IFR Checklist GSOHO Diamond DA 40 D Flight

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IFR Checklist G-SOHO Diamond DA 40 D Flight Deck and Electrical Checks External Checks

IFR Checklist G-SOHO Diamond DA 40 D Flight Deck and Electrical Checks External Checks Port Wing and Fuselage, Tail Starboard Fuselage and Wing Front Section and Nose Gear Before Starting Engine Checks Engine Starting After Start Checks Taxi Checks Radio Checks Power Checks Pre-Takeoff Checks In-Flight Checklist 1 2 3 3 4 5 5 6 6 6 7

Flight Deck and Electrical System Checks 1. 2. 3. 4. 5. 6. 7. 8.

Flight Deck and Electrical System Checks 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. Electric Master OFF All electrical switches OFF Engine Master OFF ECU Swap AUTO Flap selector UP HIS / Remote Compass SLAVE Circuit breakers all IN Power lever check travel, set IDLE Emergency fuel valve NORMAL, locked, wired Trim check sense and set to T/O Controls full and free travel Rudder pedals no foreign objects, check travel Electric Master ON Fuel contents check, >15 USG use alt. means Panel and internal lights ON, check, then OFF Pitot heater ON External lights ON (Nav, Strobes/anti-c. , Ldg) External lights check (Nav, Strobes/anti-c. , Ldg. ) Pitot head check warm outside 18. 19. back on flight deck 20. 22. 23. 24. External lights OFF (Nav, Strobes/anti-c. , Ldg) Pitot heat OFF Electric Master OFF Fire extinguisher, first aid kit check date, full, stowed 1 – Flight Deck and Electrical Checks

Below Port Wing 1. 2. 3. 4. 5. 6. 7. Torch, fuel strainer Present

Below Port Wing 1. 2. 3. 4. 5. 6. 7. Torch, fuel strainer Present Step Secure Gascolator drain Antenna secure Air intake clear Wheel Check fairing, tire, creep mark Fuel sump drain Port Wing 1. 2. 3. 4. 5. 6. 7. 8. 9. Stall warning check Fuel cap check contents, secure Pitot/static probe holes clear Light covers secure Wing surfaces, leading edge check Wing tip secure, lights, 2 static wicks Aileron movement, hinges, ctl rod Fuel vent clear Wing flap counterweight, hinges, ctrl rod Port Fuselage, Tail section 1. 2. 3. 4. 5. 6. 7. Canopy and rear door secure Fuselage check Antennas (1 top, 4 bottom) secure Elevator movement, hinges, links, 2 wicks Rudder movement, hinges, links, 1 wick Rudder trim tab secure Tail skid metal shoe present, undamaged 2 – External Checks

Starborad Fuselage 1. 2. Fuselage right side check Rear window and canopy check Starboard

Starborad Fuselage 1. 2. Fuselage right side check Rear window and canopy check Starboard Wing 1. 2. 3. 4. 5. 6. Wing flap counterweight, hinges, ctrl rod Fuel vent clear Aileron movement, hinges, ctl rod Wing tip secure, lights, 2 static wicks Wing surfaces, leading edge check Fuel cap check contents, secure Below Starboard Wing 1. 2. 3. 4. 5. Step Secure Air intake clear Fuel cooler intake as required Wheel Check fairing, tire, creep mark Fuel sump drain Front Fuselage and Nose Gear 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. Exhaust secure Wheel check fairing, tire, creep mark Air inlets (3) clear Prop check edges, spinner secure Air inlets (2) clear Gearbox oil check level Engine oil check level Ground power cover closed Yet another air intake clear Whatever it is check 3 – External Checks (continued)

Before Starting Engine 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11.

Before Starting Engine 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. Rudder pedals adjusted and locked Parking brake set Passengers briefed Seatbelts all on and fastened Rear door closed and locked Canopy closed or “cooling gap” Compass serviceable, check deviation card Instruments glasses, static check Circuit breakers all set Alternate static cock closed Alternate air check movement, CLOSED Power lever set friction, IDLE Start-up request 13. 14. 15. 16. 17. 18. 19. 20. 21. 22. 23. 24. Electric Master ON Engine instruments check Annunciator panel check, press ACK button Flight instruments erecting/flags, cage AI if required HSI / compass aligned Clock time check Avionics Master ON Intercom check Transponder Standby GPS check database COMM 2 - ATIS/ATC obtain airfield data Outside air temperature cross-check / plausible Altimeters, Autopilot QNH – elevation check (60 ft) COMM 2 - ready to start advise ATC Avionics Master OFF 4 – Before Starting Engine Checks

Engine Starting 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12.

Engine Starting 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. Area clear check clear prop Engine instruments check Fuel temperature (if Diesel) not flashing / above – 5 deg C Water Level caution light check OFF Strobe lights ON Power lever check IDLE ECU Swap AUTO Engine Master ON Glow Light wait until OFF Avionics Master check OFF Electric Master START Oil Pressure rising within 3 seconds Strobe lights OFF After Start Checks, Warm-Up 1. 2. 3. 4. 5. 6. 7. 8. Cabin heater/defrost as required Avionics Master ON Stop watch (ADF timer) start HSI, compass aligned ADF set for taxi checks Position lights ON (sunset-sunrise) Flaps Check all positions, indicators GPS ENT, check needles, no flags, ENT Now is a good time to set up the route in the GPS 5 – Engine Starting and After Start Checks

Before Taxi Checks 1. 2. 3. 4. 5. 6. 7. 8. Engine Warm-up 2

Before Taxi Checks 1. 2. 3. 4. 5. 6. 7. 8. Engine Warm-up 2 minutes since start Idle RPM 890 RPM +-20 Engine temperature check COMM 1 switch radios ATIS obtain latest Altimeters QNH – elevation check (60 ft) Autopilot set QNH COMM 1 Request Taxi to run-up area Taxi Checks 1. 2. 2. 3. Max 1400 rpm until oil and coolant in green range Brakes check P 1 and P 2 Turn-Ball-AI indications HSI-ADF-Compass indications Radio Checks 1. ADF function checks 2. NAV 1 GPS, VOR, ILS function checks 3. NAV 2 GPS, VOR, ILS function checks 4. 5. 6. DME function checks, transfer check Marker beacon receiver press to test Transponder check pressure altitude 6 – Taxi and Radio Checks

Power Checks 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12.

Power Checks 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. Parking brake check ON Front canopy closed and locked Door warning light OFF Engine Indications acceptable Fuel temperature (if Diesel) in green range / min +5 deg C Throttle friction adjusted as required Power Lever MAX Oil pressure check in green range RPM 2240 -2300 Power indicator 90 -100% Alternate air effective, then OFF Power lever IDLE, 890 RPM +-20 ECU Test - ECU A, ECU B, CAUTION - ECU BACKUP UNSAFE - ECU B checks - ECU A, ECU B, CAUTION - ECU BACKUP UNSAFE press and hold blinking light blinking, prop cycling OFF blinking 14. 15. ECU TEST RELEASE ECU SWAP ECU B, check engine, AUTOMATIC 7 – Power Checks

Pre-Takeoff Checks 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12.

Pre-Takeoff Checks 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. Charts: SID, re-land, en-route available A. T. I. S. check latest Altimeters aerodrome QNH Autopilot aerodrome QNH ATC clearances obtain Transponder set code Departure briefing satisfied Nav aids – GPS - comms set Canopy final check, front and aft Cabin heat/defrost as required Auto pilot OFF Trimmers check electric trim, set for take-off Flaps set T/O Controls full and free Engine instruments normal Fuel contents sufficient Crew take-off brief completed Ready for Departure report 8 – Pre-Takeoff Checks

1. A HSI-compass Aligned, RWY heading 2. T Transponder ALT 3. P Pitot heat

1. A HSI-compass Aligned, RWY heading 2. T Transponder ALT 3. P Pitot heat ON 4. L Landing light, Strobes ON 5. 6. 7. 8. Throttle full power 10 sec Engine Instruments check RPM, Power, Ts & Ps Brakes release Airspeed rising Takeoff 1

1. 2. 3. 4. 5. 8. 9. Airspeed 59 -73 kts Flaps retract Navigation

1. 2. 3. 4. 5. 8. 9. Airspeed 59 -73 kts Flaps retract Navigation aids Identify - bearings Airframe/engine icing check Altimeter No. 1 (pilot’s) QNH or 1013. 2 as required No. 2. aerodrome QNH 1000 ft - Landing light OFF SID/SAFETY/MSA altitudes achieved After Take-off And Climb Checks 2

Cruise Performance 2 b

Cruise Performance 2 b

1. F Fuel quantity HOWGOESIT, balance tanks 2. R En-route navigation aids set &

1. F Fuel quantity HOWGOESIT, balance tanks 2. R En-route navigation aids set & identified 3. I Airframe/engine icing check 4. E Temperature & pressures check 5. D HSI slaving - compass check 6. A Volmet/ATIS/QNH obtain QNH 7. Altimeter No. 1 (pilot’s) check set as reqd Altimeter No. 2 update QNH Minimum safe altitudes check Descent anticipated descent checks Cruise Checks 3

1. Minimum safe altitude checked 2. ATIS or latest weather obtained / recorded 3.

1. Minimum safe altitude checked 2. ATIS or latest weather obtained / recorded 3. Aerodrome minima check / recorded 4. 5. 8. STARS & approach charts crew briefing Throttle reduce Altimeter No. 2 set aerodrome QNH Pilot’s 1013. 2 or QNH Airframe/engine icing check Fuel sufficient 8. 9. Descent Checks 4

1. Approach procedure crew briefing 2. Approach/go-around aids set & identified 3. Crew/passengers all

1. Approach procedure crew briefing 2. Approach/go-around aids set & identified 3. Crew/passengers all secure 4. 7. 8. Landing light ON HSI slaving - RMI - compass checked Altimeter No. 2. check aerodrome QNH Pilot’s 1013. 2 or QNH 9. Airframe/engine icing check / operate if reqd 10. Temperatures & pressures check Approach Checks 5

2. Alternate air ON if wing ice 3. Altimeters aerodrome QNH, x-check 4. HSI

2. Alternate air ON if wing ice 3. Altimeters aerodrome QNH, x-check 4. HSI slaving - RMI - compass check 6. Decision altitude checked - recorded 5. Power/Airspeed Reduce to 95 kt 6. 1 NM / quarter scale below 108 - flaps T/O 6. FAP check altitude 8. DME or OM or beacon altimeter check 12. “Reds, Blues & Greens” for landing Pre-Landing Checks 6

1. Power Prop fine, MP 36” 100% 2. 3. Flaps rate of climb Positive

1. Power Prop fine, MP 36” 100% 2. 3. Flaps rate of climb Positive retract identified 3. 4. Positive rate of climb Flaps identified retract 4. 5. Undercarriage below 110 kt A. T. C. UP report going around 5. ! Navigation 7. Adequate altitude aids gain set 32" -2500 identify bearings rpm 6. 8. A. T. C. & engine Icing Airframe report /going check operate around if reqd 7. 9. Navigation aids SID/safety altitude identify - bearings achieved 8. 10. Airframe &No. Altimeter engine 1 (Pilot’s) Icing checkor/ 1013. 2 QNH operateasif reqd 9. SID/safety altitude No. 2 achieved QNH aerodrome 10. ! Landing 11. Altimeter. Light No. 1 (Pilot’s) QNH or 1013. 2 as reqd OFF 13. Minimum Sector Altitude No. 2 aerodrome QNH achieved 11. ! Pressures 14. Electric fuel & pump Temps>1000' OFF check 12. 15. Landing Light Prepare for Airfield Approach Checks OFF 13. Minimum Sector Altitude achieved 14. Pressures & Temps check 15. Prepare for Airfield Approach Checks Go-Around Checks 7

1. 2. 3. 4. Flaps retract Landing light OFF Pitot heat OFF Transponder set

1. 2. 3. 4. Flaps retract Landing light OFF Pitot heat OFF Transponder set to standby 7. On stand 8. 9. 10. - Radio Master OFF - GPS OFF - Magnetos live & dead check - Mixture control I. C. O. - Magneto switch OFF - Beacon leave ON - Electric fuel pump OFF - Master Switch OFF - Headsets OFF Times record Gust lock, aircraft secure as required Technical Log complete - sign After Landing Checks 8

In-Flight Engine Fire 1. 2. 3. 4. 5. 6. 7. 8. Mixture I. C.

In-Flight Engine Fire 1. 2. 3. 4. 5. 6. 7. 8. Mixture I. C. O. Fuel selector off Fuel pump off Magnetos off Throttle fully open Cabin heat / defroster closed Prop stop if possible Emergency descent full flap, 112 kts If fire stops: 9. 10. 11. Flaps retract Undercarriage override ENGAGE Airspeed 80 kts 12. 13. Select landing area Continue with Power Off Landing checklist If fire persists: 14. 15. 16. 17. 18. 19. Select landing area 20. Transponder 7700 ATC Mayday call Passengers Brief Seatbelts tight Undercarriage UP for water, rough terrain otherwise DOWN , 3 greens Master switch OFF Emergency – Engine Fire 9

In-Flight Engine Failure 1. If after power reduction Lean until engine restarts Maintain EGT

In-Flight Engine Failure 1. If after power reduction Lean until engine restarts Maintain EGT 1350 or above 2. 3. 4. Undercarriage override ENGAGE Airspeed Convert into maintaining altitude Best glide airspeed 80 kts 5. Select landing area Attempt restart (unless after fire or catastrophic failure): 6. 7. 8. 9. 10. 11. 12. 13. Electric fuel pump ON Fuel selector select tank with fuel / switch Magnetos check BOTH Throttle cruise setting Mixture rich Alternate air OPEN Magnetos check each magneto Engine indications check fuel flow, MP, etc. If unsuccessful, continue next page (Power Off Landing checklist) Emergency – Engine Failure 10

Power Off Approach and Landing 1. 2. 3. 4. 5. Best glide airspeed 80

Power Off Approach and Landing 1. 2. 3. 4. 5. Best glide airspeed 80 kts Prop lowest RPM (fully back) Transponder 7700 ATC Mayday call Passengers Seat backs Seat belts Glasses / false teeth Brace 6. 7. 8. 9. 10. 11. 12. Seatbelts tight Electric fuel pump OFF Fuel selector OFF Magnetos OFF Throttle CLOSED Mixture I. C. O. Undercarriage UP for water, rough terrain otherwise DOWN , 3 greens 13. 14. Flaps set Master switch OFF Emergency – Power Off Landing 11

Electrical Fire 1. 2. 3. 4. 5. 6. 7. 8. 9. Master switch Cabin

Electrical Fire 1. 2. 3. 4. 5. 6. 7. 8. 9. Master switch Cabin wall vents Cabin heat, defrost Electrical services Circuit breakers Master switch One VHF radio ATC Smoke / Fire ceases 10. Land as soon as practical OFF OPEN CLOSED all OFF check ON, check no smoke ON advise intentions restore essential services one by one Alternator Failure 1. 2. 3. 4. 5. 6. 7. Ammeter, ALT FAIL light cross-check ALT switch OFF Electrical load Reduce to minimum ALT circuit breaker check / reset if required ALT switch ON Ammeter, ALT FAIL light check If power not restored, advise ATC and land as soon as practical Persistent Alternator Overload (> 5 minutes) 1. 2. 3. 4. 5. 6. ALT switch BAT switch Ammeter If load not reduced: BAT switch ALT switch Electrical load Land as soon as practical ON OFF Check load reduced ON OFF Reduce to minimum Emergency – Electrical 12

High Oil Temperature 1. 2. Oil Pressure check Land at nearest airport. Prepare for

High Oil Temperature 1. 2. Oil Pressure check Land at nearest airport. Prepare for possible engine failure Low Oil Pressure 1. 2. 3. Oil Temperature check Land at nearest airport. Prepare for possible engine failure If complete loss of oil suspected, consider off-airport landing Turbocharger Failure 1. 2. 3. 4. 5. 6. Manifold pressure Throttle Propeller control Mixture Exhaust Land as soon as practical check full fine / full forward adjust as required check for smoke (oil leak) Prop Overspeed 1. 2. 3. 4. 5. Throttle Airspeed Oil pressure Propeller control Land as soon as practical retard – max 2700 RPM reduce if required check full decrease, check for control Manual Gear Extension 1. 2. 3. 4. 5. 6. 7. 8. Master switch Circuit breakers Radio lights Gear indicator bulbs Airspeed Undercarriage selector Emergency gear lever Fishtail aeroplane check ON CHECK check OFF (in daytime) / adjust CHECK below 92 kts DOWN EMERGENCY DOWN Emergency – Engine, Gear

Mass and Balance Schedule as of 31/03/2004 Mass and Balance Envelope 80 85 90

Mass and Balance Schedule as of 31/03/2004 Mass and Balance Envelope 80 85 90 95 91. 4 3600 3400 82. 75 3200 3000 2800 2600 2400 Empty 78 9 – Mass and Balance 80 85 90 95

Electrical System Schematics Hot Battery Bus Main Bus Essential Avionics Bus 1 – Flight

Electrical System Schematics Hot Battery Bus Main Bus Essential Avionics Bus 1 – Flight Deck and Electrical Checks