How to Use the Checklist:

Checklists

= Surface-7,000 = Surface- 12,000 = UAV OPS area = 7,500-12,000

How to Use the Checklist: When using the following checklist there are a few items to note: 1. Verify that you are using the proper checklist for the appropriate aircraft. 2. Bold Items are immediate action. 3. Bold Items are verbal callouts. 4. Italicized are information items. 5. ALL CAPS is action to be performed. 6. Underlined is an action to be completed when parameters have been met. 7. Verify that you have the MOST CURRENT REVISI. 8. All checklists are arranged in the following order: some items might be combined for brevity. Preflight Normal Maneuvers Abnormal (Pink) 9. Boxed checklists - - are performed as Read and Do checklists while dashed checklists - - are performed from memory. 10. ALWAYS WITH THE AFM if you are in doubt about anything. 11. Lines are included under checklist headers to identify the key tasks that must be accomplished before continuing with the checklist. DA-40F LISTS DA-40CS LISTS DA-42 LISTS Name: Phone#

DA-40F PREFLIGHT LIST DA 40F Flight Deck Weather, Flight Plan, Weight & Balance Aircraft Documents & Inspections CURRENT Flight Control Lock REMOVE Ignition Switch Electrical Equipment ALL Emergency Battery GUARDED ELT ARMED/INDICATOR Circuit Breakers IN Control Lever IDLE CUT IDLE Carburetor Heat OPERATI Flight Controls FULL DEFLECTI UP Lights & Pitot Heat OPERATI Lights & Pitot Heat G1000 Databases CURRENT Fuel Quantity Trim OPERATI Fire Extinguisher CHARGED & SECURED Baggage STOWED Left Wing Rear Ventilation Intake Left Gear Strut Wheel & Tire Chocks REMOVE Opening Around Tank Drain Tank Drain FUEL QUALITY Wing Surface 2 Stall Strips Stall Warning REMOVE COVER & Tank Filler & FUEL QUANTITY Fuel Tank Vents Pitot-Static Probe REMOVE COVER & Wing Tie-Down REMOVE Wing Tip 2 Static Wicks Aileron Aileron Paddle Hinges & Safety Pins Push Rod, Bracket, & Bonding Straps Trim Tab (don t touch!) Flap Counter Weight Hinges & Safety Pins Push Rod, Bracket, & Bonding Straps Torsion Tube & Bonding Strap Main Gear FROM AFT Brakes & Hydraulic Line Brake Pads CFIRM SUFFICIENT THICKNESS Left Fuselage Rear Cabin Door & Window Rear Door Pins Antennas Fuselage Surface Tail Skid Tail Tie-Down REMOVE Rudder Cables & Eyelets (left & right) Bottom Hinge, Mount, & Bonding Straps Static Wick Trim Tab (don t touch!) Top Hinge 5 DA-40F LISTS DA-42 LISTS ARROW LISTS

DA-40F PREFLIGHT LIST ARROW LISTS DA-42 LISTS DA-40F LISTS Elevator Hinges 2 Static Wicks Trim Tab, Linkage, Bolts & Safety Wire Lightening Discharge Right Fuselage Tail Skid & Lower Fin Fuselage Skin Rear Window Flap Main Gear FROM AFT Brakes & Hydraulic Line Brake Pads CFIRM SUFFICIENT THICKNESS Torsion Tube & Bonding Strap Hinges & Safety Pins Push Rod, Bracket, & Bonding Straps Counter Weight Aileron Hinges & Safety Pins Push Rod, Bracket, & Bonding Straps Aileron Paddle Right Wing 2 Static Wicks Wing Tip Wing Tie-Down REMOVE Fuel Tank Vents Tank Filler & FUEL QUANTITY Wing Surface 2 Stall Strips Opening Around Tank Drain Tank Drain FUEL QUALITY Right Gear Strut Wheel & Tire Chocks OAT Probe Underside REMOVE Nose Gear/Shock Absorber Cowl Exit Oil Cooler Gascolator DRAIN & FUEL QUALITY Nose Right Front Ventilation Intake Oil Level (recommended 6 qts.) Cowling & Fasteners Spinner & Fasteners Propeller Engine Cooling Intakes Engine Intake Air Filter Heater Air Intake Oil Cooler Intake Alternator & Battery Case Blast Tubes Left Front Ventilation Intake Nose Gear & Wheel Front Canopy AND CLEAN AT ANY TIME THE PIC MAY REFERENCE THE AFM FOR ITEMS NOT INCLUDED THIS LIST. 6

DA-40F NORMAL LIST Before Engine Start Pilot Documents BOARD Times & Inspections ED Preflight Inspection Passenger Briefing Rear Door CLOSED & LATCHED Baggage SECURE Rudder Pedals ADJUSTED Safety Harnesses FASTENED Quadrant Friction Lock ADJUSTED Parking Brake Circuit Breakers IN Flight Controls FREE & CORRECT Essential Bus Switch Alternate Static CLOSED Avionics DO NOT power the avionics for more than 10 minutes with the engine and alternator off. Annunciations NORMAL Brakes HOLD 1/4 OPEN RICH Tach Time CFIRM Fuel Computer ENTER AMOUNT LOWEST TANK V-speeds Engine Start Front Canopy POSITI 1 OR 2 Strobes Brakes HOLD (verify noise) Prime (cold engine) 3 7 SECDS Propeller Area CLEAR Ignition Switch START DO NOT operate the starter for more than 10 sec. After operating the starter motor, let cool for 20 sec. After 6 start attempts, allow the starter to cool for 30 mins. After Start 1000 Oil Pressure GREEN Ammeter GREEN Fuel Flow GREEN LEAN FOR TAXI G1000 Setup Avionics Master ATIS (weather) Altimeters (G1000 & STBY) Clearance Transponder Heading Bug Bug Flight Plan RAIM Annunciations Taxi Brief CO Detector Taxi Light Interior Lighting Parking Brake Brakes Flight Instruments Before Taxi OBTAIN OBTAIN CODE & ALT RWY HDG ENTER AS NECESSARY NORMAL ACCOMPLISH PRESS TO TEST RELEASE TEST TAXI DA-40F LISTS DA-42 LISTS ARROW LISTS 7

DA-40F NORMAL LIST DA-40F LISTS Run-up Area Parking Brake Engine Check CLEAR FULLEST TANK RICH 1800 RPM LEAN (all USU flights) Takeoff Roll HSI RWY HDG ### CFIRMED Power POWER (no less than 2200 RPM) AIRSPEED ALIVE VR 59 KTS. ROTATE Accelerate to climbout speed - 66 KIAS 500 Feet AGL ARROW LISTS DA-42 LISTS NOTE: Use Lean Assist Page to Set mixture 100 F rich of peak. Carburetor Heat Magnetos (175/50) Engine Gauges GREEN IDLE 1000 Before Takeoff Canopy & Windows CLOSED & LATCHED Departure Briefing CLEARANCE (EMER PLAN) Circuit Breakers IN Magnetos BOTH T/O Annunciator Panel Elevator Trim T/O Parking Brake RELEASE Traffic 360 CLEAR Carburetor Heat Final FINAL IS CLEAR Runway RUNWAY IS CLEAR Carburetor Heat COLD Landing Light (cleared for T/O) Pitot Heat VERIFY UP Landing Light Accelerate to cruise climb speed - 73 KIAS Engine Gauges Transponder Taxi Light Power 1000 Feet AGL Level Off Cruise VERIFY ALT MODE 2500 RPM LEAN NOTE: Use Lean Assist Page to Set mixture 100 F rich of peak. Power FOR CRUISE NEVER allow engine RPM to exceed 2700 Engine Gauges Annunciator Panel CLEAR Exterior Lighting Fuel MANAGE Fuel differential MUST NOT exceed 10 gallons between right & left tank 8

DA-40F NORMAL LIST Clearing Turn Radio Bug Heading Bug Emergency Landing Site Aircraft Maneuvers ANNOUNCE INTENTIS CHOSEN APPROPRIATE CFIGURED Fuel pump and carburetor heat should remain during maneuvers unless determined necessary for safety of flight Power Carburetor Heat Lights Clean Up Checklist Descent/Approach Checklist RPM COLD UP FULLEST TANK Circuit Breakers IN Exterior Lighting ATIS (weather) OBTAIN Altimeter (G1000 & stby) Annunciator Panel CLEAR Engine Gauges GREEN Fuel Quantity ENRICHEN Carburetor Heat (See: CARBURETOR HEAT SOP for proper carburetor heat operation) FULLEST TANK Safety Harnesses FASTENED Final Check Carburetor Heat COLD ESTABLISH Landing and Taxi Lights After Landing Check Runway Clear ANNOUNCE Exterior Lighting Transponder VERIFY ALT MODE Carburetor Heat COLD 1000 LEAN FOR TAXI Pitot Heat UP Taxi Brief ACCOMPLISH Engine Shutdown 1000 Parking Brake Avionics Master Essential Bus Switch Exterior Lighting IDLE CUT After engine stops: Ignition Switch Key REMOVE FROM IGNITI Hobbs & Tach Time RECORD BAT & ALT Exterior Lighting ALL Instrument & Flood Lights FLIGHT PLAN CLOSE DA-40F LISTS DA-42 LISTS ARROW LISTS 9

DA-40F NORMAL LIST DA-40F LISTS DA-42 LISTS ARROW LISTS Aircraft Secure Tie-Downs SECURED Chocks INSTALLED (main ldg gear) Pitot Cover INSTALLED Gust Lock INSTALLED Stall Warning Cover INSTALLED Parking Brake RELEASED (if Chocks Installed) Personal Items, Trash, etc. REMOVED Rear Door CLOSED & LOCKED Windows CLOSED & LATCHED Front Canopy CLOSED & LOCKED Reference Speeds Vso (dirty stall speed) 49 kts Vs1 (clean stall speed) 52 kts Vr (rotation speed) 59 kts Vy (best rate of climb) 66 kts w/flaps T/O 73 kts w/flaps UP Vref (normal approach speed) 71 kts Vref (short field approach speed) 66 kts Vglide (best glide speed) 73 kts Vfe (flap extend speed) T/O - 108 kts LDG - 90 kts Va (maneuvering speed) 108 kts (2535 lbs) 94 kts (2161 lbs) Carb Heat SOP NOTE: Carburetor heat should be used as deemed necessary by the pilot to avoid carburetor ice formation! Carburetor Heat should be used anytime carburetor icing is suspected or anytime the potential for carburetor ice is present. Carburetor heat will be for any descent and may be turned upon leveling-off. Carburetor heat will be turned during the Downwind and turned with flap application on Base. Carburetor heat will be turned 200 feet above MDA or DH on an instrument approach and then used as necessary after arriving at MDA or DH. SOP should be off when above 500 AGL unless deemed necessary for the safety of flight. Verify Fuel pressure prior to turning off the fuel pump. 10

DA-40F MANEUVER LIST Maneuvers Clearing Turn Radio ANNOUNCE INTENTIS Bug Heading Bug APPROPRIATE Aircraft CFIGURED Fuel pump and carburetor heat should remain during maneuvers unless determined necessary for safety of flight Ground Reference Maneuvers Winds IDENTIFY Emergency Landing Site SELECTED 800 AGL 95 KIAS Power ~2350 RPM Up On Pitch +4 Pivotal Calculations The formula is as follows: ground speed squared divided by 11.3 for knots and ground speed squared divided by 15 for miles per hour. Remember these are figured in Groundspeed and rounded up. KTS MPH ALT AGL 87 100 670 91 105 735 96 110 810 100 115 885 104 120 960 109 125 1050 113 130 1130 Steep Turns AT LEAST 2,000 AGL Maneuvers Checklist 95 KIAS (±10 KIAS) Bank ROLLING THRU 30 Power INCREASE ~200 RPM Pitch +2.5-5 NOSE HIGH Enter 360º Turn Bank Angle 45 /50 (±5 ) Elevator MAINTAIN BACK PRESS. Power INCREASE TO MAINTAIN AIRSPEED Rudder COORDINATED Roll-out of Turn LEAD BY 1/2 BANK Power REDUCE Repeat maneuver in opposite direction Clean Up Checklist PERFORM Slow Flight AT LEAST 2,000 AGL Maneuvers Checklist 1800 RPM APPROACH(<108 KTS) OR LANDING(<91KTS) Specified OBTAIN 5-10 KNOTS ABOVE STALL WARNING Pitch FOR AIRSPEED(+10 KTS OR +5 KTS) HOLD ASSIGNED ALT (±100 FT/±50 FT) Heading ±10 Recovery- FULL & Hdg MAINTAIN T/O, then UP when >75 KIAS Clean Up Checklist PERFORM DA-40F LISTS DA-42 LISTS ARROW LISTS 11

DA-40F MANEUVER LIST DA-40F LISTS DA-42 LISTS ARROW LISTS Power On Stall AT LEAST 2,000 AGL Maneuvers Checklist 1500 RPM As speed decreases to 73 KIAS: ALT MAINTAIN ±100 FT HDG ±10 UNLESS TURNING STALL (MAX 20 BANK) When speed reaches 73 KTS: SMOOTHLY APPLY FULL OPEN Pitch SMOOTHLY 18 NOSE UP AND HOLD Rudder MAINTAIN COORDINATI Stall Horn ANNOUNCE Stall Warning Stall Buffet ANNOUNCE Stalling Promptly Initiate Recovery Private Pilots ACS requires a recovery after a full stall occurs. Commercial Pilot ACS requires a recovery at the first indication of a stall. Recovery- Simultaneously: Pitch REDUCE BACK PRESSURE 3 NOSE HIGH Wings LEVEL VERIFY FULL OPEN When increases above 60 KTS: Pitch 5-7 73 KIAS Clean Up Checklist PERFORM Power Off Stall AT LEAST 2,000 AGL Maneuvers Checklist 1800 RPM APPROACH(<108 KTS) OR LANDING(<91 KTS) MAINTAIN ±100 FT When speed reaches 70 KTS: IDLE Pitch FOR 70 KTS (STABILIZED DESCENT) Within 100 of assigned altitude transition to a nose up attitude. Rudder MAINTAIN COORDINATI Stall Horn ANNOUNCE Stall Warning Stall Buffet ANNOUNCE Stalling Promptly Initiate Recovery Private Pilots ACS requires a recovery after a full stall occurs. Commercial Pilot ACS requires a recovery at the first indication of a stall. Recovery- Simultaneously: Pitch REDUCE BACK PRESSURE 3 NOSE HIGH Wings LEVEL VERIFY FULL OPEN T/O TING When increases above 60 KTS: Pitch 5-7 73 KIAS Clean Up Checklist PERFORM 12

DA-40F MANEUVER LIST Chandelle Lazy Eights AT LEAST 2,000 AGL Maneuvers Checklist Visual Reference Points SELECT 95 KIAS First 90 of Turn: Bank ROLL TO 30 Power FULL Pitch SLOWLY INCREASE Rudder MAINTAIN COORDINATI 90 Point MAX PITCH UP (12-15 ) Last 90 of Turn Bank SLOWLY REDUCE Pitch MAINTAIN MAX PITCH UP (12-15 ) Rudder MAINTAIN COORDINATI 180 Point WINGS LEVEL JUST ABOVE A STALL Heading ±10 Recovery: INCREASE TO 95 KIAS MAINTAIN AS AIRSPEED BUILDS Heading ±10 Rudder MAINTAIN COORDINATI Repeat maneuver in opposite direction Clean Up Checklist PERFORM AT LEAST 2,000 AGL Maneuvers Checklist Visual Reference Points SELECT Power 2250-2300 RPM 95 KIAS Slowly begin increasing pitch and bank simultaneously. At 45 Point: Pitch MAX PITCH UP Bank APPROX. 15 At 90 Point: Pitch LEVEL WITH HORIZ Bank APPROX. 30 MINIMUM AIRSPEED ABOVE A STALL At 135 Point: Pitch MAX PITCH DOWN Bank APPROX. 15 At 180 Point: Pitch LEVEL WITH HORIZ Bank WINGS LEVEL ±10 KTS FROM ENTRY SPEED ±100 FT FROM ENTRY ALT Heading ±10 Repeat maneuver in opposite direction Clean Up Checklist PERFORM DA-40F LISTS DA-42 LISTS ARROW LISTS 13

DA-40F MANEUVER LIST Steep Spiral Clean Up Checklist DA-40F LISTS DA-42 LISTS ARROW LISTS AT LEAST 4,000 AGL This maneuver must be recovered by 1,500 AGL according to USU SOPs and Commercial ACS. Maneuvers Checklist Winds IDENTIFY Ground Reference Point SELECT When over selected point: Power IDLE Carburetor Heat TRIMMED FOR BEST GLIDE While performing maneuver: BEST GLIDE ±10 KTS Bank NOT TO EXCEED 60 Ground Track MAINTAIN AROUND POINT Engine Clear PERFORM WITH HEADWIND The maneuver is terminated after performing three, 360 turns around the point or upon reaching 1,500 FT AGL. Clean Up Checklist PERFORM Power Carburetor Heat Lights RPM COLD UP FULLEST TANK 14

DA-40F ABNORMAL LIST Rough Engine ENGINE RESTART Stationary Propeller Engine Indications Ignition BOTH Carburetor Heat FOR SMOOTH RUNNING / TRY VARIOUS TINGS If engine is still running roughly, Land ASAP- Prepare for engine failure. Engine Failure TRIMMED FOR BEST GLIDE Landing Site SELECT If propeller is windmilling ENGINE RESTART Windmilling Propeller If propeller is stationary ENGINE RESTART Stationary Propeller If restart is unsuccessful proceed with ENGINE SECURE ENGINE RESTART Windmilling Propeller 70-130 KIAS Ignition BOTH Carburetor Heat APPROPRIATE If engine does not start: FULL LEAN PUSH FORWARD UNTIL ENGINE STARTS If engine will not start proceed with ENGINE SECURE & EVACUATE 70-80 KIAS APPROPRIATE Carburetor Heat Electrical equipment ALL Avionics BATTERY Ignition Switch START If starter is inoperative: Expect at least 1000 altitude loss Ignition Switch BOTH INCREASE ABOVE 130 KIAS If engine won t start, go to ENGINE SECURE & EVACUATE ENGINE SECURE Mayday ANNOUNCE Transponder SQUAWK 7700 Safety Harnesses TIGHTEN Ignition Switch When certain field can be made: LANDING Touchdown slowest airspeed & commence EVACUATE Aircraft Canopy Airplane Fire Suppressant EVACUATE STOP OPEN EVACUATE IMMEDIATELY USE AS NECESSARY 15 DA-40F LISTS DA-42 LISTS ARROW LISTS

DA-40F ABNORMAL LIST DA-40F LISTS DA-42 LISTS ARROW LISTS Engine Fire In Flight Landing Site SELECT Cabin Heat MAX POWER Emergency Windows/Canopy OPEN If fire persists: Emergency Descent INITIATE UP INCREASE WARNING: VNO = 129 KIAS, and VNE = 178 KIAS Bank 30-45 Once fire is extinguished: Bank WINGS LEVEL Pitch GENTLY BRING NOSE UP ESTABLISH BEST GLIDE Proceed with ENGINE SECURE and EVACUATE Electrical Fire In Flight Emergency Switch Cabin Heat Landing Site SELECT Emergency Windows OPEN Front Canopy UNLATCH Fire Suppressant USE AS NECESSARY Land as soon as possible Electrical Fire On The Ground IDLE IDLE CUT When the engine has stopped: Ignition Switch Canopy OPEN Airplane EVACUATE IMMEDIATELY Fire Suppressant USE AS NECESSARY Engine/Carburetor Fire During Start Starter CTINUE CRANKING If engine starts: Starter CEASE CRANKING RPM TO 1800 FOR 4 MINS Cabin Heat If engine does not start: LEAN FULL Electrical When the engine has stopped: Ignition Switch Canopy OPEN Airplane EVACUATE IMMEDIATELY Fire Suppressant USE AS NECESSARY Aircraft HAVE ED Loss Of RPM Carburetor Heat Friction Lock ADJUST 16

DA-40F ABNORMAL LIST Smoke And Fire During Takeoff If takeoff can be abandoned: IDLE Cabin Heat Brakes APPLY All Electrical Switches Airplane EVACUATE If takeoff cannot be abandoned: After climbing to a location where an emergency landing may be executed: TRIMMED FOR BEST GLIDE Cabin Heat All Electrical Switches Emergency Windows OPEN AS REQ D Front Canopy UNLATCH After Touchdown EVACUATE Door Open (On Ground Or In Flight) SLOW TO VA Front Canopy LATCHED Rear Door (Don t touch a door in flight!) LATCHED If rear door appears unlatched in flight, leave as is and land ASAP at an appropriate airfield CO Detector Illuminated Test/Reset Button If alert continues: Cabin Heat Ventilation Emergency Windows Front Canopy Land as soon as practical PRESS OPEN OPEN UNLATCH Low Volts On Ground 1200 RPM LEAVE Electrical Equipment Ammeter If caution light does not extinguish and the ammeter reads zero: RECYCLE ALTERNATOR If caution light continues and ammeter reads zero: Prepare to terminate flight Low Volts In Flight LEAVE Electrical Equipment (IF NOT REQ D) Ammeter RECYCLE ALTERNATOR If caution light does not extinguish and the ammeter reads zero: Proceed with ALTERNATOR FAILURE Overvoltage Essential Bus ALTERNATOR Unnecessary Electrical Equipment Land at nearest airfield. Expect only 30 mins. of usable electric power. Starter Engaged IDLE IDLE CUT Ignition Switch Terminate flight unscheduled maintenance is necessary. DA-40F LISTS DA-42 LISTS ARROW LISTS 17

DA-40F ABNORMAL LIST DA-40F LISTS DA-42 LISTS ARROW LISTS Circuit Breakers Alternator Failure If no circuit breakers had popped: Ammeter If ammeter appears normal: Continue to nearest practicable airport, monitor electrical system. Have mechanic fix problem. If any circuit breakers have popped: Allow cooling period and attempt to reset popped circuit breakers (reset only once.) If a reset fails: Essential Bus Switch Electrical Load REDUCE TO MINIMUM Voltage REGULARLY Electrical System MITOR Land at nearest suitable airport within 30 minutes If aircraft battery becomes depleted: Emergency Battery Switch UNGUARD and Descent Defective Control MAINTAIN TO AIRPORT TEST TO A HIGHER POWER TING A lean mixture can lead to engine roughness and a loss of power. High Cylinder Head Temperature ENRICH Oil Pressure If oil pressure is low proceed with LOW OIL PRESSURE: If oil pressure is normal: REDUCE INCREASE High Fuel Flow Fuel Pressure Low fuel pressure indicates a possible leak in the system Fuel Quantity MITOR Power Setting Land as soon as practicable to avoid fuel exhaustion Low Fuel Pressure Fuel Quantity ADJUST Land as soon as practicable; prepare for engine failure High Oil Temperature Oil Pressure If oil pressure is low proceed with LOW OIL PRESSURE If oil pressure is normal: ENRICH REDUCE INCREASE Land as soon as practicable Low Oil Pressure REDUCE Oil Temperature MITOR CHT MITOR Land as soon as practicable; prepare for engine failure 18

DA-40F ABNORMAL LIST Icing Area Pitot Heat Flight Into Icing LEAVE Cabin Heat /DEFROST RPM INCREASE Carburetor Heat Emergency Windows OPEN IF REQUIRED If Pitot Heat fails, the alternate static valve can be opened and emergency windows closed. CAUTI: Ice build-up increases stall speed. If ice does not melt before landing, a no-flap landing may be required. Spin Recovery The following steps are made immediately and simultaneously: IDLE Ailerons NEUTRAL Rudder FULL DEFLECTI OPPOSITE OF SPIN Elevator FULLY FORWARD UP When rotation has stopped: Rudder NEUTRAL Elevator PULL CAREFULLY Descent RECOVER INTO NORMAL FLIGHT WARNING: Never allow the airplane s speed to exceed VNE BEST GLIDE SPEEDS Aircraft weight (lbs) 2535 2205 1874 UP 73 68 60 T/O 72 66 59 LDG 71 63 58 DA-40F LISTS DA-42 LISTS ARROW LISTS AT ANY TIME THE PIC MAY REFERENCE THE AFM FOR ITEMS NOT INCLUDED THIS LIST. 19

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DA-40CS PREFLIGHT LIST DA 40CS Flight Deck Weather, Flight Plan, Weight & Balance Aircraft Documents & Inspections CURRENT Flight Control Lock REMOVE Ignition Switch Electrical Equipment ALL Emergency Battery GUARDED ELT ARMED/INDICATOR Circuit Breakers IN Control Lever IDLE CUT Prop FULL FORWARD IDLE OPERATI Flight Controls FULL DEFLECTI UP Lights & Pitot Heat OPERATI Lights & Pitot Heat G1000 Databases CURRENT Fuel Quantity Trim OPERATI Fire Extinguisher CHARGED & SECURED Baggage STOWED Left Wing Rear Ventilation Intake Left Gear Strut Wheel & Tire Chocks REMOVE Opening Around Tank Drain Tank Drain FUEL QUALITY Wing Surface 2 Stall Strips Stall Warning REMOVE COVER & Tank Filler & FUEL QUANTITY Fuel Tank Vents Pitot-Static Probe REMOVE COVER & Wing Tie-Down REMOVE Wing Tip 2 Static Wicks Aileron Aileron Paddle Hinges & Safety Pins Push Rod, Bracket, & Bonding Straps Trim Tab (don t touch!) Flap Counter Weight Hinges & Safety Pins Push Rod, Bracket, & Bonding Straps Torsion Tube & Bonding Strap Main Gear FROM AFT Brakes & Hydraulic Line Brake Pads CFIRM SUFFICIENT THICKNESS Left Fuselage Rear Cabin Door & Window Rear Door Pins Antennas Fuselage Surface Tail Skid Tail Tie-Down REMOVE Rudder Cables & Eyelets (left & right) Bottom Hinge, Mount, & Bonding Straps Static Wick Trim Tab (don t touch!) Top Hinge DA-40F LISTS DA-40CS LISTS ARROW LISTS 21

DA-40CS PREFLIGHT LIST ARROW LISTS DA-40CS LISTS DA-40F LISTS Elevator Hinges 2 Static Wicks Trim Tab, Linkage, Bolts & Safety Wire Lightening Discharge Right Fuselage Tail Skid & Lower Fin Fuselage Skin Rear Window Flap Main Gear FROM AFT Brakes & Hydraulic Line Brake Pads CFIRM SUFFICIENT THICKNESS Torsion Tube & Bonding Strap Hinges & Safety Pins Push Rod, Bracket, & Bonding Straps Counter Weight Aileron Hinges & Safety Pins Push Rod, Bracket, & Bonding Straps Aileron Paddle Right Wing 2 Static Wicks Wing Tip Wing Tie-Down REMOVE Fuel Tank Vents Tank Filler & FUEL QUANTITY Wing Surface 2 Stall Strips Opening Around Tank Drain Tank Drain FUEL QUALITY Right Gear Strut Wheel & Tire Chocks OAT Probe Underside REMOVE Nose Gear/Shock Absorber Cowl Exit Oil Cooler Gascolator DRAIN & FUEL QUALITY Nose Right Front Ventilation Intake Oil Level (recommended 6 qts.) Cowling & Fasteners Spinner & Fasteners Propeller Engine Cooling Intakes Engine Intake Air Filter Heater Air Intake Oil Cooler Intake Left Front Ventilation Intake Nose Gear & Wheel Front Canopy AND CLEAN AT ANY TIME THE PIC MAY REFERENCE THE AFM FOR ITEMS NOT INCLUDED THIS LIST. 22

Before Engine Start Pilot Documents BOARD Times & Inspections ED Preflight Inspection Passenger Briefing Rear Door CLOSED & LATCHED Baggage SECURE Rudder Pedals ADJUSTED Safety Harnesses FASTENED Quadrant Friction Lock ADJUSTED Parking Brake Circuit Breakers IN Alternate Air CLOSED Flight Controls FREE & CORRECT Essential Bus Switch Alternate Static CLOSED Avionics DO NOT power the avionics for more than 10 minutes with the engine and alternator off Annunciations NORMAL 1/4 OPEN Tach Time CFIRM Fuel Computer ENTER AMOUNT LOWEST TANK V-speeds Cold Engine Start Front Canopy POSITI 1 OR 2 Strobes (verify noise) 1.5 Forward RICH 3-5 sec then LEAN 1/2 Forward DA-40CS NORMAL LIST Propeller Area CLEAR Brakes HOLD Ignition Switch START DO NOT operate the starter for more than 10 sec. After operating the starter motor, let cool for 20 sec. After 6 start attempts, allow the starter to cool for 30 mins. After Engine Fires Full RICH Oil Pressure GREEN Ammeter GREEN Fuel Pressure GREEN (14-35 psi) Annunciations NORMAL 1000 LEAN FOR TAXI HOT Engine Start Front Canopy POSITI 1 OR 2 Strobes (verify noise) 1.5 Forward RICH 1-3 sec then Lean Brakes HOLD Propeller Area CLEAR Ignition Switch START After Engine Fires Full RICH Oil Pressure GREEN Ammeter GREEN Fuel Pressure GREEN (14-35 psi) Annunciations NORMAL 1000 LEAN FOR TAXI 23 DA-40F LISTS DA-40CS LISTS ARROW LISTS

DA-40CS NORMAL LIST DA-40F LISTS DA-40CS LISTS ARROW LISTS 24 Flooded Engine Start HALFWAY FORWARD FULL LEAN Ignition Switch START DO NOT operate the starter for more than 10 sec. After operating the starter motor, let cool for 20 sec. After 6 start attempts, allow the starter to cool for 30 mins. RETARD AFTER ENGINE FIRES After Engine Fires Full RICH Oil Pressure GREEN Ammeter GREEN Fuel Pressure GREEN (14-35 psi) Annunciations NORMAL 1000 LEAN FOR TAXI Avionics Master ATIS (weather) Altimeters (3) Clearance Transponder Heading Bug Bug Flight Plan RAIM Pitot Heat Ammeter Annunciations G1000 Setup OBTAIN OBTAIN CODE & ALT RWY HDG ENTER AS NECESSARY TEST (ammeter must rise) GREEN NORMAL Auto Pilot Test Taxi Brief Taxi Light Interior Lighting Seats and Belts Rear Canopy Door Warning Lights Parking Brake Brakes Flight Instruments Align Aircraft Into Wind Parking Brake Fuel Tank Selector Fuel Pressure Before Taxi Engine Check PERFORM ACCOMPLISH SECURE CLOSED AND LOCKED RELEASE TEST TAXI FULLEST TANK RICH 2000 RPM 15-35 PSI LEAN (all USU flights) NOTE: Use Lean Assist Page to Set mixture 100 F rich of peak. Engine Instruments Circuit Breakers Prop 1. Decrease in RPM 2. Decrease in Oil Pressure GREEN IN CYCLE 3 TIMES 3. Increase in Manifold Pressure Magnetos (175/50) IDLE 1000 Alternate Air /CLOSED Lights AS REQ D Transponder ALT

DA-40CS NORMAL LIST Before Takeoff 1000 Feet AGL Canopy & Windows Departure Briefing Circuit Breakers Magnetos Prop Annunciator Panel Elevator Trim Parking Brake Traffic Final Runway Landing Light Pitot Heat Transponder Takeoff Roll CLOSED & LATCHED CLEARANCE (EMER PLAN) IN BOTH T/O FULL FORWARD T/O RELEASE 360 CLEAR FINAL IS CLEAR RUNWAY IS CLEAR (cleared for T/O) /ALT Prop FULL FORWARD HSI RWY HDG ### CFIRMED Power POWER (2680 ±20 RPM) ABORT T/O if more than ±20 AIRSPEED ALIVE VR 59 KTS. ROTATE Accelerate to climbout speed - 66 KIAS 500 Feet AGL Prop 2400 (MAX) VERIFY UP Landing Light Accelerate to cruise climb speed - 73 KIAS Engine Gauges Transponder Taxi Light Level Off Cruise VERIFY ALT MODE /Prop TO POWER TABLE Landing Light VERIFY VERIFY CHT 150-400 F Oil Temp 165-220 F LEAN Trim AS NEEDED Fuel Tank Selector FULLEST TANK Turn On Before Switching Fuel differential MUST NOT exceed 10 gallons between right & left tank Reference Speeds Vso (dirty stall speed) 49 kts Vs1 (clean stall speed) 52 kts Vr (rotation speed) 59 kts Vy (best rate of climb) 66 kts w/flaps T/O 73 kts w/flaps UP Vref (normal approach speed) 71 kts Vref (short field approach speed) 66 kts Vglide (best glide speed) 73 kts Vfe (flap extend speed) T/O - 108 kts LDG - 90 kts Va (maneuvering speed) 108 kts (2535 lbs) 94 kts (2161 lbs) DA-40F LISTS DA-40CS LISTS ARROW LISTS 25

DA-40CS NORMAL LIST DA-40F LISTS DA-40CS LISTS ARROW LISTS Clearing Turn Radio Bug Heading Bug Emergency Landing Site Aircraft Power Lights Maneuvers ANNOUNCE INTENTIS CHOSEN APPROPRIATE CFIGURED Fuel pump should remain during maneuvers unless determined necessary for safety of flight Circuit Breakers Exterior Lighting ATIS (weather) Altimeter (3) Annunciator Panel Engine Gauges Fuel Quantity Safety Harnesses Clean Up Checklist AS APPROPRIATE UP FULLEST TANK Descent/Approach Checklist IN OBTAIN CLEAR GREEN ENRICHEN FULLEST TANK FASTENED Seat Belts Trim Lights Prop Go Around Prop Final Check APPROACH VERIFY FULLEST TANK VERIFY SECURED AT OR BELOW VFE T/O AS NEEDED BEFORE LANDING AS APPROPRIATE FULL FORWARD 13 MP LDG 66 71 KTS NOTE: If LANDING IN STRG WIND AND TURBULENCE USE A HIGHER APPROACH SPEED AND/OR USE LESS FLAPS. Go Around Check FULL FORWARD 66 KTS T/O ANNOUNCE At 500 AGL or Safe 2400 RPM (MAX) UP 73 KTS 26

DA-40CS NORMAL LIST After Landing Check Aircraft Secure Runway Clear ANNOUNCE Exterior Lighting Transponder VERIFY ALT MODE IDLE LEAN FOR TAXI Pitot Heat UP Taxi Brief ACCOMPLISH Engine Shutdown 1000 Parking Brake Avionics Master Essential Bus Switch Exterior Lighting IDLE CUT After engine stops: Ignition Switch Key REMOVE FROM IGNITI Hobbs & Tach Time RECORD BAT & ALT Exterior Lighting ALL Instrument & Flood Lights FLIGHT PLAN CLOSE Tie-Downs SECURED Chocks INSTALLED (main ldg gear) Pitot Cover INSTALLED Gust Lock INSTALLED Stall Warning Cover INSTALLED Parking Brake RELEASED (if Chocks Installed) Personal Items, Trash, etc. REMOVED Rear Door CLOSED & LOCKED Windows CLOSED & LATCHED Front Canopy CLOSED & LOCKED SOP should be off when above 500 AGL unless deemed necessary for the safety of flight. Verify Fuel pressure prior to turning off the fuel pump. Operations at high altitudes may cause vapor bubbles, resulting in intermittent low fuel pressure indications. If this occurs, the electric fuel pump may be turned and the flight can be continued as normal. If the low fuel pressure message remains, refer to the LOW FUEL PRES- SURE emergency checklist. DA-40F LISTS DA-40CS LISTS ARROW LISTS 27

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DA-40CS MANEUVER LIST Maneuvers Steep Turns Clearing Turn Radio ANNOUNCE INTENTIS Bug Heading Bug APPROPRIATE Aircraft CFIGURED Fuel pump should remain during maneuvers unless determined necessary for safety of flight Ground Reference Maneuvers Winds IDENTIFY Emergency Landing Site SELECTED 800 AGL 95 KIAS Power ` 18 M.P. Up On Pitch +4 Pivotal Calculations The formula is as follows: ground speed squared divided by 11.3 for knots and ground speed squared divided by 15 for miles per hour. Remember these are figured in Groundspeed and rounded up. KTS MPH ALT AGL 87 100 670 91 105 735 96 110 810 100 115 885 104 120 960 109 125 1050 113 130 1130 AT LEAST 2,000 AGL Maneuvers Checklist 95 KIAS (±10 KIAS) Bank ROLLING THRU 30 Power INCREASE ~1-2 MP Pitch +2.5-5 NOSE HIGH Enter 360º Turn Bank Angle 45 /50 (±5 ) Elevator MAINTAIN BACK PRESS. Power INCREASE TO MAINTAIN AIRSPEED Rudder COORDINATED Roll-out of Turn LEAD BY 1/2 BANK Power REDUCE Repeat maneuver in opposite direction Clean Up Checklist PERFORM Slow Flight AT LEAST 2,000 AGL Maneuvers Checklist 12 M.P. APPROACH(<108 KTS) OR LANDING(<91KTS) Specified OBTAIN 5-10 KNOTS ABOVE STALL WARNING Pitch FOR AIRSPEED(+10 KTS OR +5 KTS) HOLD ASSIGNED ALT (±100 FT/±50 FT) Heading ±10 Recovery- FULL & Hdg MAINTAIN T/O, then UP when >75 KIAS Clean Up Checklist PERFORM DA-40F LISTS DA-40CS LISTS ARROW LISTS 29

DA-40CS MANEUVER LIST DA-40F LISTS DA-40CS LISTS ARROW LISTS Power Off Stall AT LEAST 2,000 AGL Maneuvers Checklist 12 MP APPROACH(<108 KTS) OR LANDING(<91 KTS) MAINTAIN ±100 FT When speed reaches 70 KTS: IDLE Pitch FOR 70 KTS (STABILIZED DESCENT) Within 100 of assigned altitude transition to a nose up attitude. Rudder MAINTAIN COORDINATI Stall Horn ANNOUNCE Stall Warning Stall Buffet ANNOUNCE Stalling Promptly Initiate Recovery Private Pilots ACS requires a recovery after a full stall occurs. Commercial Pilot ACS requires a recovery at the first indication of a stall. Recovery- Simultaneously: Pitch REDUCE BACK PRESSURE 3 NOSE HIGH Wings LEVEL VERIFY FULL OPEN T/O TING When increases above 60 KTS: Pitch 5-7 73 KIAS Clean Up Checklist PERFORM Power On Stall AT LEAST 2,000 AGL Maneuvers Checklist 12 MP As speed decreases to 73 KIAS: ALT MAINTAIN ±100ft HDG ±10 UNLESS TURNING STALL (MAX 20 BANK) When speed reaches 73 KTS: SMOOTHLY APPLY FULL OPEN Pitch SMOOTHLY 18 NOSE UP AND HOLD Rudder MAINTAIN COORDINATI Stall Horn ANNOUNCE Stall Warning Stall Buffet ANNOUNCE Stalling Promptly Initiate Recovery Private Pilots ACS requires a recovery after a full stall occurs. Commercial Pilot ACS requires a recovery at the first indication of a stall. Recovery- Simultaneously: Pitch REDUCE BACK PRESSURE 3 NOSE HIGH Wings LEVEL VERIFY FULL OPEN When increases above 60 KTS: Pitch 5-7 73 KIAS Clean Up Checklist PERFORM 30

DA-40CS MANEUVER LIST Chandelle AT LEAST 2,000 AGL Maneuvers Checklist Visual Reference Points SELECT 95 KIAS First 90 of Turn: Bank ROLL TO 30 Power FULL Pitch SLOWLY INCREASE Rudder MAINTAIN COORDINATI 90 Point MAX PITCH UP (12-15 ) Last 90 of Turn Bank SLOWLY REDUCE Pitch MAINTAIN MAX PITCH UP (12-15 ) Rudder MAINTAIN COORDINATI 180 Point WINGS LEVEL JUST ABOVE A STALL Heading ±10 Recovery: INCREASE TO 95 KIAS MAINTAIN AS AIRSPEED BUILDS Heading ±10 Repeat maneuver in opposite direction Clean Up Checklist PERFORM Lazy Eights AT LEAST 2,000 AGL Maneuvers Checklist Visual Reference Points SELECT Power 17-18 MP 95 KIAS Slowly begin increasing pitch and bank simultaneously. At 45 Point: Pitch MAX PITCH UP Bank APPROX. 15 At 90 Point: Pitch LEVEL WITH HORIZ Bank APPROX. 30 MINIMUM AIRSPEED ABOVE A STALL At 135 Point: Pitch MAX PITCH DOWN Bank APPROX. 15 At 180 Point: Pitch LEVEL WITH HORIZ Bank WINGS LEVEL ±10 KTS FROM ENTRY SPEED ±100 FT FROM ENTRY ALT Heading ±10 Repeat maneuver in opposite direction Clean Up Checklist PERFORM DA-40F LISTS DA-40CS LISTS ARROW LISTS 31

DA-40CS MANEUVER LIST DA-40F LISTS DA-40CS LISTS ARROW LISTS Steep Spiral AT LEAST 4,000 AGL This maneuver must be recovered by 1,500 AGL according to USU SOPs and Commercial ACS. Maneuvers Checklist Winds IDENTIFY Ground Reference Point SELECT When over selected point: Power IDLE TRIMMED FOR BEST GLIDE While performing maneuver: BEST GLIDE ±10 KTS Bank NOT TO EXCEED 60 Ground Track MAINTAIN AROUND POINT Engine Clear PERFORM WITH HEADWIND The maneuver is terminated after performing three, 360 turns around the point or upon reaching 1,500 FT AGL. Clean Up Checklist PERFORM Power Lights Clean Up Checklist AS APPROPRIATE UP FULLEST TANK 32

DA-40CS ABNORMAL LIST Rough Engine ENGINE RESTART Stationary Propeller Engine Indications Ignition BOTH Alternate Air OPEN FOR SMOOTH RUNNING / TRY VARIOUS TINGS If engine is still running roughly, Land ASAP- Prepare for engine failure. Engine Failure TRIMMED FOR BEST GLIDE Landing Site SELECT If propeller is windmilling ENGINE RESTART Windmilling Propeller If propeller is stationary ENGINE RESTART Stationary Propeller If restart is unsuccessful proceed with ENGINE SECURE ENGINE RESTART Windmilling Propeller 80 KIAS FULLEST TANK Ignition BOTH APPROPRIATE Alternate Air OPEN If engine does not start: FULL LEAN PUSH FORWARD UNTIL ENGINE STARTS If engine will not start proceed with ENGINE SECURE & EVACUATE 80 KIAS Electrical Equipment ALL Avionics BATTERY APPROPRIATE Alternate Air OPEN Ignition Switch START If starter is inoperative: Expect at least 1000 altitude loss Ignition Switch BOTH INCREASE ABOVE 130 KIAS If engine won t start, go to ENGINE SECURE & EVACUATE ENGINE SECURE Mayday ANNOUNCE Transponder SQUAWK 7700 Safety Harnesses TIGHTEN Ignition Switch When certain field can be made: LANDING Touchdown slowest airspeed & commence EVACUATE Aircraft Canopy Airplane Fire Suppressant EVACUATE STOP OPEN EVACUATE IMMEDIATELY USE AS NECESSARY 33 DA-40F LISTS DA-40CS LISTS ARROW LISTS

DA-40CS ABNORMAL LIST DA-40F LISTS DA-40CS LISTS ARROW LISTS 34 Engine Fire In Flight Landing Site SELECT Cabin Heat MAX POWER Emergency Windows/Canopy OPEN If fire persists: Emergency Descent INITIATE UP INCREASE WARNING: VNO = 129 KIAS, and VNE = 178 KIAS Bank 30-45 Once fire is extinguished: Bank WINGS LEVEL Pitch GENTLY BRING NOSE UP ESTABLISH BEST GLIDE Proceed with ENGINE SECURE and EVACUATE Electrical Fire In Flight Emergency Switch Cabin Heat Landing Site SELECT Emergency Windows OPEN Front Canopy UNLATCH Fire Suppressant USE AS NECESSARY Land as soon as possible Friction Lock RPM Lever Loss Of RPM ADJUST HIGH RPM Electrical Fire On The Ground IDLE IDLE CUT When the engine has stopped: Ignition Switch Canopy OPEN Airplane EVACUATE IMMEDIATELY Fire Suppressant USE AS NECESSARY Engine Fire During Start LEAN Cabin Heat Brakes HOLD FULL When the engine has stopped: Ignition Switch Canopy OPEN Airplane EVACUATE IMMEDIATELY Fire Suppressant USE AS NECESSARY Aircraft HAVE ED Door Open (On Ground Or In Flight) SLOW TO VA Front Canopy LATCHED Rear Door (Don t touch a door in flight!) LATCHED If rear door appears unlatched in flight, leave as is and land ASAP at an appropriate airfield

Smoke And Fire During Takeoff If takeoff can be abandoned: IDLE Cabin Heat Brakes APPLY All Electrical Switches If takeoff cannot be abandoned: After climbing to a location where an emergency landing may be executed: TRIMMED FOR BEST GLIDE Cabin Heat All Electrical Switches Emergency Windows OPEN AS REQ D Front Canopy UNLATCH After Touchdown EVACUATE CO Contamination Cabin Heat Ventilation Emergency Windows Forward Canopy Land as soon as practical Low Volts On Ground OPEN OPEN UNLATCH 1200 RPM LEAVE Electrical Equipment Ammeter If caution light does not extinguish and the ammeter reads zero: RECYCLE ALTERNATOR If caution light continues and ammeter reads zero: Prepare to terminate flight DA-40CS ABNORMAL LIST Low Volts In Flight LEAVE Electrical Equipment (IF NOT REQ D) Ammeter RECYCLE ALTERNATOR If caution light does not extinguish and the ammeter reads zero: Proceed with ALTERNATOR FAILURE Alternator Failure Circuit Breakers If no circuit breakers had popped: Ammeter If ammeter appears normal: Continue to nearest practicable airport, monitor electrical system. Have mechanic fix problem. If any circuit breakers have popped: Allow cooling period and attempt to reset popped circuit breakers (reset only once.) If a reset fails: Essential Bus Switch Electrical Load REDUCE TO MINIMUM Voltage REGULARLY Electrical System MITOR Land at nearest suitable airport within 30 minutes If aircraft battery becomes depleted: Emergency Battery Switch UNGUARD and Starter Engaged IDLE IDLE CUT Ignition Switch Terminate flight unscheduled maintenance is necessary. 35 DA-40F LISTS DA-40CS LISTS ARROW LISTS

DA-40CS ABNORMAL LIST DA-40F LISTS DA-40CS LISTS ARROW LISTS Defective Control MAINTAIN TO AIRPORT Descent TEST TO A HIGHER POWER TING A lean mixture can lead to engine roughness and a loss of power High Cylinder Head Temperature ENRICH Oil Pressure If oil pressure is low proceed with LOW OIL PRESSURE: If oil pressure is normal: REDUCE INCREASE High Fuel Flow Fuel Pressure Low fuel pressure indicates a possible leak in the system Fuel Quantity MITOR Power Setting Land as soon as practicable to avoid fuel exhaustion Low Fuel Pressure Overvoltage Essential Bus ALTERNATOR Unnecessary Electrical Equipment Land at nearest airfield High Oil Temperature Oil Pressure If oil pressure is low proceed with LOW OIL PRESSURE CHT EGT If oil pressure is normal: ENRICH REDUCE INCREASE Land as soon as practicable Low Oil Pressure REDUCE Oil Temperature MITOR CHT MITOR Land as soon as practicable; prepare for engine failure Fuel Quantity ADJUST Land as soon as practicable; prepare for engine failure 36

DA-40CS ABNORMAL LIST Icing Area Pitot Heat Flight Into Icing LEAVE Cabin Heat /DEFROST RPM INCREASE Alternate Air OPEN Emergency Windows OPEN IF REQUIRED If Pitot Heat fails, the alternate static valve can be opened and emergency windows closed. CAUTI: Ice build-up increases stall speed. If ice does not melt before landing, a no-flap landing may be required. Spin Recovery The following steps are made immediately and simultaneously: IDLE Ailerons NEUTRAL Rudder FULL DEFLECTI OPPOSITE OF SPIN Elevator FULLY FORWARD UP When rotation has stopped: Rudder NEUTRAL Elevator PULL CAREFULLY Descent RECOVER INTO NORMAL FLIGHT WARNING: Never allow the airplane s speed to exceed VNE BEST GLIDE SPEEDS Aircraft weight (lbs) 2535 2205 1874 UP 73 68 60 T/O 72 66 59 LDG 71 63 58 DA-40F LISTS DA-40CS LISTS ARROW LISTS AT ANY TIME THE PIC MAY REFERENCE THE AFM FOR ITEMS NOT INCLUDED THIS LIST. 37

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DA-42 PREFLIGHT LIST DA42 Flight Deck Left Wing Weather, Flight Plan, Weight & Balance Aircraft Documents & Inspections CURRENT Flight Control Lock REMOVE Electrical Equipment ALL Circuit Breakers IN Gear Selector ED DOWN Power Levers IDLE Electric Master Fuel Quantity LANDING Lights & Pitot Heat OPERATI Stall Warning Horn OPERATI G1000 Database CURRENT Battery Voltage (+24.1 Volts) Electric Master Fire Extinguisher CHARGED & SECURED Baggage STOWED Left Main Gear Left Gear Strut and Downlock Wheel & Tire Squat Switch Limit Switches (2) (don t touch!) Brakes & Hydraulic Line Gear Doors and Linkage Chocks REMOVE Left Engine Nacelle 3 Air Inlets & 2 Air Outlets Gear Box Oil Spinner and Propeller Engine Oil Level Fuel Drains (2) FUEL QUALITY Cowling Exhaust Wing Leading Edge and Surfaces Stall Warning Tank Air Vent Fuel Caps & FUEL QUANTITY Pitot-Static Mast REMOVE COVER & Wing Tie-Down REMOVE Wing Tip and Lights Static Wicks (2) Aileron Aileron Paddle Hinges & Safety pins Push Rod, Bracket, & Bonding Straps Trim Tab (don t touch!) 39 Flap Counter Weight Hinges & Safety Pins Push Rod, Bonding Straps, and Linkage Tongue in Groove Assembly Fuel Cooler Air In & Outlet Main Gear FROM AFT Step Left Fuselage Rear Cabin Door & Window Rear Door Pins Antennas Fuselage Surface Tail Skid Tail Tie-Down REMOVE DA-40F LISTS DA-40CS LISTS DA-42 LISTS

DA-42 PREFLIGHT LIST DA-40F LISTS DA-40CS LISTS DA-42 LISTS Rudder Static Wick (1) Trim Tab (don t touch!) Cables and Eyelets Top and Bottom Hinges Elevator Elevator FREEDOM OF MOVEMENT Elevator Trim Tab Hinges Static Wicks (2) Lightening Discharge Right Fuselage Fuselage Surface Rear Window Step Right Wing-Flap Main Gear FROM AFT Fuel Cooler Air In & Outlet Tongue in Groove Assembly Push Rod, Bonding Straps, and Linkage Hinges & Safety Pins Counter Weight Aileron Hinges & Safety Pins Push Rod, Bracket, & Bonding Straps Aileron Paddle Right Wing Static Wicks (2) Wing Tip and Lights Wing Tie-Down REMOVE Wing Leading Edge and Surfaces Fuel Caps & FUEL QUANTITY Tank Air Vent Right Engine Nacelle 3 Air Inlets & 2 Air Outlets Gear Box Oil Spinner and Propeller Engine Oil Level Fuel Drains (2) FUEL QUALITY Cowling Exhaust Cabin Air Inlet Right Main Gear Right Gear Strut and Downlock Wheel & Tire Stall heat inhibitor switch Limit Switches (2) (don t touch!) Brakes & Hydraulic Line Gear Doors and Linkage Chocks REMOVE Strut and Lock Limit Switches (2) Wheel & Tire Gear Door and Linkage Nose Gear Nose Section (don t touch!) De-Ice Fluid (if installed) 3/4 FULL Baggage Doors CLOSED, LATCHED, & LOCKED OAT Probe and Battery Drain EPU Connection Landing and Taxi Lights Front Canopy AND CLEAN AT ANY TIME THE PIC MAY REFERENCE THE AFM FOR ITEMS NOT INCLUDED THIS LIST. 40

DA-42 NORMAL LIST Before Engine Start Pilot Documents BOARD Parking Brake Times & Inspections ED Preflight Inspection Passenger Briefing Rear Door CLOSED & LATCHED Baggage & Tow Bar SECURE Rudder Pedals ADJUSTED Safety Harnesses FASTENED Quadrant Friction Lock ADJUSTED Alternators ECUs AUTO Lights Emergency Switch GUARDED ELT ARMED Circuit Breakers IN Alternate Air CLOSED Gear Selector DOWN Manual Gear Extension Handle Avionics Master Electric Master Engine Master (Left & Right) Pitot Heat Alternate Static CLOSED Power Levers IDLE s Trim (2) Flight Controls FREE & CORRECT Electric Master Annunciations NORMAL Fuel Computer & ED PFD/MFD BACK UP MODE Tach Time Gear Warning/Fire Detector V-speeds Variable Elevator Backstop Engine Start CFIRM TEST RETRACT Normal order: Start Left Engine First Front Canopy POSITI 1 OR 2 Fuel Temperature ED Strobes Brakes HOLD Propeller Area CLEAR Engine Master Annunciations / Engine Instruments Glow Indication Ignition Switch START DO NOT operate the starter for more than 10 sec. After operating the starter motor, let cool for 20 sec. After 6 start attempts, allow the starter to cool for 30 mins. NOTE: Ignition Switch must be held until TACH indicates >500 RPM. Oil Pressure RPM 900 +/- 20 Annunciations Engine Instruments After Start OUTSIDE RED IN 3 SEC GREEN Warm Up Time START (Idle 2 Mins.) Pitot Heat Voltage & Load INDICATI Pitot Heat After 2 min warm up time, do not exceed 1400 RPM until Oil is > 50 C, and Coolant > 60 C DA-40F LISTS DA-40CS LISTS DA-42 LISTS 41

DA-40F LISTS DA-40CS LISTS DA-42 LISTS DA-42 NORMAL LIST PFD/MFD NORMAL MODE Avionics Master s CROSSFEED Circuit Breakers ED 42 G1000 Setup ATIS (weather) OBTAIN Altimeters (3) Clearance OBTAIN Transponder CODE & ALT Heading Bug RWY HDG Bug Flight Plan ENTER RAIM AS NECESSARY Annunciations NORMAL Before Taxi Auto Pilot Test PERFORM Standby Instruments & Taxi Light Interior Lighting Taxi Brief ACCOMPLISH Parking Brake RELEASE Brakes TEST Flight Instruments TAXI Engine Check Run-up Area CLEAR Parking Brake s Power Levers IDLE ECU Test INITIATE ECU Swap PERFORM Engine Gauges GREEN Parking Brake RELEASE Before Takeoff Canopy & Windows CLOSED & LATCHED Departure Briefing CLEARANCE (EMER PLAN) Single Engine Climb Performance Annunciator Panel UP Circuit Breakers Elevator Trim T/O Rudder Trim Traffic 360 CLEAR Engine Instruments GREEN Final FINAL IS CLEAR Runway RUNWAY IS CLEAR Landing Light (cleared for T/O) Pitot Heat Takeoff Roll HSI RWY HDG ### CFIRMED Brakes HOLD Power Levers FULL FORWARD % Load STABILIZED AT 90-100% Engine Gauges GREEN Brakes RELEASE AIRSPEED ALIVE VR 70-72 KTS. ROTATE After liftoff: Brakes TAP Landing Gear UP WITH POSITIVE RATE 500 Feet AGL Power REDUCE TO 90% VERIFY UP Landing Gear VERIFY UP

DA-42 NORMAL LIST 1000 Feet AGL Engine Gauges Transponder VERIFY ALT MODE Landing and Taxi Lights Level Off Power REDUCE TO 70% Engine Gauges Annunciator Panel CLEAR Exterior Lighting Maneuvers Clearing Turn Radio ANNOUNCE INTENTIS Bug Heading Bug APPROPRIATE Aircraft CFIGURED Clean Up UP Gear UP Power 60% Lights Alternate Air Bug Heading Bug APPROPRIATE Aircraft CFIGURED Descent/Approach ATIS (weather) OBTAIN Altimeters (3) Safety Harnesses FASTENED Gear Warning Horn TEST Gear Selector DOWN 3 GREEN (below 194) Engine Gauges GREEN s Parking Brake RELEASED Approach Landing and Taxi Lights Final Checks Landing Gear DOWN 3 GREEN ESTABLISH Landing and Taxi Lights After Landing When Clear of Runway Runway Clear ANNOUNCE Exterior Lighting Transponder VERIFY ALT MODE UP Pitot Heat Taxi Brief ACCOMPLISH Cool Down Time START (Idle 2 Mins.) Engine Shutdown Parking Brake Avionics Master Exterior Lighting 2 Min. Cool Down Time VERIFY Engine Masters (Left & Right) Hobbs & Tach Time RECORD Electric Master Exterior Lighting ALL Instrument & Flood Lights FLIGHT PLAN CLOSE DA-40F LISTS DA-40CS LISTS DA-42 LISTS 43

DA-42 NORMAL LIST DA-40F LISTS DA-40CS LISTS Aircraft Secure Gust Lock INSTALLED Tie-downs SECURED Chocks INSTALLED (main ldg gear) Pitot Mast Cover INSTALLED Parking Brake RELEASED (if Chocks Installed) Personal Items, Trash, etc. REMOVED Rear Door CLOSED & LOCKED Windows CLOSED & LATCHED Front Canopy CLOSED & LOCKED SOP Emergency s Event One engine Inoperative VMCA 68 KIAS One engine Inoperative Best Rate VYSE 82 KIAS NOTE: Vx is always less than Vy. For the DA-42 however, the actual value of Vx is below the minimum safe speed with one engine being inoperative. The minimum speed for best angle of climb was therefore raised to the value of Vy. OPERATING SPEEDS DA-42 LISTS Aircraft Weight Climbout Speed (V y ) Cruise Climb Speed ( UP) Approach Speed ( UP) Short Field Landing UP UP APP LDG LDG Below 3748 77 KIAS 85 KIAS MIN. 82 KIAS 76 KIAS 75 KIAS Above 3748 79 KIAS 86 KIAS MIN. 82 KIAS 78 KIAS 75 KIAS NOTE: Speeds listed for landing are referenced to the runway being made. Hold 82 KIAS until runway threshold for Normal landings. For Shortfield landings establish 75 KIAS on final 44

DA-42 MANEUVERS LIST Clearing Turn Radio Bug Heading Bug Aircraft Maneuvers Steep Turns ANNOUNCE INTENTIS APPROPRIATE CFIGURED AT LEAST 3,000 AGL Maneuvers Checklist Power Levers 50% LOAD 105-110 KIAS Enter 360 Turn: Bank Angle 50 (± 5 ) Power Levers INCREASE 10% Elevator BACK PRESSURE TO MAINT. ALT. Rudder COORDINATED Roll Out of Turn POWER AS NEEDED Repeat maneuver in opposite direction. Clean Up Checklist PERFORM Slow Flight (Minimum Controllable ) AT LEAST 3,000 AGL Maneuvers Checklist Power Levers 50% LOAD Before Landing Checklist Set Up: Specified OBTAIN (+5/-0 KTS) MAINTAIN ENTRY ALT ±50 FT Heading MAINTAIN ±10 Rudder COORDINATED Power Levers LDG Landing Gear APP Clean Up Checklist RECOVERY: FULL FORWARD MAINTAIN ±50 FT RETRACT RETRACT ACCELERATE TO VY (77 or 79 KIAS) RETRACT Power-On Stall (Departure Stalls) PERFORM AT LEAST 3,000 AGL Maneuvers Checklist Power Levers 50% LOAD and Gear VERIFY UP 90-100 KTS Perform Stall: s 65-100% LOAD Pitch SLOWLY PITCHING UP(~20 ) Rudder COORDINATED Directional Control MAINTAIN Stall Horn ANNOUNCE Stall Warning Stall Buffet ANNOUNCE Stalling Promptly Initiate Recovery Commercial Pilot ACS requires a recovery at the first indication of a stall. RECOVERY: PITCH REDUCE TO +3 NOSE HIGH POWER LEVERS FULL FORWARD GEAR AND FLAPS VERIFY UP RUDDER COORDINATED AIRSPEED ACCELERATE TO BLUE LINE (82 KIAS) Clean Up Checklist PERFORM DA-40F LISTS DA-40CS LISTS DA-42 LISTS 45

DA-42 MANEUVERS LIST DA-40F LISTS DA-40CS LISTS DA-42 LISTS Power-Off Stalls AT LEAST 3,000 AGL Maneuvers Checklist Power Levers 30% LOAD MAINTAIN ±100 FT Before Landing Checklist and Gear DECREASE TO 85 KIAS Descent ESTABLISH AT 85 KIAS Stalling ANNOUNCE When within 100 of stalling altitude: Power Levers IDLE MAINTAIN WITH PITCH Pitch HOLD UNTIL STALL Directional Control MAINTAIN Stall Horn ANNOUNCE Stall Warning Stall Buffet ANNOUNCE Stalling Promptly Initiate Recovery Commercial Pilot ACS requires a recovery at the first indication of a stall. PITCH REDUCE TO +3 NOSE UP POWER LEVERS FULL FORWARD LDG FLAPS RETRACT GEAR RETRACT WITH POSITIVE TREND RUDDER COORDINATED AIRSPEED ACCELERATE TO Vy (77 or 79 KIAS) APP FLAPS RETRACT Clean Up Checklist PERFORM VMC Demo NOTE: Recovers promptly by simultaneously reducing power sufficiently on the operating engine while decreasing the angle of attack as necessary to regain airspeed and directional control. Recovery SHOULD NOT be attempted by increasing the power on the simulated failed engine. USU uses the rule of thumb of RAISE THE DEAD engine for a zero sideslip condition with a bank into the GOOD engine. AT LEAST 4,000 AGL Maneuvers Checklist Power Levers 25% LOAD MAINTAIN Critical Engine (Left) IDLE AT 100 KIAS Right Engine Full AT 90 KIAS Slow the aircraft at a rate of 1 knot per sec until one of the following occurs: Loss of Directional Control Any Indication of a Stall Full Rudder Deflection RECOVERY: RIGHT ENGINE IDLE PITCH REDUCE AIRSPEED ACCELERATE ABOVE REDLINE RIGHT POWER LEVER SMOOTHLY ADVANCE TO FULL AIRSPEED BLUE LINE - 82 KIAS (±5 KTS) HEADING MAINTAIN ENTRY HDG ±20 MAINTAIN DIRECTIAL CTROL AND AIRSPEED Gear and VERIFY UP NOTE: Recovers when VMC Demo is terminated by the CFI or DPE- by retarding Right Engine to ~50% and bringing the Left Engine up to ~50-60%. Return to a normal cruise configuration should be initiated. 46

DA-42 MANEUVERS LIST Drag Demo AT LEAST 4,000 AGL Maneuvers Checklist Power Levers 25% LOAD Critical Engine (Left) IDLE AT 100 KIAS Right Engine Full AT 90 KIAS MAINTAIN 82 KIAS Heading ±10 VSI NOTE Clean Demonstration: Critical Engine (Left) Simulate Feather @20% VSI NOTE NOTE: The Critical Engine (Left) can be completely feathered to demonstrate the maneuver. Feathering the Critical engine is an abnormal procedure and must be briefed prior to attempting the maneuver. Gear/ Demonstration: Gear Selector DOWN 3 GREEN (below 194) VSI NOTE (APP) (below 137) VSI NOTE (LDG) (below 111) VSI NOTE RECOVERY: FLAPS APP GEAR UP FLAPS RETRACT Critical Engine (Left) Slowly Increase Clean Up UP Gear UP Power 60% Lights Alternate Air Bug Heading Bug APPROPRIATE Aircraft CFIGURED DA-40F LISTS DA-40CS LISTS DA-42 LISTS NOTE: If the engine was feathered, AFTER 30 seconds ENGINE RESTART is only permissible at Pressure of 8000 FT. or Below 47

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DA-42 ABNORMAL LIST Engine Failure In Flight Directional Control MAINTAIN AT OR ABOVE BLUE LINE (82 KNOTS) Power Levers FULL FORWARD & Gear RETRACT Identify % LOAD DEAD FOOT DEAD ENGINE (YAW) Verify Dead Engine RETARD POWER LEVER SLOWLY Engine Troubleshoot NOTE: For training purposes SIMULATE ECU swap and s Power IDLE Alternate Air PULL FAILED ENGINE TO CROSSFEED es (2) ECU Swap FAILED ENGINE TO ECU B Circuit Breaker (ECU) / RE If engine doesn t restart, proceed to ENGINE SECURE Engine Secure NOTE: For training purposes SIMULATE Alternator and s. (INOP Engine) IDENTIFY, VERIFY, Alternator (Inoperative Engine) (Inoperative Engine) Mayday ANNOUNCE Transponder SQUAWK 7700 Land as soon as practical. Restarting a Feathered Engine NOTE: AFTER 30 seconds ENGINE RESTART is only permissible at Pressure of 8000 FT. or Below 125 KIAS TO 145 KIAS Power Lever (Inop. Engine) AT OR BELOW 25% s Alternate Air Alternator Engine Master If engine does not restart: REDUCE BELOW 90 KIAS Starter ENGAGE Circuit Breakers Engine Fire In Flight Power Levers FULL FORWARD AT OR ABOVE BLUE LINE (82 KNOTS) & Gear RETRACT Failed Engine IDENTIFY, VERIFY (INOP Engine) IDENTIFY, VERIFY, Alternator (Inoperative Engine) (Inoperative Engine) Cabin Heat & Defrost Canopy UNLATCH (if necessary) MAX airspeed 120 KIAS Power Levers (2) Engine Masters (2) s (2) Mayday Call Electric Master Aircraft Engine Fire On Ground IDLE CSIDER EVACUATE (once stopped) 49 DA-40F LISTS DA-40CS LISTS DA-42 LISTS

DA-42 ABNORMAL LIST DA-40F LISTS DA-40CS LISTS DA-42 LISTS Electrical Fire On Ground Mayday Call CSIDER Electric Master Power Levers (2) IDLE Engine Masters (2) s (2) When engine and aircraft stopped: Canopy OPEN Evacuate Electrical Fire In Flight Emergency Switch Mayday Call CSIDER Avionics Master Electric Master Cabin Heat & Defrost Emergency Windows OPEN (as necessary) Canopy UNLATCH (if necessary) MAX airspeed 120 KIAS Land ASAP Gear Power Levers Vno Vne Emergency Descent NOTE: The purpose of the emergency descent is to get the severely stricken aircraft out of the sky and set up for landing. Reasons could include, fire, catastrophic engine failure, or medical issues. WARNING UP DOWN IDLE 155 KIAS 194 KIAS Landing Gear Unsafe Warning If on for more than 20 seconds BELOW 156 KIAS In cold temperatures, max airspeed is 110 KIAS Gear Selector RECYCLE NOTE: If landing gear extension unsuccessful: Continue with Manual Extension. If land gear retraction unsuccessful: Consider flight with landing gear down. Manual Extension of Landing Gear BELOW 156 KIAS Gear Indicator Lights TEST Electric Master Bus Voltage NORMAL Gear Selector DOWN Manual Extension Handle PULL If necessary BELOW 110 KIAS Apply moderate yawing Gear Indicator Lights DOWN 3 GREEN 50

DA-42 ABNORMAL LIST Alternator Failure If one alternator failed: Failed Alternator Bus Voltage MITOR Electrical Equipment REDUCE AS PRACTICABLE If both alternators failed: Avionics Master LH/RH Alternator Switches Transponder STANDBY Landing Gear DOWN Emergency Gear Extension PULL Stall/Pitot Heat All Lights WARNING: With both alternators failed, engine stoppage may occur once the main battery and ECU batteries are depleted. Expect power to last 30 minutes. Land as soon as possible CO Contamination Cabin Heat Ventilation Emergency Windows Forward Canopy Max speed 120 KIAS Land as soon as practical Both ECU A & B Failure During Flight OPEN OPEN UNLATCH ECU Test Button HOLD FOR AT LEAST 2 SEC If message reappears or cannot be reset: Flight LAND AT NEAREST SUITABLE AIRFIELD Prepare for possible engine failure. Door Open (On Ground Or In Flight) REDUCE Front Canopy LATCHED Rear Door (Don t touch a door in flight!) LATCHED Nose Baggage Doors LATCHED Canopy or rear door unlatched: BELOW 140 KIAS Leave the door as is and land ASAP at an appropriate airfield Nose Baggage Doors Unlatched: REDUCE UNTIL DOOR IS STABLE Land at the nearest suitable airfield. Separation of the baggage door may damage the propeller and lead to an engine failure. L/R ECU A or B Failure If ECU failure is on ground: Flight TERMINATE Aircraft Engine HAVE ED If ECU failure is in flight: ECU Test Button HOLD FOR AT LEAST 2 SEC If message resets: Flight CTINUE The engine must be serviced after landing. If message reappears or cannot be reset: Flight LAND AT NEAREST SUITABLE AIRFIELD Aircraft Engine HAVE ED DA-40F LISTS DA-40CS LISTS DA-42 LISTS 51

COLD WEATHER OPS

KLGU ELEV: 4457 CTAF: 122.80 ASOS: 135.275 KBMC ELEV: 4229 CTAF: 123.05 AWOS: 135.075 U10 ELEV: 4728 CTAF: 122.80