checklists - usu
TRANSCRIPT
Checklists
= Surface-7,000 = Surface- 12,000 = UAV OPS area = 7,500-12,000
Rev. 03.19
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 REVISION.8. All checklists are arranged in the following order: some items might be combined for brevity.
PreflightNormal
ManeuversAbnormal (Pink)
9. Boxed checklists - - are performed as “Read and Do” checklists while dashed checklists - - are performed from memory.10. ALWAYS CHECK 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.
Name:_____________________________________________
Phone#____________________________________________
DA-40F CHECKLISTS
DA-40CS CHECKLISTS
DA-42 CHECKLISTS
Rev. 03.19
5Rev. 03.19
DA-40F PREFLIGHT CHECKLIST
DA 40F FligHt DeCk
Weather, Flight Plan, Weight & Balance COMPLETEAircraft Documents & Inspections CURRENTFlight Control Lock REMOVEIgnition Switch OFFElectrical Equipment ALL OFFEmergency Battery GUARDEDELT ARMED/INDICATOR OFFCircuit Breakers CHECK INMixture Control Lever IDLE CUTOFFThrottle IDLECarburetor Heat OFFMaster Switch ONFlaps CHECK OPERATIONFlight Controls CHECK FULL DEFLECTIONFlaps UPLights & Pitot Heat CHECK OPERATIONLights & Pitot Heat OFFG1000 Databases CURRENTFuel Quantity CHECKMaster Switch OFFTrim CHECK OPERATION Fire Extinguisher CHARGED & SECURED Baggage STOWED
leFt wing
Rear Ventilation Intake INSPECTLeft Gear Strut INSPECT Wheel & Tire INSPECTChocks REMOVEOpening Around Tank Drain INSPECTTank Drain CHECK FUEL QUALITYWing Surface INSPECT2 Stall Strips INSPECTStall Warning REMOVE COVER & INSPECT
Tank Filler INSPECT & CHECK FUEL QUANTITYFuel Tank Vents INSPECTPitot-Static Probe REMOVE COVER & INSPECTWing Tie-Down REMOVEWing Tip INSPECT2 Static Wicks INSPECT
Aileron
Aileron Paddle INSPECTHinges & Safety Pins INSPECT Push Rod, Bracket, & Bonding Straps INSPECT Trim Tab INSPECT (don’t touch!)
FlAp
Counter Weight INSPECTHinges & Safety Pins INSPECTPush Rod, Bracket, & Bonding Straps INSPECTTorsion Tube & Bonding Strap INSPECTMain Gear INSPECT FROM AFTBrakes & Hydraulic Line INSPECTBrake Pads CONFIRM SUFFICIENT THICKNESS
leFt FUselAge
Rear Cabin Door & Window INSPECTRear Door Pins INSPECTAntennas INSPECTFuselage Surface INSPECTTail Skid INSPECTTail Tie-Down REMOVE
rUDDer Cables & Eyelets INSPECT (left & right)Bottom Hinge, Mount, & Bonding Straps INSPECTStatic Wick INSPECTTrim Tab INSPECT(don’t touch!) Top Hinge INSPECT
DA-40F CHECKLISTSDA-42 CHECKLISTS
ARROW CHECKLISTS
Rev. 03.196
DA-40F PREFLIGHT CHECKLIST
elevAtor
Hinges INSPECT2 Static Wicks INSPECTTrim Tab, Linkage, Bolts & Safety Wire INSPECTLightening Discharge INSPECT
rigHt FUselAge
Tail Skid & Lower Fin INSPECTFuselage Skin INSPECTRear Window INSPECT
FlAp
Main Gear INSPECT FROM AFTBrakes & Hydraulic Line INSPECTBrake Pads CONFIRM SUFFICIENT THICKNESS Torsion Tube & Bonding Strap INSPECTHinges & Safety Pins INSPECTPush Rod, Bracket, & Bonding Straps INSPECTCounter Weight INSPECT
Aileron
Hinges & Safety Pins INSPECTPush Rod, Bracket, & Bonding Straps INSPECTAileron Paddle INSPECT
rigHt wing
2 Static Wicks INSPECTWing Tip INSPECTWing Tie-Down REMOVEFuel Tank Vents INSPECTTank Filler INSPECT & CHECK FUEL QUANTITY Wing Surface INSPECT2 Stall Strips INSPECTOpening Around Tank Drain INSPECTTank Drain CHECK FUEL QUALITY
Right Gear Strut INSPECTWheel & Tire INSPECTChocks REMOVE OAT Probe INSPECT
UnDersiDe
Nose Gear/Shock Absorber INSPECTCowl Exit INSPECTOil Cooler INSPECTGascolator DRAIN & CHECK FUEL QUALITY
nose Right Front Ventilation Intake INSPECTOil Level CHECK (recommended 6 qts.)Cowling & Fasteners INSPECTSpinner & Fasteners INSPECTPropeller INSPECTEngine Cooling Intakes INSPECTEngine Intake Air Filter INSPECTHeater Air Intake INSPECTOil Cooler Intake INSPECTAlternator & Battery Case Blast Tubes INSPECTLeft Front Ventilation Intake INSPECTNose Gear & Wheel INSPECTFront Canopy INSPECT AND CLEAN
AT ANY TIME THE PIC MAY REFERENCE THE AFM FOR ITEMS NOT INCLUDED ON THIS CHECKLIST.
DA-4
0F C
HECK
LISTS
DA-4
2 CH
ECKL
ISTS
ARRO
W CH
ECKL
ISTS
Rev. 03.19 7
DA-40F NORMAL CHECKLIST
BeFore engine stArt
Pilot Documents ONBOARDTimes & Inspections CHECKEDPreflight Inspection COMPLETEPassenger Briefing COMPLETERear Door CLOSED & LATCHEDBaggage SECURERudder Pedals ADJUSTEDSafety Harnesses FASTENEDQuadrant Friction Lock ADJUSTEDParking Brake SETCircuit Breakers CHECK INFlight Controls FREE & CORRECTEssential Bus Switch OFFAlternate Static CLOSEDAvionics Master Switch OFFMaster Switch ON
DO NOT power the avionics for more than 10 minutes with the engine and alternator off.
Annunciations NORMALBrakes HOLDThrottle 1/4 OPENMixture RICHTach Time CONFIRMFuel Computer ENTER AMOUNTFuel Selector LOWEST TANKV-speeds SET
engine stArt
Front Canopy POSITION 1 OR 2Strobes ONBrakes HOLDFuel Pump ON (verify noise)
Prime (cold engine) 3 – 7 SECONDSFuel Pump OFF Propeller Area CLEARIgnition 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
Throttle SET 1000 Oil Pressure GREENAmmeter GREEN Fuel Flow GREEN Mixture LEAN FOR TAXI
g1000 setUp
Avionics Master ONATIS (weather) OBTAINAltimeters (G1000 & STBY) SETClearance OBTAINTransponder CODE & ALTHeading Bug SET RWY HDGAltitude Bug SETFlight Plan ENTERRAIM CHECK AS NECESSARY Annunciations NORMAL
BeFore tAxi
Taxi Brief ACCOMPLISHCO Detector PRESS TO TESTTaxi Light ONInterior Lighting AS REQUIREDParking Brake RELEASEBrakes TESTFlight Instruments CHECK ON TAXI
DA-40F CHECKLISTSDA-42 CHECKLISTS
ARROW CHECKLISTS
Rev. 03.198
DA-40F NORMAL CHECKLIST
engine CHeCk
Run-up Area CLEARParking Brake SETFuel Selector FULLEST TANK Mixture RICHThrottle 1800 RPMMixture LEAN (all USU flights)
NOTE: Use Lean Assist Page to Set mixture 100°F rich of peak.
Carburetor Heat CHECKMagnetos CHECK (175/50)Engine Gauges GREEN Throttle IDLE CHECKThrottle SET 1000
BeFore tAkeoFF
Canopy & Windows CLOSED & LATCHEDDeparture Briefing CLEARANCE (EMER PLAN)Circuit Breakers CHECK INMagnetos BOTHFlaps SET T/OAnnunciator Panel CHECKElevator Trim SET T/OParking Brake RELEASETraffic 360° CLEARCarburetor Heat ONFinal “FINAL IS CLEAR”Runway “RUNWAY IS CLEAR”Carburetor Heat COLDLanding Light ON (cleared for T/O)Fuel Pump ONPitot Heat ON
tAkeoFF roll
HSI “RWY HDG ### CONFIRMED”Power “POWER CHECK” (no less than 2200 RPM)Airspeed “AIRSPEED ALIVE” VR “59 KTS. ROTATE”
Accelerate to climbout speed - 66 KIAS500 Feet Agl
Flaps VERIFY UPFuel Pump OFFLanding Light OFF
Accelerate to cruise climb speed - 73 KIAS
1000 Feet Agl
Engine Gauges CHECKTransponder VERIFY ALT MODE Taxi Light AS REQUIRED
level oFF CrUise
Power SET 2500 RPM Mixture LEAN
NOTE: Use Lean Assist Page to Set mixture 100°F rich of peak.
Power SET FOR CRUISENEVER allow engine RPM to exceed 2700
Engine Gauges CHECK Annunciator Panel CLEAR Exterior Lighting AS REQUIRED Fuel MANAGE
Fuel differential MUST NOT exceed 10 gallons between right & left tank
DA-4
0F C
HECK
LISTS
DA-4
2 CH
ECKL
ISTS
ARRO
W CH
ECKL
ISTS
Rev. 03.19 9
DA-40F NORMAL CHECKLIST
MAneUvers
Clearing Turn COMPLETERadio ANNOUNCE INTENTIONSAltitude Bug SET Heading Bug SETEmergency Landing Site CHOSENAirspeed APPROPRIATEAircraft CONFIGURED
Fuel pump and carburetor heat should remain OFF during maneuvers unless determined necessary for safety of flight
CleAn Up CHeCklist
Power SET _______ RPMCarburetor Heat COLDFuel Pump OFFFlaps UPLights AS REQUIREDFuel Selector FULLEST TANKMixture SET
DesCent/ApproACH CHeCklist
Circuit Breakers CHECK INExterior Lighting AS REQUIRED ATIS (weather) OBTAINAltimeter (G1000 & stby) SET _______Annunciator Panel CLEAREngine Gauges GREENFuel Quantity CHECKFuel Pump ONMixture ENRICHENCarburetor Heat ON(See: CARBURETOR HEAT SOP for proper carburetor
heat operation)Fuel Selector FULLEST TANKSafety Harnesses FASTENED
FinAl CHeCk
Carburetor Heat COLDFlaps SETAirspeed ESTABLISHLanding and Taxi Lights ON
AFter lAnDing CHeCk
Runway Clear ANNOUNCEExterior Lighting AS REQUIREDTransponder VERIFY ALT MODECarburetor Heat CHECK COLDThrottle SET 1000Mixture LEAN FOR TAXIFuel Pump OFFPitot Heat OFFFlaps UPTaxi Brief ACCOMPLISH
engine sHUtDown
Throttle SET 1000Parking Brake SETAvionics Master OFF Essential Bus Switch OFFExterior Lighting AS REQUIREDMixture IDLE CUTOFF
After engine stops:Ignition Switch OFFKey REMOVE FROM IGNITIONHobbs & Tach Time RECORDMaster Switch BAT & ALT OFFExterior Lighting ALL OFFInstrument & Flood Lights OFFFLIGHT PLAN CLOSE
DA-40F CHECKLISTSDA-42 CHECKLISTS
ARROW CHECKLISTS
Rev. 03.1910
DA-40F NORMAL CHECKLIST
AirCrAFt seCUre
Tie-Downs SECUREDChocks INSTALLED (main ldg gear) Pitot Cover INSTALLED Gust Lock INSTALLEDStall Warning Cover INSTALLEDParking Brake RELEASED (if Chocks Installed)Personal Items, Trash, etc. REMOVEDRear Door CLOSED & LOCKEDWindows CLOSED & LATCHEDFront Canopy CLOSED & LOCKED
reFerenCe speeDs
Vso (dirty stall speed) 49 ktsVs1 (clean stall speed) 52 ktsVr (rotation speed) 59 ktsVy (best rate of climb) 66 kts w/flaps T/O 73 kts w/flaps UPVref (normal approach speed) 71 ktsVref (short field approach speed) 66 ktsVglide (best glide speed) 73 ktsVfe (flap extend speed) T/O - 108 kts LDG - 90 ktsVa (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 carbure-tor icing is suspected or anytime the potential for
carburetor ice is present.• Carburetor heat will be ON for any descent
and may be turned OFF upon leveling-off.• Carburetor heat will be turned ON during the
Downwind and turned OFF with flap application on Base.
• Carburetor heat will be turned OFF 200 feet above MDA or DH on an instrument approach and then used as necessary after arriving at MDA or DH.
FUel pUMp sop
Fuel Pump 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-4
0F C
HECK
LISTS
DA-4
2 CH
ECKL
ISTS
ARRO
W CH
ECKL
ISTS
Rev. 03.19 11
DA-40F MANEUVER CHECKLIST
MAneUvers
Clearing Turn COMPLETERadio ANNOUNCE INTENTIONSAltitude Bug SET Heading Bug SETAirspeed APPROPRIATEAircraft CONFIGURED
Fuel pump and carburetor heat should remain OFF during maneuvers unless determined necessary for
safety of flight
groUnD reFerenCe MAneUvers
Winds IDENTIFYEmergency Landing Site SELECTEDAltitude 800’ AGLAirspeed 95 KIASPower ~2350 RPMFlaps UpFuel Pump OnPitch +4°
Pivotal Altitude CalculationsThe 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 AGLManeuvers Checklist COMPLETE Airspeed 95 KIAS (±10 KIAS)Bank ROLLING THRU 30°Power INCREASE ~200 RPMPitch +2.5-5° NOSE HIGH
Enter 360º TurnBank Angle 45°/50° (±5°)Elevator MAINTAIN BACK PRESS.Power INCREASE TO MAINTAIN AIRSPEEDRudder COORDINATEDRoll-out of Turn LEAD BY 1/2 BANKPower REDUCE
Repeat maneuver in opposite directionClean Up Checklist PERFORM
slow FligHt
Altitude AT LEAST 2,000 AGLManeuvers Checklist COMPLETEThrottle 1800 RPMFlaps APPROACH(<108 KTS) OR LANDING(<91KTS)Specified Airspeed OBTAINAirspeed 5-10 KNOTS ABOVE STALL WARNINGThrottle AS REQUIREDPitch FOR AIRSPEED(+10 KTS OR +5 KTS)Altitude HOLD ASSIGNED ALT (±100 FT/±50 FT)
Heading ±10°
reCovery-Throttle FULLAltitude & Hdg MAINTAINFlaps T/O, then UP when >75 KIASClean Up Checklist PERFORM
DA-40F CHECKLISTSDA-42 CHECKLISTS
ARROW CHECKLISTS
Rev. 03.1912
DA-40F MANEUVER CHECKLIST
power on stAll
Altitude AT LEAST 2,000 AGLManeuvers Checklist COMPLETEThrottle 1500 RPM
As speed decreases to 73 KIAS:ALT MAINTAIN ±100 FTHDG ±10° UNLESS TURNING STALL (MAX 20° BANK)
When speed reaches 73 KTS:Throttle SMOOTHLY APPLY FULL OPENPitch SMOOTHLY 18° NOSE UP AND HOLDRudder MAINTAIN COORDINATIONStall Horn ANNOUNCE “Stall Warning”Stall Buffet ANNOUNCE “Stalling”
Promptly Initiate RecoveryPrivate 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 HIGHWings LEVELThrottle VERIFY FULL OPEN
When Airspeed increases above 60 KTS:Pitch 5-7° Airspeed 73 KIASClean Up Checklist PERFORM
power oFF stAll
Altitude AT LEAST 2,000 AGLManeuvers Checklist COMPLETEThrottle 1800 RPMFlaps APPROACH(<108 KTS) OR LANDING(<91 KTS)Altitude MAINTAIN ±100 FT
When speed reaches 70 KTS:Throttle IDLEPitch FOR 70 KTS (STABILIZED DESCENT)Within 100’ of assigned altitude transition to a nose
up attitude.Rudder MAINTAIN COORDINATIONStall Horn ANNOUNCE “Stall Warning”Stall Buffet ANNOUNCE “Stalling”
Promptly Initiate RecoveryPrivate 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 HIGHWings LEVELThrottle VERIFY FULL OPENFlaps T/O SETTING
When Airspeed increases above 60 KTS:Pitch 5-7°Airspeed 73 KIASClean Up Checklist PERFORM
DA-4
0F C
HECK
LISTS
DA-4
2 CH
ECKL
ISTS
ARRO
W CH
ECKL
ISTS
Rev. 03.19 13
DA-40F CHECKLISTSDA-42 CHECKLISTS
ARROW CHECKLISTS
CHAnDelle
Altitude AT LEAST 2,000 AGLManeuvers Checklist COMPLETEVisual Reference Points SELECTAirspeed 95 KIAS
First 90° of Turn:Bank ROLL TO 30°Power FULLPitch SLOWLY INCREASE Rudder MAINTAIN COORDINATION90° Point MAX PITCH UP (12-15°)
Last 90° of TurnBank SLOWLY REDUCEPitch MAINTAIN MAX PITCH UP (12-15°)Rudder MAINTAIN COORDINATION180° Point WINGS LEVELAirspeed JUST ABOVE A STALLHeading ±10°
Recovery:Airspeed INCREASE TO 95 KIASAltitude MAINTAIN AS AIRSPEED BUILDSHeading ±10°Rudder MAINTAIN COORDINATION
Repeat maneuver in opposite directionClean Up Checklist PERFORM
lAzy eigHts
Altitude AT LEAST 2,000 AGLManeuvers Checklist COMPLETEVisual Reference Points SELECTPower 2250 - 2300 RPMAirspeed 95 KIAS
Slowly begin increasing pitch and bank simultaneously.
At 45° Point:Pitch MAX PITCH UPBank APPROX. 15°
At 90° Point:Pitch LEVEL WITH HORIZONBank APPROX. 30°Airspeed MINIMUM AIRSPEED ABOVE A STALL
At 135° Point:Pitch MAX PITCH DOWN Bank APPROX. 15°
At 180° Point:Pitch LEVEL WITH HORIZONBank WINGS LEVELAirspeed ±10 KTS FROM ENTRY SPEEDAltitude ±100 FT FROM ENTRY ALTHeading ±10°
Repeat maneuver in opposite directionClean Up Checklist PERFORM
DA-40F MANEUVER CHECKLIST
Rev. 03.1914
DA-4
0F C
HECK
LISTS
DA-4
2 CH
ECKL
ISTS
ARRO
W CH
ECKL
ISTS
steep spirAl
Altitude AT LEAST 4,000 AGLThis maneuver must be recovered by 1,500’ AGL
according to USU SOPs and Commercial ACS.Maneuvers Checklist COMPLETEWinds IDENTIFYGround Reference Point SELECTFuel Pump ON
When over selected point:Power IDLECarburetor Heat ONAirspeed TRIMMED FOR BEST GLIDE
While performing maneuver:Airspeed BEST GLIDE ±10 KTSBank NOT TO EXCEED 60°Ground Track MAINTAIN AROUND POINTEngine 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
CleAn Up CHeCklist
Power SET _______ RPMCarburetor Heat COLDFuel Pump OFFFlaps UPLights AS REQUIREDFuel Selector FULLEST TANKMixture SET
DA-40F MANEUVER CHECKLIST
Rev. 03.19 15
DA-40F ABNORMAL CHECKLIST
roUgH engine
Engine Indications CHECK Fuel Pump ONIgnition BOTHCarburetor Heat ONMixture SET FOR SMOOTH RUNNINGFuel Selector CHECKThrottle/Mixture TRY VARIOUS SETTINGSIf engine is still running roughly, Land ASAP- Prepare
for engine failure.engine FAilUre
Airspeed TRIMMED FOR BEST GLIDELanding Site SELECTIf propeller is windmilling ENGINE RESTART Windmilling PropellerIf propeller is stationary ENGINE RESTART Stationary PropellerIf restart is unsuccessful proceed with ENGINE SECURE
engine restArt winDMilling propeller
Airspeed 70-130 KIASFuel Pump ONIgnition BOTHCarburetor Heat ONMixture SET APPROPRIATEFuel Selector CHECKIf engine does not start: Mixture FULL LEANMixture PUSH FORWARD UNTIL ENGINE STARTSIf engine will not start proceed with ENGINE SECURE & EVACUATE
engine restArt stAtionAry propeller
Airspeed 70-80 KIASFuel Selector CHECKMixture SET APPROPRIATECarburetor Heat ONElectrical equipment ALL OFFAvionics Master Switch OFFMaster Switch BATTERY ONFuel Pump ONIgnition Switch STARTIf starter is inoperative: Expect at least 1000’ altitude lossIgnition Switch BOTHAirspeed INCREASE ABOVE 130 KIASMixture CHECKIf engine won’t start, go to ENGINE SECURE & EVACUATE
engine seCUre
Mayday ANNOUNCETransponder SQUAWK 7700Fuel Selector OFFSafety Harnesses TIGHTENIgnition Switch OFF
When certain field can be made:Flaps SET LANDINGMaster Switch OFFTouchdown slowest airspeed & commence EVACUATE
evACUAte
Aircraft STOPCanopy OPENAirplane EVACUATE IMMEDIATELYFire Suppressant USE AS NECESSARY
DA-40F CHECKLISTSDA-42 CHECKLISTS
ARROW CHECKLISTS
Rev. 03.1916
DA-40F ABNORMAL CHECKLIST
engine Fire in FligHt
DA-40F CHECKLISTSDA-42 CHECKLISTS
ARROW CHECKLISTS
Landing Site SELECTCabin Heat OFFFuel Selector OFFThrottle MAX POWERFuel Pump OFFMaster Switch ONEmergency Windows/Canopy OPEN AS REQUIRED
If fire persists:Emergency Descent INITIATEFlaps UPAirspeed INCREASE
WARNING: VNO = 129 KIAS, and VNE = 178 KIAS
Bank 30-45°Once fire is extinguished:
Bank WINGS LEVELPitch GENTLY BRING NOSE UPAirspeed ESTABLISH BEST GLIDE
Proceed with ENGINE SECURE and EVACUATEeleCtriCAl Fire in FligHt
Emergency Switch ONMaster Switch OFFCabin Heat OFFLanding Site SELECTEmergency Windows OPEN AS REQUIREDFront Canopy UNLATCH AS REQUIREDFire Suppressant USE AS NECESSARY
Land as soon as possible
eleCtriCAl Fire on tHe groUnD
Master Switch OFFThrottle IDLEMixture IDLE CUTOFF
When the engine has stopped:Ignition Switch OFFCanopy OPENAirplane EVACUATE IMMEDIATELYFire Suppressant USE AS NECESSARY
engine/CArBUretor Fire DUring stArt
Starter CONTINUE CRANKINGIf engine starts:Starter CEASE CRANKINGThrottle SET RPM TO 1800 FOR 4 MINSCabin Heat OFFIf engine does not start:Mixture LEANThrottle FULLElectrical Fuel Pump OFFFuel Selector OFFMaster Switch OFFWhen the engine has stopped:Ignition Switch OFFCanopy OPENAirplane EVACUATE IMMEDIATELYFire Suppressant USE AS NECESSARYAircraft HAVE INSPECTED
loss oF rpMFuel Pump ONFuel Selector CHECKCarburetor Heat ONFriction Lock ADJUST
DA-4
0F C
HECK
LISTS
DA-4
2 CH
ECKL
ISTS
ARRO
W CH
ECKL
ISTS
Rev. 03.19 17
engine Fire in FligHt
DA-40F CHECKLISTSDA-42 CHECKLISTS
ARROW CHECKLISTS
Landing Site SELECTCabin Heat OFFFuel Selector OFFThrottle MAX POWERFuel Pump OFFMaster Switch ONEmergency Windows/Canopy OPEN AS REQUIRED
If fire persists:Emergency Descent INITIATEFlaps UPAirspeed INCREASE
WARNING: VNO = 129 KIAS, and VNE = 178 KIAS
Bank 30-45°Once fire is extinguished:
Bank WINGS LEVELPitch GENTLY BRING NOSE UPAirspeed ESTABLISH BEST GLIDE
Proceed with ENGINE SECURE and EVACUATEeleCtriCAl Fire in FligHt
Emergency Switch ONMaster Switch OFFCabin Heat OFFLanding Site SELECTEmergency Windows OPEN AS REQUIREDFront Canopy UNLATCH AS REQUIREDFire Suppressant USE AS NECESSARY
Land as soon as possible
sMoke AnD Fire DUring tAkeoFF
If takeoff can be abandoned:Throttle IDLECabin Heat OFFBrakes APPLYFuel Selector OFFAll Electrical Switches OFFAirplane EVACUATEIf takeoff cannot be abandoned:
After climbing to a location where an emergency landing may be executed:
Airspeed TRIMMED FOR BEST GLIDEFuel Selector OFFFuel Pump OFFCabin Heat OFFAll Electrical Switches OFFEmergency Windows OPEN AS REQ’DFront Canopy UNLATCH AS REQUIREDAfter Touchdown EVACUATE
Door open (on groUnD or in FligHt)Airspeed SLOW TO VA
Front Canopy CHECK LATCHEDRear Door (Don’t touch a door in flight!) CHECK LATCHEDIf rear door appears unlatched in flight, leave as is
and land ASAP at an appropriate airfield
Co DeteCtor illUMinAteD
Test/Reset Button PRESSIf alert continues:Cabin Heat OFFVentilation OPENEmergency Windows OPENFront Canopy UNLATCH
Land as soon as practical
low volts on groUnD
Throttle SET 1200 RPMMaster Switch LEAVE ONElectrical Equipment OFFAmmeter CHECKIf caution light does not extinguish and the ammeter
reads zero:Master Switch RECYCLE ALTERNATORIf caution light continues and ammeter reads zero:
Prepare to terminate flight
low volts in FligHt
Master Switch LEAVE ONElectrical Equipment OFF (IF NOT REQ’D)Ammeter CHECKMaster Switch RECYCLE ALTERNATORIf caution light does not extinguish and the ammeter
reads zero:Proceed with ALTERNATOR FAILURE
overvoltAge
Essential Bus ONMaster Switch ALTERNATOR OFFUnnecessary Electrical Equipment OFF
Land at nearest airfield. Expect only 30 mins. of usable electric power.
stArter engAgeD
Throttle IDLEMixture IDLE CUTOFFIgnition Switch OFFMaster Switch OFF
Terminate flight unscheduled maintenance is necessary.
DA-40F ABNORMAL CHECKLIST
Rev. 03.1918
AlternAtor FAilUre
Circuit Breakers CHECK
If no circuit breakers had popped:Ammeter CHECK
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 ONElectrical Load REDUCE TO MINIMUMVoltage CHECK REGULARLYElectrical System MONITORLand at nearest suitable airport within 30 minutes
If aircraft battery becomes depleted:Emergency Battery Switch UNGUARD and ON
DeFeCtive MixtUre Control
Altitude MAINTAIN TO AIRPORTDescent TEST TO A HIGHER POWER SETTING
A lean mixture can lead to engine roughness and a loss of power.
HigH CylinDer HeAD teMperAtUre
Mixture ENRICHOil Pressure CHECK
If oil pressure is low proceed withLOW OIL PRESSURE:
If oil pressure is normal:Throttle REDUCEAirspeed INCREASE
HigH FUel Flow
Fuel Pressure CHECKLow fuel pressure indicates a possible leak in the
systemFuel Quantity MONITORPower Setting CHECKLand as soon as practicable to avoid fuel exhaustion
low FUel pressUre
Fuel Pump ONFuel Quantity CHECKFuel Selector CHECKMixture ADJUST
Land as soon as practicable; prepare for engine failure
HigH oil teMperAtUre
Oil Pressure CHECKIf oil pressure is low proceed with
LOW OIL PRESSUREIf oil pressure is normal:
Mixture ENRICHThrottle REDUCEAirspeed INCREASE
Land as soon as practicable
low oil pressUre
Throttle REDUCE
Oil Temperature MONITORCHT MONITOR
Land as soon as practicable; prepare for engine failure
DA-4
0F C
HECK
LISTS
DA-4
2 CH
ECKL
ISTS
ARRO
W CH
ECKL
ISTS
DA-40F ABNORMAL CHECKLIST
Rev. 03.19 19
DA-40F ABNORMAL CHECKLISTDA-40F CHECKLISTS
DA-42 CHECKLISTSARROW CHECKLISTS
FligHt into iCing
Icing Area LEAVE
Pitot Heat ON
Cabin Heat ON/DEFROSTRPM INCREASECarburetor Heat ONEmergency Windows OPEN IF REQUIRED
If Pitot Heat fails, the alternate static valve can be opened and emergency windows closed.
CAUTION: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:
Throttle IDLEAilerons NEUTRALRudder FULL DEFLECTION OPPOSITE OF SPINElevator FULLY FORWARDFlaps UP
When rotation has stopped:Rudder NEUTRALElevator PULL CAREFULLYDescent RECOVER INTO NORMAL FLIGHT
WARNING:Never allow the airplane’s speed to exceed VNE
BEST GLIDE SPEEDS
Aircraft weight (lbs)
2535 2205 1874
Flaps UP 73 68 60Flaps T/O 72 66 59Flaps LDG 71 63 58
AT ANY TIME THE PIC MAY REFERENCE THE AFM FOR ITEMS NOT INCLUDED ON THIS CHECKLIST.
Rev. 03.1920
Blank Page
Rev. 03.19 21
DA 40Cs FligHt DeCk
Weather, Flight Plan, Weight & Balance COMPLETEAircraft Documents & Inspections CURRENTFlight Control Lock REMOVEIgnition Switch OFFElectrical Equipment ALL OFFEmergency Battery GUARDEDELT ARMED/INDICATOR OFFCircuit Breakers CHECK INMixture Control Lever IDLE CUTOFFProp FULL FORWARDThrottle IDLEMaster Switch ONFlaps CHECK OPERATIONFlight Controls CHECK FULL DEFLECTIONFlaps UPLights & Pitot Heat CHECK OPERATIONLights & Pitot Heat OFFG1000 Databases CURRENTFuel Quantity CHECKMaster Switch OFFTrim CHECK OPERATION Fire Extinguisher CHARGED & SECURED Baggage STOWED
leFt wing
Rear Ventilation Intake INSPECTLeft Gear Strut INSPECT Wheel & Tire INSPECTChocks REMOVEOpening Around Tank Drain INSPECTTank Drain CHECK FUEL QUALITYWing Surface INSPECT2 Stall Strips INSPECTStall Warning REMOVE COVER & INSPECT
Tank Filler INSPECT & CHECK FUEL QUANTITYFuel Tank Vents INSPECTPitot-Static Probe REMOVE COVER & INSPECTWing Tie-Down REMOVEWing Tip INSPECT2 Static Wicks INSPECT
Aileron
Aileron Paddle INSPECTHinges & Safety Pins INSPECT Push Rod, Bracket, & Bonding Straps INSPECT Trim Tab INSPECT (don’t touch!)
FlAp
Counter Weight INSPECTHinges & Safety Pins INSPECTPush Rod, Bracket, & Bonding Straps INSPECTTorsion Tube & Bonding Strap INSPECTMain Gear INSPECT FROM AFTBrakes & Hydraulic Line INSPECTBrake Pads CONFIRM SUFFICIENT THICKNESS
leFt FUselAge
Rear Cabin Door & Window INSPECTRear Door Pins INSPECTAntennas INSPECTFuselage Surface INSPECTTail Skid INSPECTTail Tie-Down REMOVE
rUDDer Cables & Eyelets INSPECT (left & right)Bottom Hinge, Mount, & Bonding Straps INSPECTStatic Wick INSPECTTrim Tab INSPECT(don’t touch!) Top Hinge INSPECT
DA-40CS PREFLIGHT CHECKLISTDA-40F CHECKLISTS
DA-40CS CHECKLISTSARROW CHECKLISTS
Rev. 03.1922
DA-40CS PREFLIGHT CHECKLIST
elevAtor
Hinges INSPECT2 Static Wicks INSPECTTrim Tab, Linkage, Bolts & Safety Wire INSPECTLightening Discharge INSPECT
rigHt FUselAge
Tail Skid & Lower Fin INSPECTFuselage Skin INSPECTRear Window INSPECT
FlAp
Main Gear INSPECT FROM AFTBrakes & Hydraulic Line INSPECTBrake Pads CONFIRM SUFFICIENT THICKNESS Torsion Tube & Bonding Strap INSPECTHinges & Safety Pins INSPECTPush Rod, Bracket, & Bonding Straps INSPECTCounter Weight INSPECT
Aileron
Hinges & Safety Pins INSPECTPush Rod, Bracket, & Bonding Straps INSPECTAileron Paddle INSPECT
rigHt wing
2 Static Wicks INSPECTWing Tip INSPECTWing Tie-Down REMOVEFuel Tank Vents INSPECTTank Filler INSPECT & CHECK FUEL QUANTITY Wing Surface INSPECT2 Stall Strips INSPECTOpening Around Tank Drain INSPECTTank Drain CHECK FUEL QUALITY
Right Gear Strut INSPECTWheel & Tire INSPECTChocks REMOVE OAT Probe INSPECT
UnDersiDe
Nose Gear/Shock Absorber INSPECTCowl Exit INSPECTOil Cooler INSPECTGascolator DRAIN & CHECK FUEL QUALITY
nose Right Front Ventilation Intake INSPECTOil Level CHECK (recommended 6 qts.)Cowling & Fasteners INSPECTSpinner & Fasteners INSPECTPropeller INSPECTEngine Cooling Intakes INSPECTEngine Intake Air Filter INSPECTHeater Air Intake INSPECTOil Cooler Intake INSPECTLeft Front Ventilation Intake INSPECTNose Gear & Wheel INSPECTFront Canopy INSPECT AND CLEAN
AT ANY TIME THE PIC MAY REFERENCE THE AFM FOR ITEMS NOT INCLUDED ON THIS CHECKLIST.
DA-4
0F C
HECK
LISTS
DA-4
0CS C
HECK
LISTS
ARRO
W CH
ECKL
ISTS
Rev. 03.19 23
DA-40F CHECKLISTSDA-40CS CHECKLISTS
ARROW CHECKLISTSDA-40CS NORMAL CHECKLIST
BeFore engine stArt
Pilot Documents ONBOARDTimes & Inspections CHECKEDPreflight Inspection COMPLETEPassenger Briefing COMPLETERear Door CLOSED & LATCHEDBaggage SECURERudder Pedals ADJUSTEDSafety Harnesses FASTENEDQuadrant Friction Lock ADJUSTEDParking Brake SETCircuit Breakers CHECK INAlternate Air CLOSEDFlight Controls FREE & CORRECTEssential Bus Switch OFFAlternate Static CLOSEDAvionics Master Switch OFFMaster Switch ON
DO NOT power the avionics for more than 10 minutes with the engine and alternator off
Annunciations NORMALThrottle 1/4 OPENTach Time CONFIRMFuel Computer ENTER AMOUNTFuel Selector LOWEST TANKV-speeds SET
ColD engine stArt
Front Canopy POSITION 1 OR 2Strobes ONFuel Pump ON (verify noise) Throttle 1.5” ForwardMixture RICH 3-5 sec then LEANThrottle 1/2” Forward
Propeller Area CLEARBrakes HOLDIgnition 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 FiresMixture Full RICHOil Pressure GREENFuel Pump OFF Ammeter GREENFuel Pressure GREEN (14-35 psi)Annunciations NORMALThrottle SET 1000Mixture LEAN FOR TAXI
Hot engine stArt
Front Canopy POSITION 1 OR 2Strobes ONFuel Pump ON (verify noise) Throttle 1.5” ForwardMixture RICH 1-3 sec then LeanBrakes HOLDPropeller Area CLEARIgnition Switch START
After Engine FiresMixture Full RICHOil Pressure GREENFuel Pump OFF Ammeter GREENFuel Pressure GREEN (14-35 psi)Annunciations NORMALThrottle SET 1000Mixture LEAN FOR TAXI
Rev. 03.1924
DA-40CS NORMAL CHECKLIST
FlooDeD engine stArt
Fuel Pump OFFThrottle HALFWAY FORWARDMixture FULL LEANIgnition 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.
Throttle RETARD AFTER ENGINE FIRESAfter Engine Fires
Mixture Full RICHOil Pressure GREENAmmeter GREENFuel Pressure GREEN (14-35 psi)Annunciations NORMALThrottle SET 1000Mixture LEAN FOR TAXI
g1000 setUp
Avionics Master ONATIS (weather) OBTAINAltimeters (3) SETClearance OBTAINTransponder CODE & ALTHeading Bug SET RWY HDGAltitude Bug SETFlight Plan ENTERRAIM CHECK AS NECESSARY Pitot Heat TEST (ammeter must rise)Ammeter GREENAnnunciations NORMAL
BeFore tAxi
Auto Pilot Test PERFORMTaxi Brief ACCOMPLISHTaxi Light ONInterior Lighting AS REQUIREDSeats and Belts SECURERear Canopy CLOSED AND LOCKEDDoor Warning Lights OFFParking Brake RELEASEBrakes TESTFlight Instruments CHECK ON TAXI
engine CHeCk
Align Aircraft Into WindParking Brake SETFuel Tank Selector FULLEST TANKMixture RICHThrottle 2000 RPMFuel Pressure 15-35 PSIMixture LEAN (all USU flights)
NOTE: Use Lean Assist Page to Set mixture 100°F rich of peak.
Engine Instruments GREENCircuit Breakers CHECK INProp CYCLE 3 TIMES 1. Decrease in RPM 2. Decrease in Oil Pressure
3. Increase in Manifold Pressure
Magnetos CHECK (175/50)Throttle IDLEThrottle SET 1000Alternate Air CHECK/CLOSEDLights AS REQ’DTransponder ALT
DA-4
0F C
HECK
LISTS
DA-4
0CS C
HECK
LISTS
ARRO
W CH
ECKL
ISTS
Rev. 03.19 25
DA-40F CHECKLISTSDA-40CS CHECKLISTS
ARROW CHECKLISTSDA-40CS NORMAL CHECKLIST
BeFore tAkeoFF
Canopy & Windows CLOSED & LATCHEDDeparture Briefing CLEARANCE (EMER PLAN)Circuit Breakers CHECK INMagnetos BOTHFlaps SET T/OProp FULL FORWARDAnnunciator Panel CHECKElevator Trim SET T/OParking Brake RELEASETraffic 360° CLEARFinal “FINAL IS CLEAR”Runway “RUNWAY IS CLEAR”Landing Light ON (cleared for T/O)Fuel Pump ONPitot Heat ONTransponder ON/ALT
tAkeoFF roll
Prop FULL FORWARDHSI “RWY HDG ### CONFIRMED”Power “POWER CHECK” (2680 ±20 RPM) ABORT T/O if more than ±20Airspeed “AIRSPEED ALIVE” VR “59 KTS. ROTATE”
Accelerate to climbout speed - 66 KIAS500 Feet Agl
Prop SET 2400 (MAX)Flaps VERIFY UPFuel Pump OFFLanding Light OFF
Accelerate to cruise climb speed - 73 KIAS
1000 Feet Agl
Engine Gauges CHECKTransponder VERIFY ALT MODE Taxi Light AS REQUIRED
level oFF CrUise
Throttle/Prop SET TO POWER TABLELanding Light VERIFY OFFFuel Pump VERIFY OFFCHT 150-400 F°Oil Temp 165-220 F°Mixture LEANTrim AS NEEDEDFuel Tank Selector FULLEST TANK
Turn Fuel Pump On Before SwitchingFuel differential MUST NOT exceed 10 gallons
between right & left tankreFerenCe speeDs
Vso (dirty stall speed) 49 ktsVs1 (clean stall speed) 52 ktsVr (rotation speed) 59 ktsVy (best rate of climb) 66 kts w/flaps T/O 73 kts w/flaps UPVref (normal approach speed) 71 ktsVref (short field approach speed) 66 ktsVglide (best glide speed) 73 ktsVfe (flap extend speed) T/O - 108 kts LDG - 90 ktsVa (maneuvering speed) 108 kts (2535 lbs)
94 kts (2161 lbs)
Rev. 03.1926
DA-40CS NORMAL CHECKLIST
MAneUvers
Clearing Turn COMPLETERadio ANNOUNCE INTENTIONSAltitude Bug SET Heading Bug SETEmergency Landing Site CHOSENAirspeed APPROPRIATEAircraft CONFIGURED
Fuel pump should remain OFF during maneu-vers unless determined necessary for safety of flight
CleAn Up CHeCklist
Power SET AS APPROPRIATEFuel Pump OFFFlaps UPLights AS REQUIREDFuel Selector FULLEST TANKMixture SET
DesCent/ApproACH CHeCklist
Circuit Breakers CHECK INExterior Lighting AS REQUIRED ATIS (weather) OBTAINAltimeter (3) SET _______Annunciator Panel CLEAREngine Gauges GREENFuel Quantity CHECKFuel Pump ONMixture ENRICHENFuel Selector FULLEST TANKSafety Harnesses FASTENED
FinAl CHeCk
APPROACHFuel Selector VERIFY FULLEST TANKFuel Pump VERIFY ONSeat Belts SECUREDAirspeed AT OR BELOW VFEFlaps T/OTrim AS NEEDEDLights AS REQUIRED
BEFORE LANDINGMixture SET AS APPROPRIATEProp FULL FORWARDThrottle 13” MPFlaps LDGAirspeed 66 – 71 KTS
NOTE: If LANDING IN STRONG WIND AND TURBULENCE USE A HIGHER APPROACH SPEED AND/OR USE LESS FLAPS.
go AroUnD CHeCk
Throttle FULL FORWARDAirspeed 66 KTSFlaps T/OGo Around ANNOUNCE
At 500’ AGL or Safe AltitudeProp 2400 RPM (MAX)Flaps UPFuel Pump OFFAirspeed 73 KTS
DA-4
0F C
HECK
LISTS
DA-4
0CS C
HECK
LISTS
ARRO
W CH
ECKL
ISTS
Rev. 03.19 27
DA-40F CHECKLISTSDA-40CS CHECKLISTS
ARROW CHECKLISTSDA-40CS NORMAL CHECKLIST
AFter lAnDing CHeCk
Runway Clear ANNOUNCEExterior Lighting AS REQUIREDTransponder VERIFY ALT MODEThrottle IDLEMixture LEAN FOR TAXIFuel Pump OFFPitot Heat OFFFlaps UPTaxi Brief ACCOMPLISH
engine sHUtDown
Throttle SET 1000Parking Brake SETAvionics Master OFF Essential Bus Switch OFFExterior Lighting AS REQUIREDMixture IDLE CUTOFF
After engine stops:Ignition Switch OFFKey REMOVE FROM IGNITIONHobbs & Tach Time RECORDMaster Switch BAT & ALT OFFExterior Lighting ALL OFFInstrument & Flood Lights OFFFLIGHT PLAN CLOSE
AirCrAFt seCUre
Tie-Downs SECUREDChocks INSTALLED (main ldg gear) Pitot Cover INSTALLED Gust Lock INSTALLEDStall Warning Cover INSTALLEDParking Brake RELEASED (if Chocks Installed)Personal Items, Trash, etc. REMOVEDRear Door CLOSED & LOCKEDWindows CLOSED & LATCHEDFront Canopy CLOSED & LOCKED
FUel pUMp sop
Fuel Pump 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 pres-sure indications. If this occurs, the electric fuel
pump may be turned ON and the flight can be continued as normal. If the low fuel pressure
message remains, refer to the LOW FUEL PRES-SURE emergency checklist.
Rev. 03.19
Blank Page
DA-4
0F C
HECK
LISTS
DA-4
0CS C
HECK
LISTS
ARRO
W CH
ECKL
ISTS
29Rev. 03.19
DA-40F CHECKLISTSDA-40CS CHECKLISTS
ARROW CHECKLISTSDA-40CS MANEUVER CHECKLIST
MAneUvers
Clearing Turn COMPLETERadio ANNOUNCE INTENTIONSAltitude Bug SET Heading Bug SETAirspeed APPROPRIATEAircraft CONFIGURED
Fuel pump should remain OFF during maneuvers unless determined necessary for safety of flight
groUnD reFerenCe MAneUvers
Winds IDENTIFYEmergency Landing Site SELECTEDAltitude 800’ AGLAirspeed 95 KIASPower ` 18” M.P.Flaps UpFuel Pump OnPitch +4°
Pivotal Altitude CalculationsThe 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 AGLManeuvers Checklist COMPLETE Airspeed 95 KIAS (±10 KIAS)Bank ROLLING THRU 30°Power INCREASE ~1-2” MPPitch +2.5-5° NOSE HIGH
Enter 360º TurnBank Angle 45°/50° (±5°)Elevator MAINTAIN BACK PRESS.Power INCREASE TO MAINTAIN AIRSPEEDRudder COORDINATEDRoll-out of Turn LEAD BY 1/2 BANKPower REDUCE
Repeat maneuver in opposite directionClean Up Checklist PERFORM
slow FligHt
Altitude AT LEAST 2,000 AGLManeuvers Checklist COMPLETEThrottle 12” M.P.Flaps APPROACH(<108 KTS) OR LANDING(<91KTS)Specified Airspeed OBTAINAirspeed 5-10 KNOTS ABOVE STALL WARNINGThrottle AS REQUIREDPitch FOR AIRSPEED(+10 KTS OR +5 KTS)Altitude HOLD ASSIGNED ALT (±100 FT/±50 FT)Heading ±10°
reCovery-Throttle FULLAltitude & Hdg MAINTAINFlaps T/O, then UP when >75 KIASClean Up Checklist PERFORM
Rev. 03.1930
DA-40CS MANEUVER CHECKLIST
power oFF stAll
Altitude AT LEAST 2,000 AGLManeuvers Checklist COMPLETEThrottle 12” MPFlaps APPROACH(<108 KTS) OR LANDING(<91 KTS)Altitude MAINTAIN ±100 FT
When speed reaches 70 KTS:Throttle IDLEPitch FOR 70 KTS (STABILIZED DESCENT)Within 100’ of assigned altitude transition to a nose
up attitude.Rudder MAINTAIN COORDINATIONStall Horn ANNOUNCE “Stall Warning”Stall Buffet ANNOUNCE “Stalling”
Promptly Initiate RecoveryPrivate 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 HIGHWings LEVELThrottle VERIFY FULL OPENFlaps T/O SETTING
When Airspeed increases above 60 KTS:Pitch 5-7°Airspeed 73 KIASClean Up Checklist PERFORM
power on stAll
Altitude AT LEAST 2,000 AGLManeuvers Checklist COMPLETEThrottle 12” MP
As speed decreases to 73 KIAS:ALT MAINTAIN ±100ftHDG ±10° UNLESS TURNING STALL (MAX 20° BANK)
When speed reaches 73 KTS:Throttle SMOOTHLY APPLY FULL OPENPitch SMOOTHLY 18° NOSE UP AND HOLDRudder MAINTAIN COORDINATIONStall Horn ANNOUNCE “Stall Warning”Stall Buffet ANNOUNCE “Stalling”
Promptly Initiate RecoveryPrivate 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 HIGHWings LEVELThrottle VERIFY FULL OPEN
When Airspeed increases above 60 KTS:Pitch 5-7° Airspeed 73 KIASClean Up Checklist PERFORM
DA-4
0F C
HECK
LISTS
DA-4
0CS C
HECK
LISTS
ARRO
W CH
ECKL
ISTS
Rev. 03.19 31
CHAnDelle
Altitude AT LEAST 2,000 AGLManeuvers Checklist COMPLETEVisual Reference Points SELECTAirspeed 95 KIAS
First 90° of Turn:Bank ROLL TO 30°Power FULLPitch SLOWLY INCREASERudder MAINTAIN COORDINATION 90° Point MAX PITCH UP (12-15°)
Last 90° of TurnBank SLOWLY REDUCEPitch MAINTAIN MAX PITCH UP (12-15°)Rudder MAINTAIN COORDINATION180° Point WINGS LEVELAirspeed JUST ABOVE A STALLHeading ±10°
Recovery:Airspeed INCREASE TO 95 KIASAltitude MAINTAIN AS AIRSPEED BUILDSHeading ±10°
Repeat maneuver in opposite directionClean Up Checklist PERFORM
lAzy eigHts
Altitude AT LEAST 2,000 AGLManeuvers Checklist COMPLETEVisual Reference Points SELECTPower 17-18” MPAirspeed 95 KIAS
Slowly begin increasing pitch and bank simultaneously.
At 45° Point:Pitch MAX PITCH UPBank APPROX. 15°
At 90° Point:Pitch LEVEL WITH HORIZONBank APPROX. 30°Airspeed MINIMUM AIRSPEED ABOVE A STALL
At 135° Point:Pitch MAX PITCH DOWNBank APPROX. 15°
At 180° Point:Pitch LEVEL WITH HORIZONBank WINGS LEVELAirspeed ±10 KTS FROM ENTRY SPEEDAltitude ±100 FT FROM ENTRY ALTHeading ±10°
Repeat maneuver in opposite directionClean Up Checklist PERFORM
DA-40F CHECKLISTSDA-40CS CHECKLISTS
ARROW CHECKLISTSDA-40CS MANEUVER CHECKLIST
Rev. 03.1932
steep spirAl
Altitude AT LEAST 4,000 AGLThis maneuver must be recovered by 1,500’ AGL
according to USU SOPs and Commercial ACS.Maneuvers Checklist COMPLETEWinds IDENTIFYGround Reference Point SELECTFuel Pump ON
When over selected point:Power IDLEAirspeed TRIMMED FOR BEST GLIDE
While performing maneuver:Airspeed BEST GLIDE ±10 KTSBank NOT TO EXCEED 60°Ground Track MAINTAIN AROUND POINTEngine 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
CleAn Up CHeCklist
Power SET AS APPROPRIATEFuel Pump OFFFlaps UPLights AS REQUIREDFuel Selector FULLEST TANKMixture SET
DA-40CS MANEUVER CHECKLISTDA
-40F
CHE
CKLIS
TSDA
-40C
S CHE
CKLIS
TSAR
ROW
CHEC
KLIST
S
Rev. 03.19 33
DA-40CS ABNORMAL CHECKLIST
roUgH engine
Engine Indications CHECK Fuel Pump ONIgnition BOTHAlternate Air OPENMixture SET FOR SMOOTH RUNNINGFuel Selector CHECKThrottle/Mixture TRY VARIOUS SETTINGSIf engine is still running roughly, Land ASAP- Prepare
for engine failure.engine FAilUre
Airspeed TRIMMED FOR BEST GLIDELanding Site SELECTIf propeller is windmilling ENGINE RESTART Windmilling PropellerIf propeller is stationary ENGINE RESTART Stationary PropellerIf restart is unsuccessful proceed with ENGINE SECURE
engine restArt winDMilling propeller
Airspeed 80 KIASFuel Selector FULLEST TANKIgnition BOTHMixture SET APPROPRIATEFuel Pump ONAlternate Air OPENIf engine does not start: Mixture FULL LEANMixture PUSH FORWARD UNTIL ENGINE STARTSIf engine will not start proceed with ENGINE SECURE & EVACUATE
engine restArt stAtionAry propeller
Airspeed 80 KIASElectrical Equipment ALL OFFAvionics Master Switch OFFMaster Switch BATTERY ONMixture SET APPROPRIATEFuel Selector CHECKFuel Pump ONAlternate Air OPENIgnition Switch STARTIf starter is inoperative: Expect at least 1000’ altitude lossIgnition Switch BOTHAirspeed INCREASE ABOVE 130 KIASMixture CHECKIf engine won’t start, go to ENGINE SECURE & EVACUATE
engine seCUre
Mayday ANNOUNCETransponder SQUAWK 7700Fuel Selector OFFSafety Harnesses TIGHTENIgnition Switch OFF
When certain field can be made:Flaps SET LANDINGMaster Switch OFFTouchdown slowest airspeed & commence EVACUATE
evACUAte
Aircraft STOPCanopy OPENAirplane EVACUATE IMMEDIATELY
Fire Suppressant USE AS NECESSARY
DA-40F CHECKLISTSDA-40CS CHECKLISTS
ARROW CHECKLISTS
Rev. 03.1934
DA-40CS ABNORMAL CHECKLIST
engine Fire in FligHt
Landing Site SELECTCabin Heat OFFFuel Selector OFFThrottle MAX POWERFuel Pump OFFMaster Switch ONEmergency Windows/Canopy OPEN AS REQUIRED
If fire persists:Emergency Descent INITIATEFlaps UPAirspeed INCREASE
WARNING: VNO = 129 KIAS, and VNE = 178 KIAS
Bank 30-45°Once fire is extinguished:
Bank WINGS LEVELPitch GENTLY BRING NOSE UPAirspeed ESTABLISH BEST GLIDE
Proceed with ENGINE SECURE and EVACUATE
eleCtriCAl Fire in FligHt
Emergency Switch ONMaster Switch OFFCabin Heat OFFLanding Site SELECTEmergency Windows OPEN AS REQUIREDFront Canopy UNLATCH AS REQUIREDFire Suppressant USE AS NECESSARY
Land as soon as possible
loss oF rpMFuel Pump ONFuel Selector CHECKFriction Lock ADJUST
RPM Lever HIGH RPM
eleCtriCAl Fire on tHe groUnD
Master Switch OFFThrottle IDLEMixture IDLE CUTOFF
When the engine has stopped:Ignition Switch OFFCanopy OPENAirplane EVACUATE IMMEDIATELYFire Suppressant USE AS NECESSARY
engine Fire DUring stArt
Fuel Selector OFFMixture LEANCabin Heat OFFBrakes HOLDThrottle FULLFuel Pump OFFMaster Switch OFFWhen the engine has stopped:Ignition Switch OFFCanopy OPENAirplane EVACUATE IMMEDIATELYFire Suppressant USE AS NECESSARYAircraft HAVE INSPECTED
Door open (on groUnD or in FligHt)Airspeed SLOW TO VA
Front Canopy CHECK LATCHEDRear Door (Don’t touch a door in flight!) CHECK LATCHEDIf rear door appears unlatched in flight, leave as is
and land ASAP at an appropriate airfield
DA-4
0F C
HECK
LISTS
DA-4
0CS C
HECK
LISTS
ARRO
W CH
ECKL
ISTS
Rev. 03.19 35
DA-40F CHECKLISTSDA-40CS CHECKLISTS
ARROW CHECKLISTSDA-40CS ABNORMAL CHECKLIST
sMoke AnD Fire DUring tAkeoFF
If takeoff can be abandoned:Throttle IDLECabin Heat OFFBrakes APPLYFuel Selector OFFAll Electrical Switches OFFIf takeoff cannot be abandoned:
After climbing to a location where an emergency landing may be executed:
Airspeed TRIMMED FOR BEST GLIDEFuel Selector OFFFuel Pump OFFCabin Heat OFFAll Electrical Switches OFFEmergency Windows OPEN AS REQ’DFront Canopy UNLATCH AS REQUIREDAfter Touchdown EVACUATE
Co ContAMinAtion
Cabin Heat OFFVentilation OPENEmergency Windows OPENForward Canopy UNLATCH
Land as soon as practical
low volts on groUnD
Throttle SET 1200 RPMMaster Switch LEAVE ONElectrical Equipment OFFAmmeter CHECKIf caution light does not extinguish and the ammeter
reads zero:Master Switch RECYCLE ALTERNATORIf caution light continues and ammeter reads zero:
Prepare to terminate flight
low volts in FligHt
Master Switch LEAVE ONElectrical Equipment OFF (IF NOT REQ’D)Ammeter CHECKMaster Switch RECYCLE ALTERNATORIf caution light does not extinguish and the ammeter
reads zero:
Proceed with ALTERNATOR FAILURE
AlternAtor FAilUre
Circuit Breakers CHECKIf no circuit breakers had popped:Ammeter CHECK
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 ONElectrical Load REDUCE TO MINIMUMVoltage CHECK REGULARLYElectrical System MONITORLand at nearest suitable airport within 30 minutes
If aircraft battery becomes depleted:Emergency Battery Switch UNGUARD and ON
stArter engAgeD
Throttle IDLEMixture IDLE CUTOFFIgnition Switch OFFMaster Switch OFF
Terminate flight unscheduled maintenance is necessary.
Rev. 03.1936
DeFeCtive MixtUre Control
Altitude MAINTAIN TO AIRPORTDescent TEST TO A HIGHER POWER SETTINGA lean mixture can lead to engine roughness and a
loss of powerHigH CylinDer HeAD teMperAtUre
Mixture ENRICHOil Pressure CHECK
If oil pressure is low proceed withLOW OIL PRESSURE:
If oil pressure is normal:Throttle REDUCEAirspeed INCREASE
HigH FUel Flow
Fuel Pump ONFuel Pressure CHECK
Low fuel pressure indicates a possible leak in the system
Fuel Quantity MONITORPower Setting CHECKLand as soon as practicable to avoid fuel exhaustion
low FUel pressUre
Fuel Pump ONFuel Quantity CHECKFuel Selector CHECKMixture ADJUST
Land as soon as practicable; prepare for engine failure
overvoltAge
Essential Bus ONMaster Switch ALTERNATOR OFFUnnecessary Electrical Equipment OFF
Land at nearest airfieldHigH oil teMperAtUre
Oil Pressure CHECKIf oil pressure is low proceed with
LOW OIL PRESSURECHT CHECKEGT CHECK
If oil pressure is normal:Mixture ENRICHThrottle REDUCEAirspeed INCREASE
Land as soon as practicable
low oil pressUre
Throttle REDUCE
Oil Temperature MONITORCHT MONITOR
Land as soon as practicable; prepare for engine failure
DA-40CS ABNORMAL CHECKLISTDA
-40F
CHE
CKLIS
TSDA
-40C
S CHE
CKLIS
TSAR
ROW
CHEC
KLIST
S
Rev. 03.19 37
FligHt into iCing
Icing Area LEAVE
Pitot Heat ON
Cabin Heat ON/DEFROSTRPM INCREASEAlternate Air OPENEmergency Windows OPEN IF REQUIRED
If Pitot Heat fails, the alternate static valve can be opened and emergency windows closed.
CAUTION: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:
Throttle IDLEAilerons NEUTRALRudder FULL DEFLECTION OPPOSITE OF SPINElevator FULLY FORWARDFlaps UP
When rotation has stopped:Rudder NEUTRALElevator PULL CAREFULLYDescent RECOVER INTO NORMAL FLIGHT
WARNING:Never allow the airplane’s speed to exceed VNE
BEST GLIDE SPEEDS
Aircraft weight (lbs)
2535 2205 1874
Flaps UP 73 68 60Flaps T/O 72 66 59Flaps LDG 71 63 58
AT ANY TIME THE PIC MAY REFERENCE THE AFM FOR ITEMS NOT INCLUDED ON THIS CHECKLIST.
DA-40CS ABNORMAL CHECKLISTDA-40F CHECKLISTS
DA-40CS CHECKLISTSARROW CHECKLISTS
Rev. 03.1938
Blank Page
Rev. 03.19 39
DA-42 PREFLIGHT CHECKLIST
DA42 FligHt DeCk
Weather, Flight Plan, Weight & Balance COMPLETEAircraft Documents & Inspections CURRENTFlight Control Lock REMOVEElectrical Equipment ALL OFF Circuit Breakers CHECK INGear Selector CHECKED DOWN Power Levers IDLE Electric Master ONFuel Quantity CHECK Flaps LANDINGLights & Pitot Heat CHECK OPERATIONStall Warning Horn CHECK OPERATIONG1000 Database CURRENTBattery Voltage CHECK (+24.1 Volts)Electric Master OFFFire Extinguisher CHARGED & SECURED Baggage STOWED
leFt MAin geAr
Left Gear Strut and Downlock INSPECT Wheel & Tire INSPECTSquat Switch INSPECTLimit Switches (2) INSPECT (don’t touch!)Brakes & Hydraulic Line INSPECTGear Doors and Linkage INSPECTChocks REMOVE
leFt engine nACelle
3 Air Inlets & 2 Air Outlets INSPECTGear Box Oil INSPECTSpinner and Propeller INSPECTEngine Oil Level CHECKFuel Drains (2) CHECK FUEL QUALITYCowling INSPECTExhaust INSPECT
leFt wing
Wing Leading Edge and Surfaces INSPECTStall Warning CHECK Tank Air Vent INSPECTFuel Caps INSPECT & CHECK FUEL QUANTITYPitot-Static Mast REMOVE COVER & INSPECTWing Tie-Down REMOVE Wing Tip and Lights INSPECTStatic Wicks (2) INSPECT
Aileron
Aileron Paddle INSPECTHinges & Safety pins INSPECTPush Rod, Bracket, & Bonding Straps INSPECTTrim Tab INSPECT (don’t touch!)
FlAp
Counter Weight INSPECTHinges & Safety Pins INSPECTPush Rod, Bonding Straps, and Linkage INSPECTTongue in Groove Assembly INSPECTFuel Cooler Air In & Outlet INSPECTMain Gear INSPECT FROM AFTStep INSPECT
leFt FUselAge
Rear Cabin Door & Window INSPECT Rear Door Pins INSPECTAntennas INSPECTFuselage Surface INSPECTTail Skid INSPECTTail Tie-Down REMOVE
DA-40F CHECKLISTSDA-40CS CHECKLISTS
DA-42 CHECKLISTS
Rev. 03.1940
DA-42 PREFLIGHT CHECKLIST
rUDDer
Static Wick (1) INSPECTTrim Tab INSPECT (don’t touch!) Cables and Eyelets INSPECTTop and Bottom Hinges INSPECT
elevAtor
Elevator CHECK FREEDOM OF MOVEMENTElevator Trim Tab INSPECTHinges INSPECTStatic Wicks (2) INSPECTLightening Discharge INSPECT
rigHt FUselAge
Fuselage Surface INSPECTRear Window INSPECTStep INSPECT
rigHt wing-FlAp
Main Gear INSPECT FROM AFTFuel Cooler Air In & Outlet INSPECTTongue in Groove Assembly INSPECTPush Rod, Bonding Straps, and Linkage INSPECTHinges & Safety Pins INSPECTCounter Weight INSPECT
Aileron
Hinges & Safety Pins INSPECTPush Rod, Bracket, & Bonding Straps INSPECTAileron Paddle INSPECT
rigHt wing
Static Wicks (2) INSPECTWing Tip and Lights INSPECTWing Tie-Down REMOVE Wing Leading Edge and Surfaces INSPECTFuel Caps INSPECT & CHECK FUEL QUANTITYTank Air Vent INSPECT
rigHt engine nACelle
3 Air Inlets & 2 Air Outlets INSPECT Gear Box Oil INSPECTSpinner and Propeller INSPECTEngine Oil Level CHECKFuel Drains (2) CHECK FUEL QUALITYCowling INSPECTExhaust INSPECTCabin Air Inlet INSPECT
rigHt MAin geAr
Right Gear Strut and Downlock INSPECT Wheel & Tire INSPECTStall heat inhibitor switch INSPECTLimit Switches (2) INSPECT (don’t touch!)Brakes & Hydraulic Line INSPECTGear Doors and Linkage INSPECTChocks REMOVE
nose geAr
Strut and Lock INSPECTLimit Switches (2) INSPECT (don’t touch!)Wheel & Tire INSPECTGear Door and Linkage INSPECT
nose seCtion
De-Ice Fluid (if installed) 3/4 FULLBaggage Doors CLOSED, LATCHED, & LOCKEDOAT Probe and Battery Drain INSPECT EPU Connection INSPECTLanding and Taxi Lights INSPECTFront Canopy INSPECT AND CLEAN
AT ANY TIME THE PIC MAY REFERENCE THE AFM FOR ITEMS NOT INCLUDED ON THIS CHECKLIST.
DA-4
0F C
HECK
LISTS
DA-4
0CS C
HECK
LISTS
DA-4
2 CHE
CKLIS
TS
Rev. 03.19 41
DA-40F CHECKLISTSDA-40CS CHECKLISTS
DA-42 CHECKLISTSDA-42 NORMAL CHECKLIST
BeFore engine stArt
Pilot Documents ONBOARDParking Brake SET Times & Inspections CHECKED Preflight Inspection COMPLETE Passenger Briefing COMPLETERear Door CLOSED & LATCHEDBaggage & Tow Bar SECURERudder Pedals ADJUSTEDSafety Harnesses FASTENED Quadrant Friction Lock ADJUSTEDAlternators ONECUs AUTOLights OFFEmergency Switch GUARDED ELT ARMEDCircuit Breakers CHECK INAlternate Air CLOSEDGear Selector DOWNManual Gear Extension Handle CHECKAvionics Master OFFElectric Master OFFEngine Master (Left & Right) OFFPitot Heat OFFAlternate Static CLOSEDPower Levers IDLEFuel Selectors ONTrim (2) SETFlight Controls FREE & CORRECTElectric Master ONAnnunciations NORMALFuel Computer SET & CHECKEDPFD/MFD BACK UP MODE
Tach Time CONFIRMGear Warning/Fire Detector TESTV-speeds SETVariable Elevator Backstop CHECKFlaps RETRACT
engine stArt
Normal order: Start Left Engine FirstFront Canopy POSITION 1 OR 2Fuel Temperature CHECKEDStrobes ONBrakes HOLD Propeller Area CLEAREngine Master ONAnnunciations / Engine Instruments CHECKGlow Indication OFFIgnition 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 OUTSIDE RED IN 3 SECRPM 900 +/- 20 CHECK Annunciations CHECK
Engine Instruments GREEN
AFter stArt
Warm Up Time START (Idle 2 Mins.)Pitot Heat ONVoltage & Load CHECK INDICATIONPitot Heat OFF
After 2 min warm up time, do not exceed 1400 RPM until Oil is > 50°C, and Coolant > 60°C
Rev. 03.1942
DA-42 NORMAL CHECKLIST
PFD/MFD NORMAL MODEAvionics Master ONFuel Selectors CROSSFEEDCircuit Breakers CHECKED
g1000 setUp
ATIS (weather) OBTAINAltimeters (3) SETClearance OBTAINTransponder CODE & ALTHeading Bug SET RWY HDGAltitude Bug SETFlight Plan ENTERRAIM CHECK AS NECESSARY Annunciations NORMAL
BeFore tAxi
Auto Pilot Test PERFORMStandby Instruments CHECK & SETTaxi Light ONInterior Lighting AS REQUIREDTaxi Brief ACCOMPLISHParking Brake RELEASEBrakes TESTFlight Instruments CHECK ON TAXI
engine CHeCk
Run-up Area CLEARParking Brake SETFuel Selectors ON Power Levers IDLEECU Test INITIATEECU Swap PERFORMEngine Gauges GREEN Parking Brake RELEASE
BeFore tAkeoFF
Canopy & Windows CLOSED & LATCHEDDeparture Briefing CLEARANCE (EMER PLAN)Single Engine Climb Performance CHECKAnnunciator Panel CHECKFlaps UPCircuit Breakers CHECKElevator Trim SET T/ORudder Trim AS REQUIREDTraffic 360° CLEAREngine Instruments GREENFinal “FINAL IS CLEAR”Runway “RUNWAY IS CLEAR”Landing Light ON (cleared for T/O)Pitot Heat ON
tAkeoFF roll
HSI “RWY HDG ### CONFIRMED”Brakes HOLDPower Levers FULL FORWARD% Load STABILIZED AT 90-100%Engine Gauges GREENBrakes RELEASEAirspeed “AIRSPEED ALIVE” VR “70-72 KTS. ROTATE”
After liftoff:Brakes TAPLanding Gear UP WITH POSITIVE RATE
500 Feet Agl
Power REDUCE TO 90%Flaps VERIFY UPLanding Gear VERIFY UP
DA-4
0F C
HECK
LISTS
DA-4
0CS C
HECK
LISTS
DA-4
2 CHE
CKLIS
TS
Rev. 03.19 43
DA-40F CHECKLISTSDA-40CS CHECKLISTS
DA-42 CHECKLISTSDA-42 NORMAL CHECKLIST
1000 Feet Agl
Engine Gauges CHECKTransponder VERIFY ALT MODE Landing and Taxi Lights AS REQUIRED
level oFF
Power REDUCE TO 70%Engine Gauges CHECKAnnunciator Panel CLEARExterior Lighting AS REQUIRED
MAneUvers
Clearing Turn COMPLETERadio ANNOUNCE INTENTIONSAltitude Bug SET Heading Bug SETAirspeed APPROPRIATEAircraft CONFIGURED
CleAn Up Flaps UPGear UPPower SET 60%Lights AS REQUIREDAlternate Air OFFAltitude Bug SET Heading Bug SETAirspeed APPROPRIATEAircraft CONFIGURED
DesCent/ApproACH
ATIS (weather) OBTAINAltimeters (3) SETSafety Harnesses FASTENED
Gear Warning Horn TESTGear Selector “DOWN 3 GREEN” (below 194)Engine Gauges GREENFuel Selectors ONParking Brake RELEASEDApproach Flaps AS REQUIREDLanding and Taxi Lights ON
FinAl CHeCks
Landing Gear “DOWN 3 GREEN”Flaps SETAirspeed ESTABLISHLanding and Taxi Lights ON
AFter lAnDing wHen CleAr oF rUnwAy
Runway Clear ANNOUNCEExterior Lighting AS REQUIREDTransponder VERIFY ALT MODE Flaps UPPitot Heat OFFTaxi Brief ACCOMPLISHCool Down Time START (Idle 2 Mins.)
engine sHUtDown
Parking Brake SETAvionics Master OFFExterior Lighting AS REQUIRED2 Min. Cool Down Time VERIFY
Engine Masters (Left & Right) OFFHobbs & Tach Time RECORD Electric Master OFFExterior Lighting ALL OFF Instrument & Flood Lights OFFFLIGHT PLAN CLOSE
Rev. 03.1944
DA-42 NORMAL CHECKLIST
AirCrAFt seCUre
Gust Lock INSTALLEDTie-downs SECUREDChocks INSTALLED (main ldg gear)Pitot Mast Cover INSTALLEDParking Brake RELEASED (if Chocks Installed)Personal Items, Trash, etc. REMOVEDRear Door CLOSED & LOCKEDWindows CLOSED & LATCHEDFront Canopy CLOSED & LOCKED
sopEmergency Airspeeds
Event AirspeedOne engine Inoperative VMCA 68 KIASOne engine Inoperative Best Rate VYSE 82 KIAS
OPERATING SPEEDS
Aircraft Weight Flaps Below
3748Above 3748
Climbout Speed (Vy)
UP 77 KIAS 79 KIAS
Cruise Climb Speed
(Flaps UP)UP 85 KIAS
MIN.
86 KIAS MIN.
Approach Speed
(Flaps UP)
APP LDG
82 KIAS76 KIAS
82 KIAS78 KIAS
Short Field Landing LDG 75 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
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.
DA-4
0F C
HECK
LISTS
DA-4
0CS C
HECK
LISTS
DA-4
2 CHE
CKLIS
TS
Rev. 03.19 45
DA-40F CHECKLISTSDA-40CS CHECKLISTS
DA-42 CHECKLISTSDA-42 MANEUVERS CHECKLIST
MAneUvers
Clearing Turn COMPLETERadio ANNOUNCE INTENTIONSAltitude Bug SET Heading Bug SETAirspeed APPROPRIATEAircraft CONFIGURED
steep tUrns
Altitude AT LEAST 3,000 AGL Maneuvers Checklist COMPLETEPower Levers 50% LOADAirspeed 105-110 KIAS
Enter 360° Turn:Bank Angle 50° (± 5°)Power Levers INCREASE 10%Elevator BACK PRESSURE TO MAINT. ALT.Rudder COORDINATEDRoll Out of Turn POWER AS NEEDED
Repeat maneuver in opposite direction.Clean Up Checklist PERFORM
slow FligHt (MiniMUM ControllABle AirspeeD)Altitude AT LEAST 3,000 AGLManeuvers Checklist COMPLETEPower Levers 50% LOADBefore Landing Checklist COMPLETE
Set Up:Specified Airspeed OBTAIN (+5/-0 KTS)Altitude MAINTAIN ENTRY ALT ±50 FTHeading MAINTAIN ±10°Rudder COORDINATED
RECOVERY:Power Levers FULL FORWARDAltitude MAINTAIN ±50 FTLDG Flaps RETRACTLanding Gear RETRACTAirspeed ACCELERATE TO VY (77 or 79 KIAS)APP Flaps RETRACT
Clean Up Checklist PERFORM
power-on stAll (DepArtUre stAlls)
Altitude AT LEAST 3,000 AGLManeuvers Checklist COMPLETEPower Levers 50% LOADFlaps and Gear VERIFY UPAirspeed 90-100 KTS
Perform Stall:Throttles 65-100% LOADPitch SLOWLY PITCHING UP(~20°)Rudder COORDINATEDDirectional Control MAINTAINStall Horn ANNOUNCE “Stall Warning”Stall Buffet ANNOUNCE “Stalling”
Promptly Initiate RecoveryCommercial Pilot ACS requires a recovery at the
first indication of a stall.
RECOVERY:
PITCH REDUCE TO +3° NOSE HIGHPOWER LEVERS FULL FORWARDGEAR AND FLAPS VERIFY UPRUDDER COORDINATEDAIRSPEED ACCELERATE TO BLUE LINE (82 KIAS)
Clean Up Checklist PERFORM
Rev. 03.1946
DA-42 MANEUVERS CHECKLIST
power-oFF stAlls
Altitude AT LEAST 3,000 AGLManeuvers Checklist COMPLETEPower Levers 30% LOADAltitude MAINTAIN ±100 FTBefore Landing Checklist COMPLETEFlaps and Gear AS REQUIREDAirspeed DECREASE TO 85 KIASDescent ESTABLISH AT 85 KIASStalling Altitude ANNOUNCE
When within 100’ of stalling altitude:Power Levers IDLEAltitude MAINTAIN WITH PITCHPitch HOLD UNTIL STALLDirectional Control MAINTAINStall Horn ANNOUNCE “Stall Warning”Stall Buffet ANNOUNCE “Stalling”
Promptly Initiate RecoveryCommercial Pilot ACS requires a recovery at the
first indication of a stall.PITCH REDUCE TO +3° NOSE UPPOWER LEVERS FULL FORWARDLDG FLAPS RETRACTGEAR RETRACT WITH POSITIVE TRENDRUDDER COORDINATEDAIRSPEED ACCELERATE TO Vy (77 or 79 KIAS)APP FLAPS RETRACTClean 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.
Altitude AT LEAST 4,000 AGLManeuvers Checklist COMPLETEPower Levers 25% LOADAltitude MAINTAINCritical Engine (Left) IDLE AT 100 KIASRight Engine Full AT 90 KIASSlow 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 IDLEPITCH REDUCEAIRSPEED ACCELERATE ABOVE REDLINERIGHT POWER LEVER SMOOTHLY ADVANCE TO FULLAIRSPEED BLUE LINE - 82 KIAS (±5 KTS)HEADING MAINTAIN ENTRY HDG ±20°MAINTAIN DIRECTIONAL CONTROL AND AIRSPEEDGear and Flaps 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.
DA-4
0F C
HECK
LISTS
DA-4
0CS C
HECK
LISTS
DA-4
2 CHE
CKLIS
TS
Rev. 03.19 47
DA-40F CHECKLISTSDA-40CS CHECKLISTS
DA-42 CHECKLISTSDA-42 MANEUVERS CHECKLIST
DrAg DeMo
Altitude AT LEAST 4,000 AGLManeuvers Checklist COMPLETEPower Levers 25% LOADCritical Engine (Left) IDLE AT 100 KIASRight Engine Full AT 90 KIASAirspeed MAINTAIN 82 KIASHeading ±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/Flaps Demonstration:
Gear Selector “DOWN 3 GREEN” (below 194)VSI NOTE Flaps (APP) SET (below 137)VSI NOTEFlaps (LDG) SET (below 111)VSI NOTE
RECOVERY:FLAPS APPGEAR UPFLAPS RETRACTCritical Engine (Left) Slowly Increase
NOTE: If the engine was feathered, AFTER 30 seconds ENGINE RESTART is only permissible at Pressure Altitude of 8000 FT. or Below
CleAn Up Flaps UPGear UPPower SET 60%Lights AS REQUIREDAlternate Air OFFAltitude Bug SET Heading Bug SETAirspeed APPROPRIATEAircraft CONFIGURED
Rev. 03.19
Blank Page
49Rev. 03.19
DA-40F CHECKLISTSDA-40CS CHECKLISTS
DA-42 CHECKLISTS
engine FAilUre in FligHt
Directional Control MAINTAINAirspeed AT OR ABOVE BLUE LINE (82 KNOTS)Power Levers FULL FORWARDFlaps & Gear RETRACTIdentify % LOAD DEAD FOOT DEAD ENGINE (YAW)Verify Dead Engine RETARD POWER LEVER SLOWLY
engine troUBlesHoot
NOTE: For training purposes SIMULATE ECU swap and Fuel Selectors OFF
Power IDLEAlternate Air PULL ONFuel Selector FAILED ENGINE TO CROSSFEEDMaster Switches (2) CHECK ONECU Swap FAILED ENGINE TO ECU “B”Circuit Breaker (ECU) CHECK / RESETIf engine doesn’t restart, proceed to ENGINE SECURE
engine seCUre
NOTE: For training purposes SIMULATE Alternator and Fuel Selectors OFF.
Master Switch (INOP Engine) IDENTIFY, VERIFY, OFFAlternator (Inoperative Engine) OFFFuel Selector (Inoperative Engine) OFFMayday ANNOUNCETransponder SQUAWK 7700
Land as soon as practical.
restArting A FeAtHereD engine
NOTE: AFTER 30 seconds ENGINE RESTART is only permissible at Pressure Altitude of 8000 FT. or Below
Airspeed 125 KIAS TO 145 KIASPower Lever (Inop. Engine) AT OR BELOW 25%Fuel Selectors ONAlternate Air AS REQUIREDAlternator ONEngine Master ON
If engine does not restart:Airspeed REDUCE BELOW 90 KIASStarter ENGAGECircuit Breakers CHECK
engine Fire in FligHt
Power Levers FULL FORWARDAirspeed AT OR ABOVE BLUE LINE (82 KNOTS)Flaps & Gear RETRACTFailed Engine IDENTIFY, VERIFYMaster Switch (INOP Engine) IDENTIFY, VERIFY, OFFAlternator (Inoperative Engine) OFFFuel Selector (Inoperative Engine) OFFCabin Heat & Defrost OFFCanopy UNLATCH (if necessary)
MAX airspeed 120 KIAS
engine Fire on groUnD
Power Levers (2) IDLE Engine Masters (2) OFFFuel Selectors (2) OFFMayday Call CONSIDERElectric Master OFFAircraft EVACUATE (once stopped)
DA-42 ABNORMAL CHECKLIST
Rev. 03.1950
eleCtriCAl Fire on groUnD
Mayday Call CONSIDERElectric Master OFFPower Levers (2) IDLE Engine Masters (2) OFFFuel Selectors (2) OFF
When engine and aircraft stopped:Canopy OPEN
EvacuateeleCtriCAl Fire in FligHt
Emergency Switch ONMayday Call CONSIDERAvionics Master OFFElectric Master OFF Cabin Heat & Defrost OFFEmergency Windows OPEN (as necessary)Canopy UNLATCH (if necessary)
MAX airspeed 120 KIASLand ASAP
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.
Flaps UPGear DOWNPower Levers IDLEAirspeed AS REQUIRED
WARNINGVno 155 KIASVne 194 KIAS
lAnDing geAr UnsAFe wArning
If on for more than 20 secondsAirspeed BELOW 156 KIAS
In cold temperatures, max airspeed is 110 KIASGear 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
Airspeed BELOW 156 KIASGear Indicator Lights TESTElectric Master CHECK ONBus Voltage CHECK NORMALGear Selector DOWNManual Extension Handle PULL
If necessaryAirspeed BELOW 110 KIAS
Apply moderate yawingGear Indicator Lights “DOWN 3 GREEN”
DA-42 ABNORMAL CHECKLISTDA
-40F
CHE
CKLIS
TSDA
-40C
S CHE
CKLIS
TSDA
-42 C
HECK
LISTS
Rev. 03.19 51
AlternAtor FAilUre
If one alternator failed:Failed Alternator OFFBus Voltage MONITORElectrical Equipment REDUCE AS PRACTICABLE
If both alternators failed:Avionics Master OFFLH/RH Alternator Switches OFFTransponder STANDBYLanding Gear DOWNEmergency Gear Extension PULLStall/Pitot Heat OFFAll Lights OFF
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 OFFVentilation OPENEmergency Windows OPENForward Canopy UNLATCH
Max speed 120 KIASLand as soon as practical
BotH eCU A & B FAilUre DUring FligHt
ECU Test Button HOLD FOR AT LEAST 2 SECIf message reappears or cannot be reset:
Flight LAND AT NEAREST SUITABLE AIRFIELDPrepare for possible engine failure.
Door open (on groUnD or in FligHt)Airspeed REDUCEFront Canopy CHECK LATCHEDRear Door (Don’t touch a door in flight!) CHECK LATCHEDNose Baggage Doors CHECK LATCHED
Canopy or rear door unlatched:Airspeed BELOW 140 KIASLeave the door as is and land ASAP at an appropri-
ate airfieldNose Baggage Doors Unlatched:
Airspeed REDUCE UNTIL DOOR IS STABLELand 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 TERMINATEAircraft Engine HAVE INSPECTED
If ECU failure is in flight:ECU Test Button HOLD FOR AT LEAST 2 SEC
If message resets:Flight CONTINUE
The engine must be serviced after landing.
If message reappears or cannot be reset:Flight LAND AT NEAREST SUITABLE AIRFIELDAircraft Engine HAVE INSPECTED
DA-40F CHECKLISTSDA-40CS CHECKLISTS
DA-42 CHECKLISTSDA-42 ABNORMAL CHECKLIST
Rev. 03.19
COLD WEATHER OPS
klgUelev: 4457CtAF: 122.80Asos: 135.275
kBMCelev: 4229CtAF: 123.05Awos: 135.075
U10 elev: 4728CtAF: 122.80