE ELECTRICAL FIRE ENGINE FIRE DURING START Indications Smoke/flames coming out of engine compartment Actions to Take Mixture ............................................ ... Cut Off Throttle ........................................... Full Open Starter ............................ .Continue to Engage Fuel Selectors............................................ Off Fuel Pumps ............................................... Off Fire Extinguisher ...................................... Use Aircraft ............................................ Evacuate *The fire extinguisher uses halon which will remove the oxygen from the area to put out the fire. EMERGENCY DESCENT Actions to Take Alt Air ..................................................... Open Throttles ................................................ Closed Propellers .....................................Full Increase Mixture ........................................As Required Gear ............................. Down (Below 140kts) Airspeed ..............................................135kts Bank ..........................................................45˚ Below 75kts or Gear Down Indications Sudden yawing motion, low manifold pressure, Low RPM Actions to Take Throttles ........................ Immediately Closed Brakes ......................................... As Required Directional Control .......................... Maintain *Use rudder and aileron controls to maintain desired heading If Insufficient Runway Remains Brakes ............................................ Maximum Mixtures ........................................ .... Cut-Off Fuel Selectors ........................................... Off Magnetos L/R ...........................................Off Battery Master.......................................... Off Directional Control .......................... Maintain Obstacles............................................... Avoid NSA Master Checklist Seminoles Fuel Injected Rev 12 pg 17 NSA Master Checklist Seminoles Fuel Injected Rev 12 pg 18 This page is intentionally left blank Indications Reduced airspeed, rapid rotation, altimeter rapidly descending, turn coordinator full deflection Actions to Take Throttles ......... ..................................... Closed Rudder ........... Full opposite to direction of spin Control Wheel ............................ Full forward Ailerons ..............................................Neutral Rudder ........ Neutralize when Rotation Stops Control Wheel ........... Smooth back pressure INTENTIONAL SPINS ARE PROHIBITED ENGINE FAILURE DURING FLIGHT Sudden yawing motion, low manifold Actions to Take Airspeed ........................................Vyse (88kts) Directional Control ....................... ..... Maintain Mixture ................................................. Full Rich Propellers ....................................... Full Increase Throttles ..............................................Full Open .............................................................. ............................................................. Inop Engine ................................ Identify/Verify *Identification of failed engine can be done by noting a reduction in MP, RPM, CHT, and EGT or determining which foot is not applying rudder pressure while maintaining desired heading. *Verification of failed engine is done by reducing throttle of suspected failed engine and noting the absence of engine or aircraft response. FIX-BEFORE SECURING ENGINE ......................................... Fuel Selector .................................... On/X-Feed Fuel Pump ..................................................... On Mixture ................................................. Full Rich ......................................................... Left Mag (inop) .............................. Off, then On Right Mag (inop) ............................ Off, then On Oil Temperature ........................................ Check Oil Pressure ............................................... Check On Operating Engine Power .............................................. As Required ................................................ Fuel Pump ....................................... As Required Cowl Flap ........................................ As Required Bank . .............................. 2˚-3˚ into Oper Engine Airspeed……………………………at least Vyse (88kts) Electrical Load ......................................... Reduce LAND AS SOON AS PRACTICAL NSA Master Checklist Seminoles Fuel Injected Rev 12 pg 19 NSA Master Checklist Seminoles Fuel Injected Rev 12 pg 20 ENGINE ROUGHNESS Indications Engine sputtering, unusual noise or vibrations Actions to Take ON AFFECTED ENGINE Alt Air ........................................... ……..Open If roughness continues after 1 min Alt Air ............................ ........... Close Mixture…………….Adjust for max smoothness Fuel Pump ................................................. On Engine Gauges .................................... Check Left Magneto ........................... ...Off, then On Right Magneto......................... ...Off, then On *If at any time the engine begins to run smoothly, maintain settings that provide maximum smoothness. ENGINE SECURING PROCEDURE Actions to Take ON THE INOPERATIVE ENGINE Throttle .............................................. Closed Propeller........................................... Feather Mixture ..............................................Cut-Off Cowl Flaps ........................................... Closed Magnetos ................................................. Off Fuel Pump .................................................Off Alternator Switch ..................................... Off Fuel Selector ............................................ Off Electrical Load ................................... Reduce LAND AS SOON AS PRACTICAL ONE ENGINE INOP LANDING Actions to Take Inoperative Engine .....................Secure Seat Belts .......................................Fastened OPERATIVE ENGINE Fuel Selector ............................................ On Mixture .......................................... .Full Rich Propeller ................................ ..Full Increase Fuel Pump ................................................ On Cowl Flaps ...................... …………As required Approach......................................... Normal WHEN LANDING IS ASSURED Gear ................................................... Down Flaps ................................... …25˚ (2 nd notch) Final Approach Speed ......................... 90kts *As power is reduced, the aircraft will yaw in the direction of the operating engine. Under some conditions, aircraft single engine climb performance and obstacle clearance may make a single engine go around impossible. ONE ENGINE INOP GO-AROUND Actions to Take Mixture (op engine) ..........................Full Rich Propeller (op engine) ................ Full Increase Throttle ..........................Smoothly Advance Airspeed………………………at least Vyse (88kts) Flaps ........................ Retract Incrementally Gear .......................................................... Up Bank ........................ ..2˚-3˚ into Good Engine Rudder ................................... 1/2 trapezoid Cowl Flaps ................................. As Required UNFEATHERING PROCEDURES Actions to Take ON INOPERATIVE ENGINE Fuel Selector ............................................ On Magnetos ................................................. On Fuel Pump ................................................ On Throttle ............................ …….Open ¼ inch Propeller .............................. ….Full increase * If engine is stationary (not rotating) after 7 seconds, starter assist is required. Mixture ............Advance (after prop rotation) Throttle ................... ……<15 MP until warm *Keep the MP of the restarted engine as low as practical until the CHTs are above 200˚F Alternator ................................................ On If restart is not successful, secure inoperative engine (pg 19) UNFEATHERING PROCEDURES/STARTER ASSISTED Actions to Take ON INOPERATIVE ENGINE Fuel Selector ............................................. On Magnetos .................................................. On Fuel Pump ................................................. On Throttle .............................. …...Open ¼ inch Propeller ........... …Increase to cruise setting Mixture ................................. ………..Full rich Eng start ........Engage until prop windmills Throttle .................... <15 MAP until warm *Keep the MP of the restarted engine as low as practical until the CHTs are above 200˚ f Alternator ................................................ On LOW/HIGH OIL PRESSURE Indications Master warning, triple chime, flashing red oil pressure Actions to Take ON AFFECTED ENGINE WITH LOW OIL P Throttle ......................................... Minimum Propeller ....................................... Decrease *If accompanied by normal oil temp LAND AS SOON AS PRACTICAL *If low oil pressure is accompanied by high oil temperature, secure the affected engine and LAND AS SOON AS POSSIBLE *Loss of oil pressure can indicate oil exhaustion which will result in a serious emergency and severe engine damage. If oil is depleted, the engine will seize and if feathering is not initiated above 950 RPM the propeller may not feather. HIGH OIL TEMP/CHT Indications L ENG CHT or R ENG CHT CAS message or flashing red oil temperature, master warning, triple chime Actions to Take ON AFFECTED ENGINE Cowl Flaps ............................................Open Mixture .......................................... Enrichen Power ............................................... Reduce Airspeed ......................................... Increase *High oil temperature or CHT’s can be caused by low oil quantity. *Monitor oil pressure gauge and if low… LAND AS SOON AS PRACTICAL NSA Master Checklist Seminoles Fuel Injected Rev 12 pg 22 NSA Master Checklist Seminoles Fuel Injected Rev 12 pg 21 LOSS OF FUEL FLOW Indications Fuel flow gauge abnormally low Actions to Take AFFECTED ENGINE Fuel Pump ............................................. On FUEL QUANTITY Indications L FUEL QTY / R FUEL QTY L FUEL QTY / R FUEL QTY Master Warning/Caution, Triple/Double Chime Actions to Take X-Feed.......................................As Necessary *If one tank has low fuel quantity LAND AS SOON AS PRACTICAL *If both tanks have low fuel quantity LAND AS SOON AS POSSIBLE *Low fuel caution is activated at 10 gallons remaining in either tank *Low fuel warning is activated at 5 gallons remaining in either tank LANDING GEAR UNSAFE Indications CHECK GEAR CAS Messages and Aural Alert Actions to Take Gear .................................................... Down Gear Position .................................. 3 Green LANDING GEAR MALFUNCTION/MANUAL EXTENSION Indications GEAR SYS or GEAR SYS, master warning/caution, triple/double chime, landing gear indication of ● Actions to Take Circuit Breaker ....................................... Check Battery Master ........................................... On Alternators .............................................. Check Airspeed ................................ Less than 100kts Gear Knob .............................................. Down Emergency Gear Knob .............................. Pull Gear Indications ................................ 3 Green *Leave emergency gear knob out until the airplane has been put on jacks to check the gear. HYDRAULIC PUMP DOES NOT DEACTIVATE Indications HYDR PUMP ON CAS message, master warning, triple chime Actions to Take Gear Pump Circuit Breaker...................... Pull (Row 2, Col 12) * Prior to landing, reset the gear pump circuit breaker to bring down the landing gear. *If breaker opens, complete manual extension of landing gear (pg 21) HYDRAULIC PUMP DOES NOT ACTIVATE Indications Gear does not change position after moving gear lever Actions to Take Gear Knob…………Return to original position Gear Pump Circuit Breaker .................. Reset (Row 2, Col 12) *After pulling a circuit breaker, wait 10 seconds for a cool off period before pushing circuit breaker back in. * Do not reset the circuit breaker a second time. Gear Knob............................................ Reset *If landing gear is still up, perform manual gear extension. If gear is still down, keep airspeed below VLE (140kts) SINGLE ALTERNATOR FAILURE Indications L ALT FAIL or R ALT FAIL low alternator amps, master warning, triple chime Actions to Take Verify Failure ..................................... Alt amps Electrical Load ........................ 65 amps or less Alternator Switch ...................................... Off Alternator Field Circuit Breaker .............. Reset (Row 2, Col 15/16) *After pulling a circuit breaker, wait 10 seconds for a cool off period before pushing circuit breaker back in. Do not reset the circuit breaker a second time. Alternator ................................................. On IF ALTERNATOR IS STILL FAILED Alternator ................................................. Off Alternator Amps ...............Less than 65 amps DUAL ALTERNATOR FAILURE Indications L ALT FAIL and R ALT FAIL Low alternator amps, master warning, triple chime Actions to Take Verify Failure.............................. ..Alt amps Alternator Switch ............................... …Off Alternator Field Circuit Breaker………Reset (Row 2, Col 15/16) *After pulling a circuit breaker, wait 10 seconds for a cool off period before pushing circuit breaker back in. Do not reset the circuit breaker a second time. Alternator ........................................ ……On IF ONLY ONE ALTERNATOR RESETS Operating Alternator ........................ …On Failed Alternator ................................ ..Off Alternator Amps............ Less than 65 amps IF NEITHER ALTERNATOR RESETS Alternators .................................. Both Off Following Circuit Breakers ..................Pull Non Ess Bus........................... (Row 1, Col 1) Lighting Bus........................... (Row 1, Col 2) Avionics Bus .......................... (Row 1, Col 3) Avionics Master ................................... Off Emergency Battery .................... Verify Arm EXIT AND AVOID IMC AS SOON AS PRACTICAL TO ENSURE 30 MINS OF BATTERY LIFE Battery Amps............ …………-20 Amps Max Pitot Heat.......................... Limit to 15 mins Com Radio .......................... Limit to 3 mins *With both alternators failed, the main battery is the primary source of power. NSA Master Checklist Seminoles Fuel Injected Rev 12 pg 24 NSA Master Checklist Seminoles Fuel Injected Rev 12 pg 23 COMPLETE ELECTRICAL FAILURE/EMERGENCY Indications EMERG BATT ON, E-Volts Indication on PFD Actions to Take Emergency Battery ................... Verify arm Standby Inst.................................Verify on Aircraft Control........................ Use standby Battery Master ..................................... Off Alternators.................................... ……..Off LAND AS SOON AS POSSIBLE FLASHING RED E-VOLTS INDICATES THAT THE EMERGENCY BATTERY IS ALMOST DEAD AND COMPLETE ELECTRICAL FAILURE IS IMMINENT *All lights and the landing gear pump is now inoperative. *Only the following equipment is operational on the emergency bus: PFD, COM 1, NAV 1, audio panel, engine instruments, standby instruments, avionics lighting/dimming. PFD FAILURE Indications PFD Screen goes black Actions to Take Standby Instruments .....................Verify On Aircraft Control ........................ Use Standby Display Backup .............. .Red Button/Push Com 2.................... Activate (Com 1 is inop) Nav 2 ...................... Activate (Nav 1 is inop) Com 2/Mic ................ Select on Audio Panel EXIT AND AVOID IMC AS SOON AS PRACTICAL * Auto Pilot is now Inoperative. MFD FAILURE Indications MFD screen goes black Actions to Take Display Backup .................Red Button/Push Com 1...................... Activate (Com 2 is inop) Nav 1.........................Activate (Nav 2 is inop) EXIT AND AVOID IMC AS SOON AS PRACTICAL *PFD should automatically revert to revisionary mode with MFD failure. Pushing the display backup button ensures this transition. *The following Equipment are Inoperative with an MFD Failure: COM 2, NAV 2, GPS 2, XM, ADF, DME, ESP. AHRS FAILURE Indications Sky/Ground presentation removed, course pointer straight up, Red X’s and amber text on all attitude and heading indicators Actions to Take Standby Instruments……………Verify on/use PFD Messages ................................ Consider AHRS Circuit Breaker ........................... Reset (Row 2, Col 8) *After pulling a circuit breaker, wait 10 seconds for a cool off period before pushing circuit breaker back in. Do not reset the circuit breaker a second time. EXIT AND AVOID IMC AS SOON AS PRACTICAL *Course information and Traffic Alerts are still available with an AHRS Failure. *Autopilot will be inoperative if AHRS remains inoperative. ADC FAILURE Indications Red X’s and amber text on all Airspeed, Altitude and Vertical Speed indicators Actions to Take Standby Instruments……………..Verify on/use PFD Messages .................................Consider ADC Circuit Breaker ............................. Reset (Row 2, Col 7) *After pulling a circuit breaker, wait 10 seconds fora cool off period before pushing circuit breaker back in. Do not reset the circuit breaker a second time. EXIT AND AVOID IMC AS SOON AS PRACTICAL *Traffic and Autopilot will become inoperative during ADC Failure. ERRONEOUS/LOSS OF ENGINE SYSTEMS DISPLAY Indications Yellow X’s over affected engine indications or fuel displays Actions to Take GEA Circuit Breaker ..............................Reset (Row 2, Col 3) *After pulling a circuit breaker, wait 10 seconds for a cool off period before pushing circuit breaker back in. Do not reset the circuit breaker a second time. *Set power based on throttle lever position, engine sound and speed. Use known power settings from POH for approximate fuel flow values. *All engine, electrical, and fuel indications are now invalid. LAND AS SOON AS PRACTICAL NSA Master Checklist Seminoles Fuel Injected Rev 12 pg 26 NSA Master Checklist Seminoles Fuel Injected Rev 12 pg 25 . ELECTRIC PITCH TRIM FAILURE Indication Red boxed PTRM on PFD Actions to Take Autopilot .................................. Disconnect COOLING FAN FAILURE Indications AV FAN FAIL or PFD FAN FAIL or MFD FAN FAIL CAS messages Actions to Take Battery Master ..............................Verify On Alternator ......................................Verify On *If messages are displayed on the ground, do not fly. *If message is displayed while in flight, it is permissible to continue the flight, fix the issue prior to next flight *Dim displays COMMUNICATIONS FAILURE Indications Inability to communicate/receive on Com 1 or Com 2 Actions to Take Volume Knobs ................................... Check Headset Jacks ........................Troubleshoot *Verify co-pilot side, check connection Frequency ......................................... Verify IF COMMUNICATIONS ARE STILL FAILED Audio panel circuit breaker ....................Pull (Row 2, Col 9) EXIT AND AVOID IMC AS SOON AS PRACTICAL *When power is lost to the Audio Panel, a failsafe connection activates between the pilot headset and Com 1. PITOT HEAT FAILURE Indications PITOT HEAT FAIL CAS message, master caution, double chime Actions to Take Pitot Heat ................................................. Off Pitot Heat Circuit Breaker .................... Reset (Row 2, Col 2) *After pulling a circuit breaker, wait 10 seconds for a cool off period before pushing circuit breaker back in Do not reset the circuit breaker a second time. Pitot Heat .................................................. On If pitot heat is still inop EXIT AND AVOID IMC AS SOON AS PRACTICAL DUAL GPS FAILURE Indications Amber DR on HSI and Amber DR on moving map display Actions to Take Navigation.................. Use alternate source (VOR, ILS, LOC, Pilotage/Dead Reckoning) *DR mode (dead reckoning)-is active when in enroute mode (>30nm from destination airport in flight plan) and uses heading, airspeed, and last known position and can be used for 20 minutes. LOSS OF NAVIGATION INFORMATION Indications Amber VOR, VAPP, GPS, BC, LOC, or GS flashing on PFD Actions to Take Autopilot .............Select another lateral mode NAV source ......... .............................. Identify Autopilot ...................................... Select NAV If on instrument approach in IMC…Go missed AUTOPILOT MALFUNCTION Indications An unexpected roll or pitch from the desired flight path, possible flight director command deviations from desired aircraft attitudes and possible autopilot disconnect with red AFCS annunciation, red or amber A/P annunciation on PFD. Actions to Take Control Wheel ...........................Grasp Firmly Attitude Indicators ..................... Cross Check Autopilot ....................................... Disconnect Pitch trim.............................................. Retrim Autopilot Circuit Breaker ......................... Pull (Row 3, Col 2) Autopilot ........................... Do not re-engage AUTOMATIC AUTOPILOT DISCONNECT Indications Flashing red or white A/P on PFD and aural disconnect tone Actions to Take Autopilot ..................................... Disconnect Pitch trim........................................... Retrim ELECTRIC PITCH TRIM RUNAWAY Indication An unexpected pitch deviation from the desired flight path and red PTRM annunciation Actions to Take Autopilot ............................. Disconnect Control Wheel .................. Grasp Firmly Attitude Indicators .............Cross Check Autopilot .............................. Disconnect Pitch trim circuit breaker .............. Reset (Row 3, Col 2) Trim ....................................Set Manually AUTOPILOT OVERSPEED Indications MAXSPD annunciation at top of Airspeed tape Actions to Take Throttle .......................... ................. Reduce Autopilot ........................ Disconnect if need Pitch ........................................................ Up *In the event of an overspeed, the autopilot will pitch the aircraft nose up to slow the aircraft down NSA Master Checklist Seminoles Fuel Injected Rev 12 pg 27 NSA Master Checklist Seminoles Fuel Injected Rev 12 pg 28 EMERGENCY EXIT Actions to Take Thermoplastic Cover……………………Remove Emergency Exit Handle…………Pull Forward Window ............................... ………Push Out AUTOPILOT UNDERSPEED Indications MINSPD annunciation at top of airspeed tape and USP ACTIVE annunciation on PFD Actions to Take Autopilot .................... Disconnect if need Throttle .......................................Increase Flap/Gear................................... Consider AUTOPILOT OUT-OF-TRIM Indications Amber, ← AIL, AIL→, ↑ELE or ↓ELE on PFD Actions to Take IF← AIL or AIL→ annunciation ......... Verify Slip/Skid indicator centered If↑ELE or ↓ELE annunciation……Suspect elevator trim issue Control Wheel .................... Grasp Firmly Autopilot ................................ Disconnect Pitch Trim .................................... Retrim Autopilot .................... Re-Engage if able AUTOPILOT PREFLIGHT TEST FAILURE Indications PFT on PFD Actions to Take Autopilot Circuit Breaker .......................... Pull (Row 3, Col 2) Pitch Trim Circuit Breaker ........................ Pull (Row 3, Col 1) *Reset both circuit breakers simultaneously *After pulling a circuit breaker, wait 10 seconds for a cool off period before pushing circuit breaker back in. * Do not reset the circuit breaker a second time. ONLY ATTEMPT ONCE OPEN DOOR Actions to Take Airspeed ............................. Less than 82kts Cabin Vents ........................ .............Closed Storm Window ................................... Open Door.................................................... Latch STARTER ENGAGED Indications L START ENGD or R START ENGD CAS message, master warning, triple chime Actions to Take Throttle............................................. Reduce Eng Start Circuit Breaker .................. ...... Pull (Row 1, Col 12) LAND AS SOON AS PRACTICAL *If on the ground, immediately shut down the engine. CARBON MONOXIDE INDICATION Indications CO LEVEL HIGH CAS message, master warning, triple chime Actions to Take CO Reset .......................................... Push *Button can be found on engine information page on MFD. IF WARNING CONTINUES Heater ...................................... Shut Off Vents ............................................. Open *CAS msg remains until CO level drops 50PPM LAND AS SOON AS PRACTICAL ABNORMAL FLIGHT DIRECTOR MODE TRANSITIONS Indications Flashing lateral or vertical modes on PFD Actions to Take Autopilot Mode ..... Select different modes *If on an instrument approach, disconnect the autopilot and hand fly the approach. PROPELLER OVERSPEED Indications Excessively/Abnormally High RPM Actions to Take AFFECTED ENGINE Throttle ............................................Reduce Propeller........................................... Reduce Oil Pressure .........................................Check Airspeed ........................................... Reduce Throttles ............................ Below 2700 RPM *The propeller overspeed is usually caused by a malfunction in the propeller governor which allows the blades to rotate to full low pitch. HEATER OVERHEAT Indications HTR OVERHEAT CAS message, master warning, triple chime Actions to Take Cabin Heat ............................................... Off *An overheat safety switch in the heater unit has deactivated the heater. Resetting the overheat safety switch can only be done on the ground by removing the nose cover.