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. ALWAYS WITH THE AFM if you are in doubt about anything. 10. Line 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 Name: DA-42 LISTS Phone# ARROW LISTS

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 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 Pin 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 Nose gear/shock absorber Cowl exit Oil cooler Gascolator Nose REMOVE DRAIN & FUEL QUALITY 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

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 Annunciations NORMAL Brakes HOLD 1/4 OPEN RICH Tach Time CFIRM Fuel Computer ENTER AMOUNT LOWEST TANK V-speeds DO NOT power the avionics for more than 10 minutes with the engine and alternator off Engine Start Front Canopy POSITI 1 OR 2 Strobes Brakes HOLD (verify noise) DA-40F NORMAL LIST Prime (cold engine) 3 7 SECDS Propeller Area CLEAR Ignition Switch START After Start 1000 Oil Pressure GREEN Ammeter GREEN Fuel Flow GREEN LEAN FOR TAXI G1000 Setup Avionics Master ATIS (weather) OBTAIN Altimeters (G1000 & STBY) Clearance OBTAIN Transponder ALT Heading Bug RWY HDG Altitude Bug Flight Plan ENTER RAIM AS NECESSARY Annunciations NORMAL Before Taxi Taxi Brief ACCOMPLISH CO Detector PRESS TO TEST Taxi Light Interior Lighting Parking Brake RELEASE Brakes TEST Flight Instruments TAXI DA-40F LISTS DA-42 LISTS ARROW LISTS 7

DA-40F NORMAL LIST Pitot Heat DA-40F LISTS DA-42 LISTS ARROW LISTS 8 Engine Check Run-up Area CLEAR Parking Brake FULLEST TANK RICH 1800 RPM LEAN (all USU flights) 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 CLEAR Elevator Trim T/O Parking Brake RELEASE Carburetor Heat Traffic 360 CLEAR Final FINAL IS CLEAR Runway RUNWAY IS CLEAR Carburetor Heat COLD Landing Light (cleared for T/O) Takeoff Roll HSI RWY HDG ### CFIRMED Power POWER (no less than 2200 RPM) AIRSPEED ALIVE VR 59 KTS. ROTATE Accelerate to climbout speed 500 Feet AGL. VERIFY UP Landing Light Accelerate to cruise climb speed 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

DA-40F NORMAL LIST Clearing Turn Radio Altitude 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 Exterior Lighting Runway Clear ANNOUNCE 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 ARROW LISTS DA-42 LISTS DA-40F 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 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 Altitude 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 Altitude 800 AGL 95 KIAS Power ~2350 RPM Up On Pitch +4 Pivotal Altitude 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 Altitude AT LEAST 2,000 AGL Clearing Turns PERFORM Maneuver Checklist Bank ROLLING THRU 30 Power INCREASE ~200 RPM Pitch 7 + NOSE HIGH 95 KIAS (±10 KIAS) Enter 360º Turn Bank Angle 45 (±5 ) Elevator MAINTAIN BACK PRESS. Power INCREASE TO MAINTAIN AIRSPEED Rudder COORDINATED Roll-out of Turn LEAD BY 1/2 BANK Power REDUCE Clean Up Checklist PERFORM Slow Flight 1800 RPM APPROACH(<108 KTS) OR LANDING(<91KTS) Specified OBTAIN 5-10 KNOTS ABOVE STALL Pitch FOR APPROPRIATE AIRSPEED(+10 KTS) Altitude HOLD ASSIGNED ALT (+\- 100 FT) Heading +\- 10 White Arc Green Arc 49 KIAS - 91 KIAS 52 KIAS - 129 KIAS DA-40F LISTS DA-42 LISTS ARROW LISTS 11

DA-40F MANEUVER LIST DA-40F LISTS DA-42 LISTS ARROW LISTS Power On Stall Power Off Stall 1500 RPM As speed decreases to 66 KIAS: ALT ±100ft HDG ±10 UNLESS TURNING STALL (MAX 20 BANK) When speed reaches 66 KTS: SMOOTHLY APPLY FULL OPEN Pitch SMOOTHLY 12 NOSE UP AND HOLD Rudder MAINTAIN COORDINATI Stall Horn ANNOUNCE Stall Warning Stall Buffet ANNOUNCE Stalling Promptly Initiate Recovery Recovery- Simultaneously: Pitch REDUCE BACK PRESSURE 3 NOSE HIGH Wings LEVEL VERIFY FULL OPEN When increases above 60 KTS: Pitch 5-7 73 KIAS 1800 RPM APPROACH(<108 KTS) OR LANDING(<91 KTS) 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 Recovery- Pitch 3 NOSE HIGH Wings LEVEL VERIFY FULL OPEN T/O TING When increases above 60 KTS: Pitch 5-7 73 KIAS Power Carburetor Heat Lights Clean Up Checklist RPM COLD UP FULLEST TANK 12

DA-40F ABNORMAL LIST Rough Engine Engine Indications Fuel pump 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 UNTILL ENGINE STARTS If engine will not start proceed with ENGINE SECURE & EVACUATE ENGINE RESTART Stationary Propeller 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 Speed INCREASE ABOVE 130 KIAS CHECH If engine won t start, go to ENGINE SECURE & EVACUATE ENGINE SECURE Mayday ANNOUNCE Transponder SQUAK 7700 Safety Harnesses TIGHTEN Ignition Switch LANDING Touchdown slowest airspeed & commence EVACUATE Aircraft Canopy Airplane Fire Suppressant EVACUATE STOP OPEN EVACUATE IMMEDIATELY USE AS NECESSARY DA-40F LISTS DA-42 LISTS ARROW LISTS 13

DA-40F ABNORMAL LIST ARROW LISTS DA-42 LISTS DA-40F LISTS 14 Engine Fire In Flight Landing Site SELECT Cabin Heat MAX POWER Emergency Windows OPEN After touchdown proceed with 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 Loss Of RPM Carburetor Heat Friction Lock ADJUST 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 Smoke And Fire During Takeoff If takeoff can be abandoned: IDLE Cabin Heat Brakes APPLY All Electrical Switches Cabin Heat If takeoff cannot be abandoned: After climbing to a location where an emergency landing may be executed: TRIMMED FOR KIAS 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 Forward Canopy Land as soon as practical Low Volts On Ground PRESS 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 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 DA-40F ABNORMAL LIST 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 Land at nearest suitable airport within 30 minutes. Starter Engaged IDLE IDLE CUT Ignition Switch Terminate flight unscheduled maintenance is necessary. Defective Control Altitude MAINTAIN TO AIRPORT Descent TEST TO A HIGHER POWER TING A lean mixture can lead to engine roughness and a loss of power 15 DA-40F LISTS DA-42 LISTS ARROW LISTS

DA-40F ABNORMAL LIST DA-40F LISTS DA-42 LISTS ARROW LISTS High Cylinder Head Temperature ENRICH 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 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 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 BEST GLIDE SPEEDS Aircraft weight 2535 2205 1874 (lbs) UP 73 68 60 T/O 72 66 59 LDG 71 63 58 AT ANY TIME THE PIC MAY REFERENCE THE AFM FOR ITEMS NOT INCLUDED THIS LIST. 16

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 Circuit Breakers IN Control Lever IDLE CUT IDLE Prop Full Forward 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 Pin 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 17

DA-40CS PREFLIGHT LIST DA-40F LISTS DA-40CS LISTS ARROW 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 Nose gear/shock absorber Cowl exit Oil cooler Gascolator Nose REMOVE DRAIN & FUEL QUALITY 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. 18

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 Annunciations NORMAL 1/4 OPEN Tach Time CFIRM Fuel Computer ENTER AMOUNT LOWEST TANK V-speeds DO NOT power the avionics for more than 10 minutes with the engine and alternator off Cold Engine Start Front Canopy POSITI 1 OR 2 Strobes (verify noise) 1.5 Forward RICH 3-5 sec then Lean DA-40CS NORMAL LIST 1/2 Forward Propeller Area CLEAR Brakes HOLD 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 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 DA-40F LISTS DA-40CS LISTS ARROW LISTS 19

DA-40CS NORMAL LIST DA-40F LISTS DA-40CS LISTS ARROW LISTS 20 Flooded Engine Start Halfway Forward FULL LEAN Ignition Switch START 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 Altitude Bug Flight Plan RAIM Pitot Heat Ammeter Annunciations G1000 Setup OBTAIN OBTAIN 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 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 Parking Brake RELEASE

DA-40CS NORMAL LIST Canopy & Windows Departure Briefing Circuit Breakers Magnetos Prop Annunciator Panel Elevator Trim Parking Brake Traffic Final Runway Landing Light Pitot Heat Transponder Prop HSI Power VR Before Takeoff Takeoff Roll CLOSED & LATCHED CLEARANCE (EMER PLAN) IN BOTH T/O FULL FORWARD CLEAR T/O RELEASE 360 CLEAR FINAL IS CLEAR RUNWAY IS CLEAR (cleared for T/O) /ALT FULL FORWARD RWY HDG ### CFIRMED POWER (2680 +/- 20 RPM) ABORT T/O if more then +\- 20 AIRSPEED ALIVE 60 KTS. ROTATE Accelerate to climbout speed 500 Feet AGL Prop 2400. VERIFY UP Landing Light Accelerate to cruise climb speed Engine Gauges Transponder Taxi Light 1000 Feet AGL Level Off Cruise VERIFY ALT MODE Set to Power Table Landing Light Verify Off Verify Off Cruise Climb 70-85 kts Prop 1800-2400 RPM CHT 150-400 F Oil Temp 165-220 F Adjust Trim As Needed Fuel Tank Selector Fullest Tank Turn On Before Switching Fuel differential MUST NOT exceed 10 gallons between right & left tank Vso (dirty stall speed) Vs1 (clean stall speed) Vr (rotation speed) Vx (best angle) Vy (best rate) Vref (approach speed) Vglide (best glide speed) Vfe (flap extend speed) Reference Speeds 49 kts 52 kts 60 kts 60 kts 65 kts 65 kts 75 kts T/O 108 kts LDG 90 kts DA-40F LISTS DA-40CS LISTS ARROW LISTS 21

DA-40CS NORMAL LIST DA-40F LISTS DA-40CS LISTS ARROW LISTS Clearing Turn Radio Altitude 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 Lights Circuit Breakers Exterior Lighting ATIS (weather) Altimeter (3) Annunciator Panel Engine Gauges Fuel Quantity Safety Harnesses Clean Up Checklist Descent/Approach Checklist RPM UP FULLEST TANK IN OBTAIN CLEAR GREEN ENRICHEN FULLEST TANK FASTENED Seat Belts Trim Lights Prop Prop Landing Final Check APPROACH VERIFY FULLEST TANK VERIFY SECURED AT OR BELOW VFE T/O AS NEEDED BEFORE LANDING FULL RICH FULL FORWARD 13 MP LDG 65 70 KTS NOTE: If LANDING IN STRG WIND AND TURBULENCE USE A HIGHER APPROACH SPEED AND/ OR USE LESS FLAPS. Go Around Check FULL FORWARD 60 KTS T/O At 500 AGL or Safe Altitude 2400 RPM 70 KTS UP REFER TO LANDING 22

DA-40CS NORMAL LIST After Landing Check Exterior Lighting Runway Clear ANNOUNCE 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 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 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. DA-40F LISTS DA-40CS LISTS ARROW LISTS 23

ARROW LISTS DA-40CS LISTS DA-40F LISTS Blank Page

DA-40CS MANEUVER LIST Maneuvers Clearing Turn Radio ANNOUNCE INTENTIS Altitude Bug Heading Bug APPROPRIATE Aircraft CFIGURED Fuel pump should remain during maneuvers unless determined necessary for safety of flight Steep Turns Altitude AT LEAST 2,000 AGL Clearing Turns PERFORM Maneuver Checklist Bank ROLLING THRU 30 Power INCREASE ~200 RPM Pitch 7 + NOSE HIGH 95 KIAS (±10 KIAS) 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 Clean Up Checklist PERFORM Slow Flight 18 M.P. APPROACH(<108 KTS) OR LANDING(<91KTS) Specified OBTAIN 5-10 KNOTS ABOVE STALL Pitch FOR APPROPRIATE AIRSPEED(+10 KTS) Altitude HOLD ASSIGNED ALT (+\- 100 FT) Heading +\- 10 White Arc Green Arc Power Off Stall 49 KIAS - 91 KIAS 52 KIAS - 129 KIAS 18 M.P. APPROACH(<108 KTS) OR LANDING(<91 KTS) 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 Recovery- Pitch 3 NOSE HIGH Wings LEVEL VERIFY FULL OPEN T/O TING When increases above 60 KTS: Pitch 5-7 73 KIAS DA-40F LISTS DA-40CS LISTS ARROW LISTS 25

DA-40CS MANEUVER LIST DA-40F LISTS DA-40CS LISTS ARROW LISTS Power On Stall 15 M.P. As speed decreases to 66 KIAS: ALT ±100ft HDG ±10 UNLESS TURNING STALL (MAX 20 BANK) When speed reaches 66 KTS: SMOOTHLY APPLY FULL OPEN Pitch SMOOTHLY 12 NOSE UP AND HOLD Rudder MAINTAIN COORDINATI Stall Horn ANNOUNCE Stall Warning Stall Buffet ANNOUNCE Stalling Promptly Initiate Recovery Recovery- Simultaneously: Pitch REDUCE BACK PRESSURE 3 NOSE HIGH Wings LEVEL VERIFY FULL OPEN When increases above 60 KTS: Pitch 5-7 73 KIAS Ground Reference Maneuvers Winds IDENTIFY Emergency Landing Site SELECTED Altitude 800 AGL 95 KIAS Power ` 18 M.P. Up On Pitch +4 Pivotal Altitude 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 Clean Up Checklist Power Lights M.P. UP FULLEST TANK 26

DA-40CS ABNORMAL LIST Rough Engine Engine Indications Fuel pump 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 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 ENGINE RESTART Stationary Propeller 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 Speed INCREASE ABOVE 130 KIAS If engine won t start, go to ENGINE SECURE & EVACUATE ENGINE SECURE Mayday ANNOUNCE Transponder SQUAK 7700 Safety Harnesses TIGHTEN Ignition Switch LANDING Touchdown slowest airspeed & commence EVACUATE Aircraft Canopy Airplane Fire Suppressant EVACUATE STOP OPEN EVACUATE IMMEDIATELY USE AS NECESSARY DA-40F LISTS DA-40CS LISTS ARROW LISTS 27

DA-40CS ABNORMAL LIST DA-40F LISTS DA-40CS LISTS ARROW LISTS 28 Engine Fire In Flight Landing Site SELECT Cabin Heat MAX POWER Emergency Windows OPEN After touchdown proceed with 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 Loss Of RPM Carburetor Heat Friction Lock ADJUST Engine Fire During Start LEAN Cabin Heat Brakes HOLD FULL Electrical When the engine has stopped: Ignition Switch Canopy OPEN Airplane EVACUATE IMMEDIATELY Fire Suppressant USE AS NECESSARY Aircraft HAVE ED Smoke And Fire During Takeoff If takeoff can be abandoned: IDLE Cabin Heat Brakes APPLY All Electrical Switches If takeoff cannot be abandoned: Cabin Heat After climbing to a location where an emergency landing may be executed: TRIMMED FOR KIAS Cabin Heat All Electrical Switches Emergency Windows OPEN AS REQ D Front Canopy UNLATCH After Touchdown EVACUATE

DA-40CS ABNORMAL LIST 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 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 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 Land at nearest suitable airport within 30 minutes. Starter Engaged IDLE IDLE CUT Ignition Switch Terminate flight unscheduled maintenance is necessary. Defective Control Altitude MAINTAIN TO AIRPORT Descent TEST TO A HIGHER POWER TING A lean mixture can lead to engine roughness and a loss of power DA-40F LISTS DA-40CS LISTS ARROW LISTS 29

DA-40CS ABNORMAL LIST DA-40F LISTS DA-40CS LISTS ARROW LISTS High Cylinder Head Temperature ENRICH 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 Overvoltage Essential Bus ALTERNATOR Unnecessary Electrical Equipment Land at nearest airfield High Oil Temperature Oil Pressure CHT EGT 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 BEST GLIDE SPEEDS Aircraft weight 2535 2205 1874 (lbs) UP 73 68 60 T/O 72 66 59 LDG 71 63 58 AT ANY TIME THE PIC MAY REFERENCE THE AFM FOR ITEMS NOT INCLUDED THIS LIST. 30

DA42 Flight Deck Weather, Flight Plan, Weight & Balance Aircraft Documents & Inspections CURRENT Electrical Equipment ALL Gear Selector ED DOWN Circuit Breakers IN Power Levers IDLE Electrical Master Fuel Quantity LANDING Lights & Pitot Heat 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 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 FUEL QUALITY Cowling Exhaust DA-42 PREFLIGHT LIST Left Wing 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 Aileron Aileron Paddle Hinges & Safety pins Push Rod, Bracket, & Bonding Straps Trim Tab (don t touch!) Flap Counter Weight Hinges & Safety Pins Linkage Bonding Straps Tongue in Groove Assembly Fuel Cooler Air In & Outlet Main Gear FROM AFT Step Left Fuselage Rear Cabin Door & Window Antennas Fuselage Surface Tail Skid Tail Tie-Down REMOVE DA-40F LISTS DA-40CS LISTS DA-42 LISTS 31

DA-42 PREFLIGHT LIST DA-40F LISTS DA-40CS LISTS DA-42 LISTS Rudder and Elevator Static Wicks Trim Tab (don t touch!) Elevator FREEDOM OF MOVEMENT Rudder FREEDOM OF MOVEMENT Hinges Lightening Discharge Hinges Static Wicks Right Fuselage Fuselage Surface Rear Window Step Right Wing-Flap Main Gear FROM AFT Fuel Cooler Air in & Outlet Tongue in Groove Assembly Bonding Straps Hinges & Safety Pins Linkage Counter Weight Aileron Aileron Paddle Hinges & Safety pins Push Rod, Bracket, & Bonding Straps 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 FUEL QUALITY Cowling Exhaust Right Main Gear Right Gear Strut and Downlock Wheel & Tire Stall heat inhibitor switch Brakes & Hydraulic Line Gear Doors and Linkage Chocks REMOVE Nose Gear Strut and Lock Wheel & Tire Gear Door and Linkage Nose Section Baggage Doors CLOSED, LATCHED, & LOCKED OAT Probe and Battery Drain EPU Connection Landing and Taxi Lights 32

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 ECU s 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 NOTE: Ignition Switch must be held until TACH indicates >500 RPM. After Start Oil Pressure OUTSIDE RED IN 3 SEC Pitot Heat Voltage & Load INDICATI Annunciations RPM 900 +/- 20 Pitot Heat Engine Instruments GREEN Warm Up Time START Warm Up: Idle 2 Min. After 2 min warm up time, do not exceed 1400 RPM until Oil is > 50 C, and Coolant > 60 C PFD/MFD NORMAL MODE DA-40F LISTS DA-40CS LISTS DA-42 LISTS 33

DA-42 NORMAL LIST DA-42 LISTS DA-40CS LISTS DA-40F LISTS Avionics Master s CROSSFEED Circuit Breakers ED 34 G1000 Setup ATIS (weather) OBTAIN Altimeters (3) Clearance OBTAIN Transponder CODE & ALT Heading Bug RWY HDG Altitude 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 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) Annunciator Panel CLEAR UP Circuit Breakers Elevator Trim T/O Rudder Trim Single Engine Climb Performance Traffic 360 CLEAR Final FINAL IS CLEAR Runway RUNWAY IS CLEAR Line Up Procedures Landing Light (cleared for T/O) Pitot Heat HSI RWY HDG ### CFIRMED Brakes HOLD Power Levers FULL FORWARD % Load STABILIZED AT 100% Engine Gauges GREEN Brakes RELEASE AIRSPEED ALIVE VR 70-72 KTS. ROTATE 500 Feet AGL Power REDUCE TO 90% VERIFY UP Landing Gear VERIFY UP 1000 Feet AGL Engine Gauges Transponder VERIFY ALT MODE Landing and Taxi Lights

DA-42 NORMAL LIST Level Off Checklist Power REDUCE TO 70% Engine Gauges Annunciator Panel CLEAR Exterior Lighting Maneuvers Clearing Turn Radio ANNOUNCE INTENTIS Altitude Bug Heading Bug APPROPRIATE Aircraft CFIGURED Clean Up UP Gear UP Power 60% Lights Alternate Air Altitude 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 Brakes RELEASED Approach Landing and Taxi Lights Landing Gear Landing and Taxi Lights Final Checks DOWN 3 GREEN ESTABLISH After Landing When Clear of Runway Runway Clear Exterior Lighting Transponder Pitot Heat Cool Down Time Cool Down: Engine Shutdown ANNOUNCE VERIFY ALT MODE UP START Idle 2 Minutes Parking Brake Avionics Master Exterior Lighting 2 Min. Cool Down Time VERIFY Engine Masters (Left & Right) Tach Time Electric Master Strobes Instrument & Flood Lights FLIGHT PLAN After Engines Stop RECORD CLOSE DA-40F LISTS DA-40CS LISTS DA-42 LISTS 35

DA-42 NORMAL LIST DA-40CS LISTS DA-40F LISTS Aircraft Secure 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 36

DA-42 MANEUVERS LIST Clearing Turn Radio Altitude Bug Heading Bug Aircraft Maneuvers Steep Turns ANNOUNCE INTENTIS APPROPRIATE CFIGURED Altitude ABOVE 3000 FT Power Levers 50% LOAD Clearing Turns AT OR BELOW VA (120 or 126 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 Slow Flight (Minimum Controllable ) NOTE: SPECIFIED AIRSPEED: Establishes and maintains an airspeed at which any further increase in angle of attack, increase in load factor, or reduction in power would result in an immediate stall. Altitude ABOVE 3000 FT Power Levers 50% LOAD Clearing Turns Before Landing Checklist Set Up: Specified OBTAIN Pitch MAINTAIN ENTRY ALT. Rudder Control COORDINATED RECOVERY: Power Levers FULL FORWARD 1ST Notch of RETRACT Landing Gear RETRACT ACCELERATE TO VY (77 or 79 KIAS) 2ND Notch of RETRACT Power-On Stall (Departure Stalls) Altitude ABOVE 3000 FT AGL Power Levers 50% LOAD Clearing Turns and Gear VERIFY UP 90-100 KTS Perform Stall: s 65-100% LOAD Pitch SLOWLY PITCHING UP(~20 ) Rudder Control COORDINATED Directional Control MAINTAIN Stall Indications (ANNOUNCE): Stall Horn ANNOUNCE Stall Warning Stall Buffet ANNOUNCE Stalling RECOVERY: PITCH DECREASE TO BLUE LINE POWER LEVERS FULL FORWARD GEAR AND FLAPS VERIFY UP RUDDER CTROL COORDINATED AIRSPEED ACCELERATE TO BLUE LINE (82 KIAS) PITCH CTROL MAINTAIN ALTITUDE DA-40F LISTS DA-40CS LISTS DA-42 LISTS 37

DA-42 MANEUVERS LIST DA-40F LISTS DA-40CS LISTS DA-42 LISTS Power-Off Stalls Altitude ABOVE 3000 FT AGL Power Levers 50% LOAD Clearing Turns Before Landing Checklist and Gear 85 KIAS Descent ESTABLISH Stalling altitude ANNOUNCE Perform Stall: Power Levers IDLE Altitude MAINTAIN WITH PITCH Pitch HOLD UNTIL STALL Directional Control MAINTAIN Stall Indications (ANNOUNCE) Stall Horn ANNOUNCE Stall Warning Stall Buffet ANNOUNCE Stalling NOTE: Recognizes and recovers promptly as the stall occurs by simultaneously reducing the angle of attack, increasing power to maximum allowable and leveling the wings to return to a straight-andlevel flight attitude with a minimum loss of altitude appropriate for the airplane RECOVERY: PITCH DECREASE TO BLUE LINE POWER LEVERS FULL FORWARD 1ST NOTCH OF FLAPS RETRACT GEAR RETRACT WITH POSITIVE TREND RUDDER CTROL COORDINATED AIRSPEED ACCELERATE TO Vy (77 or 79 KIAS) 2ND NOTCH OF FLAPS RETRACT 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. Altitude Clearing Turns Power Levers Critical Engine (Left) Right Engine Full ABOVE 4000 FT AGL 25% LOAD IDLE AT 100 KIAS AT 90 KIAS Slow aircraft until one of the following: Loss of Directional Control Any Indication of a Stall Full Rudder Deflection RECOVERY: Right Engine IDLE Pitch DECREASE TO BLUE LINE (82 KIAS) Right Power Lever FULL FORWARD AT BLUE LINE MAINTAIN DIRECTIAL CTROL AND AIRSPEED Gear and VERIFY UP NOTE: Recovers when VMC Demo is terminated by the CFI or DPE- by retarding Rignt Engine to ~50% and bringing the Left Engine up to ~50-60%. Return to a normal cruise configuration should be initiated. 38

DA-42 MANEUVERS LIST Drag Demo Altitude ABOVE 4000 FT AGL Clearing Turns Power Levers 20% LOAD Critical Engine (Left) IDLE AT 100 KIAS Right Engine Full AT 90 KIAS Maintain 82 KIAS VSI NOTE Clean Demostration: Critical Engine (Left) Simulate Feather @20% VSI NOTE NOTE: The Critical Engine (Left) can be completly feathered to demostrate the maneuver. Feathering the Critical engine is an abnormal proceedure and must be breifed prior to attempting the maneuver. Gear/ Demostration: Gear Selector DOWN 3 GREEN (below 194) VSI NOTE (APP) (below 137) VSI NOTE (LND) (below 111) VSI NOTE RECOVERY: FLAPS APP GEAR UP FLAPS RETRACT Critical Engine (Left) Slowly Increase NOTE: If Right Engine was Feathered, AFTER 30 Seconds ENGINE RESTART is only permissible at Pressure Altitude of 8000 FT. or Below Clean Up UP Gear UP Power 60% Lights Alternate Air Altitude Bug Heading Bug APPROPRIATE Aircraft CFIGURED DA-40F LISTS DA-40CS LISTS DA-42 LISTS 39

DA-42 LISTS DA-40CS LISTS DA-40F LISTS Blank Page

Engine Failure In Flight Power Levers FULL FORWARD & Gear RETRACT AT OR ABOVE BLUE LINE (82 KNOTS) 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 Engine Secure NOTE: For training purposes SIMULATE Alternator and s. (INOP Engine) IDENTIFY, VERIFY, Alternator Inoperative Engine Inoperative Engine Restarting a Feathered Engine DA-42 ABNORMAL LIST Starter Pitch Attitude Alternator If Engine Does Not Restart ENGAGE DECREASE NOTE: CLEARING TURNS SHOULD BE PERFORMED BEFORE EACH MANEUVER OR UNTIL THE AREA IS SUFFICIENTLY CLEAR (CRAG/GUMPS) NOTE: ANNOUNCEMENTS SHOULD BE MADE WHEN SLOWING BELOW BLUE AND RED LINES Engine Fire In Flight Power Levers REDUCE INCREASE >68 KIAS: Power Levers FULL FORWARD AT OR ABOVE BLUE LINE (82 KNOTS) & Gear RETRACT (INOP Engine) IDENTIFY, VERIFY, Alternator Inoperative Engine Inoperative Engine Cabin Heat & Defrost Canopy UNLATCH (if necessary) MAX airspeed 120 KIAS DA-40F LISTS DA-40CS LISTS DA-42 LISTS NOTE: AFTER 30 Seconds ENGINE RESTART is only permissible at Pressure Altitude of 8000 FT. or Below 125 KIAS TO 145 KIAS Power Lever (Inop. Engine) AT OR BELOW 25% s Alternate Air Engine Master Engine Fire On Ground Power Levers (2) IDLE Engine Masters (2) s (2) Mayday call CSIDER Electrical Master When engine and aircraft stopped: Canopy OPEN Evacuate 41

DA-42 ABNORMAL LIST DA-40F LISTS DA-40CS LISTS DA-42 LISTS Electrical Fire On Ground Mayday call CSIDER Electrical 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 MAX 156 KIAS In cold temperatures MAX 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 Laniding Gear MAX 156 KIAS Gear Indicator Lights TEST Electric Master Bus Voltage NORMAL Gear Selector DOWN Manual Extension Handle PULL If necessary MAX 110 KIAS Apply moderate yawing Gear Indicator Lights DOWN 3 GREEN 42

ARROW PREFLIGHT LIST PA28R-200 Flight Deck NOSE Inspections ED (DATE & TIMES) Oil Quantity Weight & Balance WITHIN LIMITS Cowling, Propeller, & Spinner Documents ED (A.R.O.W) Engine Cooling Inlets EXTEND Alternator Belt Radio/Avionics Switch Landing Light Assembly Landing Gear DOWN Nose Wheel Assembly Ignition Switch Tire Battery Nose Strut Fuel Quantity Shimmy Dampener FULLEST TANK Gear Doors Landing Gear Lights Strainer DRAIN & Interior Lights Windshield CLEAN & Exterior Lights LEFT WING Pitot Heat / Strut Stall Indicator Landing Gear and Hydraulic lines Lights/Heat Gear Doors Battery Wheel Assembly Alternate Air OPERATI Rotor and Brake Pads RIGHT WING Tire Flap & Aileron Fuel Tank Sump DRAIN & Position Light & Wing Tip Wing Tie Down REMOVE Wing & Leading Edge Fuel Vent Line Fuel Quantity Wing & Leading Edge Fuel Filler Cap SECURE Stall Warning Switch Fuel Vent Line Pitot Mast & Static Port Wing Tie Down REMOVE Fuel Quantity Fuel Tank Sump DRAIN & Fuel Filler Cap SECURE Wheel Assembly Position Light & Wing Tip Rotor and Brake Pads Flap & Aileron Tire Strut Landing Gear and Hydraulic lines Gear Doors DA-40F LISTS DA-40CS LISTS DA-42 LISTS ARROW LISTS 43

ARROW LISTS DA-42 LISTS ARROW PREFLIGHT LIST DA-40CS LISTS DA-40F LISTS FUSELAGE AND EMPENNAGE Antennas Left Side of Fuselage Rudder (Vertical Stabilizer) Horizontal Stabilator Anti-Servo Tab MOVEMENT Tail Tie Down REMOVED Position Light Right Side of Fuselage Baggage Door SECURED F.O.D. Check VISUALLY CLEAR General Walk-Around RETRACT Rotate Speed Best Rate of Climb Best Rate (gear-up) Best Angle of Climb Best Angle (gear-up) Gear Up speed Gear-Down Speed Stalling (flaps & gear down) Stalling (flaps & gear up) Emergency Gear extend Best Glide angle 65 MPH 95 MPH 100 MPH 85 MPH 96 MPH 125 MPH 150 MPH 64 MPH 71 MPH 100 MPH 105 MPH 44

Before Engine Start Pilot Documents BOARD Parking Brake Times & Inspections ED Preflight Inspection Passenger Briefing Door CLOSED & LATCHED Circuit Breakers IN Seats ADJUSTED Seatbelts/Shoulder Harness FASTENED VERIFY LOWEST TANK Engine Start IDLE CUT- Prop FULL FORWARD OPEN 1/8 INCH Beacon FIRST FLIGHT OF DAY, Prime (w/ ) FIRST FLIGHT OF DAY (IF USED) Prop Area CLEAR Ignition Switch START 1. INCREASE (AFTER START) 2. 1000 RPM 3. Oil Pressure IN THE GREEN 4. Fuel Pressure Flooded Engine IDLE CUT- ½ TO FULL OPEN Ignition ENGAGE 1. (after start) INCREASE 2. REDUCE TO 1000 RPM 3. Oil Pressure IN THE GREEN 4. Fuel Pressure ARROW NORMAL LIST After Start LEAN FOR TAXI Avionics Master Transponder STANDBY Engine Instruments GREEN Ammeter POSITIVE INDICATI Taxi Brief Heading Indicator ATIS (weather) Altimeters Clearance Radio/Navs Exterior Lighting Interior Lighting Parking Brake Brakes Turning Instruments Before Taxi Taxi ACCOMPLISH OBTAIN OBTAIN VERIFY UP RELEASE TEST DA-40F LISTS DA-40CS LISTS DA-42 LISTS ARROW LISTS 45

ARROW NORMAL LIST DA-40F LISTS DA-40CS LISTS DA-42 LISTS ARROW LISTS Engine Check Run-up Area CLEAR Nose Wheel STRAIGHT Parking Brake VERIFY FULLEST TANK Flight Controls FREE AND CORRECT 2000 RPM 1. Alternate Air CYCLE 2. /EGT (FOR DENSITY ALT.) 3. Prop CYCLE 4. Magnetos (175 MAX/ 50 DIFF) 5. Oil Press./Temp IN GREEN ARC 6. Ammeter 7. (PRESS.) 8. Suction Gauge Within 5 (+/- 0.1 IN.) IDLE / 1000 RPM Friction Lock ADJUST Trims (2) FOR TAKE Flight Instruments AND ED Fuel Quantities ED Parking Brake RELEASE Cabin Door & Window Exterior Lighting Pitot Heat Transponder Departure Briefing Traffic Final Runway Before Takeoff CLOSED & LATCHED & VERIFY PRESSURE ALT CLEARANCE (EMER PLAN) ED FINAL IS CLEAR RUNWAY IS CLEAR DG Nose Wheel Brakes Engine Gauges At 65 MPH Pitch Attitude Brakes Landing Gear Pitch Attitude Landing Gear Propeller Engine Gauges Propeller Landing Lights Takeoff Roll RWY HDG ### CFIRMED CENTERLINE RELEASE FULL OPEN IN THE GREEN AIRSPEED ALIVE 65 MPH. ROTATE TO VY (95 MPH) TAP RETRACT TO VY (100 MPH) 500 Feet AGL 1000 Feet AGL VERIFY UP VERIFY UP BELOW REDLINE 100-110 MPH 25-2600 RPM LEAN 46

ARROW NORMAL LIST Level Off Checklist Descent/Approach Engine Gauges Heading Indicator Power Propeller Trims (2) Maneuver Check FULLEST TANK REDUCE TO 75% BHP LEAN Clearing Turn Radio ANNOUNCE INTENTIS APPROPRIATE Configure Aircraft 1. 2. Gear 3. Fuel pump Emergency Landing Site CHOSEN Safe Altitude AS NECESSARY FOR MANEUVER Landing Gear Propeller Power Lights Alternate Air Clean Up Check UP UP 2500 RPM 18 M.P. FULLEST TANK Landing Lights Radio/Navs ATIS (weather) Altimeters Engine Gauges s Before Landing Checklist Before Landing Check, ENRICH OBTAIN GREEN FULLEST TANK REVIEW s FULLEST TANK Landing Gear DOWN (BELOW 150 MPH) Landing Gear Lights DOWN 3 GREEN (21 MP) Propeller FULL FORWARD ENRICH Landing Lights, AS DESIRED Seatbelts/Shoulder Harness FASTENED Propeller Landing Gear Windsock Final Check FULL FORWARD DOWN 3 GREEN ESTABLISHED (85-95 MPH) ED After Landing When Clear of Runway Check Exterior Lighting Pitot Heat Transponder Trims (2) TURN TO STBY UP FOR TAKE- 47 DA-40F LISTS DA-40CS LISTS DA-42 LISTS ARROW LISTS

ARROW NORMAL LIST Shutdown Check SOP V-Speeds DA-42 LISTS DA-40CS LISTS DA-40F LISTS Parking Brake Exterior Lighting ALL, EXCEPT BEAC 1000 RPM Avionics Master IDLE CUT- AFTER PROPELLER STOPS CLOSED Beacon Ignition/Keys & OUT Hobbs/Tach Time RECORD Window CLOSED & LATCHED FLIGHT PLAN CLOSE Aircraft Secure Tie-downs (3) SECURED Chocks INSTALLED (MAIN LANDING GEAR) Parking Brake RELEASED (CHOCKS INSTALLED) Personal Items, Trash, etc REMOVED Door CLOSED & LATCHED Takeoff: Rotate Speed Normal Climb (ldg down) Short Fld T/O (flaps 25º) Best Angle-of-Climb Vx (ldg dwn) Vx (ldg up) Best Rate-of-Climb Vy (ldg dwn) Vy (ldg up) Enroute: Enroute Climb (flaps up) Max Gear Retract Speed Max. Turb. Pen. (Va, 2650 lbs) Max. Structural Cruise VNE Max. Flap Extend Speed Max Gear Extend Speed Landing: Normal (flaps up) Normal (flaps 40º) Short Fld. (flaps 40º) Engine Fail after T/O Best Glide Landing W/O power (flaps up) Landing W/O power (flaps dwn) 60-70 MPH 85-95 MPH 85 MPH 85 MPH 96 MPH 95 MPH 100 MPH 110 MPH 125 MPH 131 MPH 170 MPH 214 MPH 125 MPH 150 MPH 95-105 MPH 90-100 MPH 85 MPH 95 MPH 95-105 MPH 95 MPH 90 MPH ARROW LISTS Max. Crosswind 17 Knots 48

ARROW MANEUVERS LIST Soft Field Takeoff Taxi onto Runway FULL BACK PRESS Nose Wheel CENTERLINE Ailerons ADJUST FOR CROSS WIND VERIFY 25 (2nd NOTCH) FULL OPEN Elevator Control NOSE HIGH ATTITUDE Engine gauges/ /ALIVE Lift off AT LOWEST AIRSPEED Accelerate in Ground Effect Vx: Obstacles 85 MPH Vy: No Obstacles 95 MPH Brakes TAP Landing Gear (no runway left) RETRACT Pitch Attitude TO Vy (100 MPH) RETRACT (100 AGL) Soft Field Landing Enter Pattern AT OR BELOW 150 MPH 17 M.P. Before Landing Checklist Abeam the Point- 14 M.P. 110 MPH 10 (1st NOTCH) Base- 25 (2nd NOTCH) 100 MPH Final- 12 M.P. 90 MPH 40 (3rd NOTCH/) Final Check During Flare ADD SMALL AMOUNT OF POWER Touchdown MAINS FIRST/POWER IDLE Elevator Control HOLD NOSEWHEEL Braking AVOID USING/STOPPING Elevator Control FULL BACK PRESSURE Short Field Takeoff Taxi onto Runway USE ALL AVAILABLE Nose Wheel CENTERLINE Brakes HOLD FULL OPEN Engine gauges VERIFY 25 (2nd NOTCH) Brakes RELEASE Ailerons ADJUST FOR CROSSWIND Elevator Control SLIGHTLY NOSE DOWN ALIVE 60-65 MPH ROTATE Accelerate to Vx 85 MPH Brakes TAP Landing Gear (no runway left) RETRACT Accelerate to Vx (Clean) 96 MPH Announce OBSTACLE CLEAR (100 AGL) Pitch Attitude TO Vy (100 MPH) RETRACT (100 AGL) DA-40F LISTS DA-40CS LISTS DA-42 LISTS ARROW LISTS 49

ARROW MANEUVERS LIST ARROW LISTS DA-42 LISTS DA-40CS LISTS DA-40F LISTS Short Field Landing Enter Pattern AT OR BELOW 150 MPH 17 M.P. Before Landing Checklist Abeam the Point- 14 M.P. 110 MPH 10º (1st NOTCH) Base- 25 (2nd NOTCH) 100 MPH Final- 12 M.P. 85 MPH 40º (3rd NOTCH/) Final Check Runway Made THROTTLE TO IDLE Touchdown MAINS FIRST RETRACT Braking MAXIMUM W/O SKIDDING Elevator Control FULL BACK PRESSURE Maneuver Check Clearing Turn Radio ANNOUNCE INTENTIS APPROPRIATE Configure Aircraft 1. 2. Gear 3. Fuel pump Emergency Landing Site IDENTIFIED Safe Altitude AS NECESSARY FOR MANEUVER Slow Flight Altitude AT LEAST 2,000 AGL Clearing Turns PERFORM Before Landing Checklist Gear BELOW 150 MPH GEAR DOWN BELOW 125 MPH FLAPS TO FULL, E NOTCH AT A TIME 14 M.P. Slow speed to bottom of white arc 55-63 MPH ~19 M.P. Pitch APPROPRIATE AIRSPEED (+\- 10 KTS) Altitude ASSIGNED ALT (+\- 50 FT) Heading ASSIGNED HEADING (+\- 10 ) Rudder Control COORDINATED Landing Gear Recovery FULL OPEN RETRACT E NOTCH RETRACT ACCELERATE TO Vy (100 MPH) RETRACT (E NOTCH AT A TIME) 50

ARROW MANEUVERS LIST Power Off Stalls Altitude AT LEAST 2,000 AGL Clearing Turns PERFORM Before Landing Checklist 14 M.P. Gear DOWN BELOW 150 MPH As speed decreases to 85 MPH: APPLY E AT A TIME WITHIN WHITE ARC When speed reaches 85 MPH: IDLE Pitch 85 MPH (BEGIN STABILIZED DESCENT) Perform Stall- Within 100 of assigned altitude transition to a nose up attitude. Rudder MAINTAIN COORDINATI Directional Control MAINTAIN +\- 5 Stall Indications (ANNOUNCE): Stall Light ANNOUNCE STALL WARNING Stall Buffet ANNOUNCE STALLING Recovery- Pitch REDUCE BACKPRESSURE/ENTER SLOW FLT VERIFY FULL OPEN RETRACT E NOTCH Rudder Control COORDINATED Gear UP RETRACT E NOTCH AT TIME & Trim ACCELERATE Vy (100 MPH) Pitch /CLIMB Power On Stalls Altitude AT LEAST 2,000 AGL Clearing Turns PERFORM Before Landing Checklist 14 M.P. 75 MPH Perform Stall- FULL OPEN Pitch UP ~12 Rudder Control COORDINATED Heading MAINTAIN +\- 5 Stall Indications- Stall Light ANNOUNCE STALL WARNING Stall Buffet ANNOUNCE STALLING Full BUFFET/HIGH SINK RATE Recovery- Pitch REDUCE BACKPRESSURE/ENTER SLOW FLT VERIFY FULL OPEN VERIFY UP Rudder Control COORDINATED & Trim ACCELERATE Vy (100 MPH) Pitch /CLIMB DA-40F LISTS DA-40CS LISTS DA-42 LISTS ARROW LISTS 51

ARROW MANEUVERS LIST DA-40F LISTS DA-40CS LISTS DA-42 LISTS Steep Turns Altitude AT LEAST 1,500 AGL Clearing Turns PERFORM Before Landing Checklist 20 M.P. Bank 30 Pitch 4 + Nose high AT OR BELOW VA (±10 MPH) Enter 360º Turn- Bank Angle 50 (±5 ) Elevator MAINTAIN BACK PRESS. Power INCREASE TO MAINTAIN AIRSPEED Rudder COORDINATED Roll-out of Turn LEAD BY ½ BANK Power REDUCE Clean Up Checklist PERFORM Ground Reference Winds IDENTIFY Emergency Landing Site SELECTED Altitude 800 AGL 100 MPH Power 17 MP Up On Pitch +2 Pivotal Altitude 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 Clean Up Check ARROW LISTS Landing Gear Propeller Power Lights Alternate Air UP UP 2500 RPM 18 M.P. FULLEST TANK 52

ARROW ABNORMAL LIST Engine Failure In Flight & ENGINE RESTART 105 MPH Emergency Landing Spot SELECT Above 1,000 AGL ENGINE RESTART Alternate Air OPEN FULL RICH 3/4 OPEN SWITCH TANKS/ Ignition (Mags) BOTH/START Engine Gauges SECURE ENGINE & Forced Landing Radio 121.5/ MAYDAY Transponder 7700 & IDENT IDLE CUT- Propeller FULL FORWARD CLOSED Landing Gear Ignition Forced Landing: Seats/Harnesses SECURE Cabin Door UNLATCH PRIOR TO TOUCHDOWN Touchdown SLOWEST POSSIBLE AIRSPEED Engine Failure During Takeoff IDLE Brakes APPLY Runway CLEAR IF POSSIBLE RETRACT IDLE CUT Ignition Switch Engine Failure After Takeoff 95 MPH (FLAPS UP) 90 MPH(FLAPS DOWN) Landing Site SELECT (STRAIGHT AHEAD) Altitude ABOVE 1,000 AGL ENGINE RESTART Altitude BELOW 1,000 AGL SECURE ENGINE Seats/Harnesses SECURE Cabin Door UNLATCH (PRIOR TO TOUCHDOWN) Touchdown SLOWEST AIRSPEED POSSIBLE Fire During Engine Start Starter CTINUE CRANKING Engine Fails to Start- Starter CTINUE CRANKING SECURE ENGINE PERFORM Fire Extinguisher OBTAIN & USE Engine Area FOR DAMAGE Engine Starts- 1700 RPM FOR 1 MINUTE SECURE ENGINE PERFORM Engine Area FOR DAMAGE DA-40F LISTS DA-40CS LISTS DA-42 LISTS ARROW LISTS 53

ARROW ABNORMAL LIST DA-40F LISTS DA-40CS LISTS DA-42 LISTS ARROW LISTS Engine Fire During Flight SECURE ENGINE Checklist PERFORM 125 MPH UNTIL FIRE OUT Cabin Heat & Air FORCED LANDING/Nearest Airport PERFORM Fire Does NOT Extinguish 150 MPH UNTIL FIRE OUT FORCED LANDING/Nearest Airport PERFORM Wing Fire Navigation Lights Strobe Lights Pitot Heat Perform a Side-Slip to keep flames away from the fuel tank and cabin, Land ASAP Cabin Heat & Air Flight Vents All other switches Cabin Heat & Air Flight Cabin Fire Electrical Fire In Flight TERMINATE ASAP OPEN (EXCEPT MAGS) TERMINATE ASAP Ammeter With Excessive Charge Full Scale Deflection Alternator Non-Essential Equipment Flight TERMINATE ASAP Ammeter With 0 or No Charge Alternator Radios/Avionics Switches Circuit Breakers Alternator Ammeter Radios/Avionics Switches If Ammeter Does Not Reset- Alternator Non-Essential Equipment Flight TERMINATE ASAP NOTE: If battery is dead EMERGENCY GEAR EXTENSI procedure will need to be accomplished, and all lights will be INOP. Emergency Landing Gear Extension Circuit Breakers /IN Panel Lighting Gear Indicator Bulbs /ROTATE IF GEAR IS NOT INDICATING DOWN AND LOCKED BELOW 100 MPH Gear Position Selector DOWN Emergency Gear Lever Override ENGAGED Emergency Down Position SELECTED Rudder YAW SIDE TO SIDE 54

ARROW ABNORMAL LIST Landing With A Flat Main Tire Approach NORMAL Touchdown GOOD TIRE FIRST, THEN HOLD FLAT TIRE AS LG AS POSSIBLE. NOTE: AIRCRAFT MAY YAW CE FLAT TIRE TOUCHES DOWN. Cabin Door Open In Flight BELOW 100 MPH Cabin Vents CLOSED Storm Window OPEN If Upper latch is open CLOSE IF lower latch is open OPEN PULL DOOR CLOSED AND CLOSE UPPER LATCH Propeller Overspeed RETARD Oil Pressure Prop Control FULL DECREASE (THEN IF RESPDING) REDUCE BELOW 2700 RPM Loss Of Fuel Pressure FULL RICH SWITCH TANKS/ VERIFY Loss Of Oil Pressure Navigate NEAREST AIRPORT Power Adjustments AVOID (UNLESS NECESSARY) Flight END AS SO AS POSSIBLE DA-40F LISTS DA-40CS LISTS DA-42 LISTS ARROW LISTS 55

COLD WEATHER OPS

KLGU ELEV: 4457 CTAF: 122.80 ASOS: 135.275 KMLD ELEV: 4503 CTAF: 122.90 KBMC ELEV: 4229 CTAF: 123.05 AWOS: 135.075 U10 ELEV: 4728 CTAF: 122.80