Diamond DA40 TDI OH-STL - MIK
Diamond DA40 TDI OH-STL NORMAL, EMERGENCY AND ABNORMAL CHECKLISTS 20.6.2013 Malmin Ilmailukerho ry Edition #1 Does not replace the Airplane Flight Manual
DA40 DA40 TDI TDI G1000 G1000 PREFLIGHT PREFLIGHT INTERIOR DA40 TDI G1000INTERIOR PREFLIGHT PREFLIGHT PROCEDURES PROCEDURES Left Left fuselage fuselage PREFLIGHT PROCEDURES Canopy Canopy left left side side EXTERIOR. EXTERIOR. Rear Rear door door Left fuselage 1 1Check Check Aircraft Aircraft papers papers PREFLIGHT INTERIOR Fuselage Fuselage leftleft side side Canopy left side 2 2 Remove Remove pitot pitot cover cover EXTERIOR. Antennas Antennas Rear door 3 3Check Check interior interior forfor foreign foreign 1 Check Aircraft papers Tail Tail Fuselage left side objects objects 2 Remove pitot cover Elevator Elevator & & rudder (freedom (freedom of of Antennas rudder 4 4Check Check flight flight controls controls free free 3 Check interior for foreign movement, movement, hinges) hinges) 5 5Check Check circuit circuit breakers breakers Tail objects Trim Trim - tab - tab 6 6Emergency Emergency Fuel Fuel Valve Valve Elevator & rudder (freedom of 4 Check flight controls free Tail Tail skid skid lower lower finfin NORMAL NORMAL movement, hinges) 5 Check circuit breakers Static Static dischargers dischargers 7 7Engine Engine Master Master OFF OFF Trim - tab 6 Emergency Fuel Valve 8 8ECU ECU SWAP SWAP AUTO AUTO Right Right fuselage fuselage Tail skid lower fin NORMAL 9 9Essential Essential bus bus OFF OFF Fuselage Fuselage right right side side Static dischargers 7 Engine Master OFF 1010Avionic Avionic Master Master electrics electrics OFF OFF Rear Rear window window 8 ECU SWAP AUTO Right fuselage 1111Electric Electric Master Master ONON Canopy Canopy right right side side 9 Essential bus OFF Fuselage right side Check Check battery battery voltage voltage 10 Avionic Master electrics OFF Right wing wing Rear Right window 1212Check Check fuel fuel quantity quantity temp temp 11 Electric Master ON Wing Wing flap flap side Canopy right 1313External External lights lights ONON Check battery voltage Aileron Aileron (freedom (freedom of of movement, movement, 1414Pitot Pitot heat heat ONON Right wing 12 Check fuel quantity temp hinges, hinges, control control linkage, linkage, 1515Check Check stall stall warning warning Wing flap 13 External lights ON security) security) 1616Check Check pitot pitot heat heat Aileron (freedom of movement, 14 Pitot heat ON Static Static dischargers dischargers 1717Check Check external external lights lights hinges, control linkage, 15 Check stall warning Wing Wing tip,tip, position position light light 1818Pitot Pitot heat heat / ext. / ext. lights lights OFF OFF security) 16 Check pitot heat Wing Wing leading leading edge, edge, toptopand and 1919Electric Electric Master Master OFF, OFF, Static dischargers 17 Check external lights bottom bottom surface, surface, stall stall strips strips key key removed removed Wing tip, position light 18 Pitot heat / ext. lights OFF Fuel Fuel filler filler cap cap Wing leading edge, top- and 19PREFLIGHT Electric Master OFF, PREFLIGHT EXTERIOR EXTERIOR Fuel Fuel vent vent bottom surface, stall strips key removed Drain Drain fuel fuel sump sump Left Left main main gear gear Fuel filler cap Fuel cooling baffle Wheel Wheel fairing fairingEXTERIOR PREFLIGHT Right Right main main gear gear Fuel vent ground temp 20 C installed Tire Tire condition, condition, pressure pressure (2,5 (2,5 bar), bar), Wheel Wheel fairing fairing Drain fuel sump Left main gear ground temp 20 C removed position position mark mark Tire Tire condition, condition, pressure pressure (2,5 (2,5 bar), bar), Wheel fairing Right main gear Brake, Brake, hydraulic hydraulic line line position position mark mark Tire condition, pressure (2,5 bar), Wheel fairing Brake, Brake, hydraulic hydraulic line line Left Left wing wing position mark Tire condition, pressure (2,5 bar), Wing Wing leading leading edge, edge, topand and Brake, hydraulic linetopNose Nose section section position mark bottom bottom surface, surface, stall stall strips strips OAT OAT sensor sensor line Brake, hydraulic Left wing Drain Drain fuel fuel sump sump Propeller Propeller surface surface Wing leading edge, top- and Nose section Stall Stall warning warning Spinner Spinner bottom surface, stall strips OAT sensor Fuel Fuel vent vent Cowling, Cowling, AirAir inlets inlets (5)(5) Drain fuel sump Propeller surface Fuel Fuel filler filler cap cap Stall warning Nose Nose gear gear Spinner Pitot, Pitot, static static probe probe (cover (cover Fuel vent Wheel Wheel fairing fairing Cowling, Air inlets (5) removed) removed) Fuel filler cap Tire Tire condition, condition, pressure pressure (2,0 (2,0 bar), bar), Landing/Taxi Landing/Taxi light light Nose gear Pitot, static probe (cover position position mark mark Wing Wing tip,tip, position position light light Wheel fairing removed) Static Static dischargers dischargers Engine Engine bay bay Tire condition, pressure (2,0 bar), Landing/Taxi light Aileron Aileron (freedom (freedom of of movement, movement, Engine Engine oil oil level level (4,5 (4,5 – 6,0 – 6,0 l) l) position mark Wing tip, position light hinges, hinges, control control linkage, linkage, Gearbox Gearbox oil oil level level Static dischargers Engine bay security) security) Drain Drain fuel fuel strainer strainer Aileron (freedom of movement, Engine oil level (4,5 – 6,0 l) Wing Wing flap flap hinges, control linkage, Gearbox oil level 01.12.2012 01.12.2012 Diamond Diamond Aircraft Aircraft Flight Flight Training Training Division Division Page Page 2 2 security) Drain fuel strainer 20.6.2013 Malmin Ilmailukerho ry Edition Edition # 16 # 16 Does Does not not replace replace the the Airplane Airplane Flight Flight Manual Manual Wing#1 flap Edition Does not replace the Airplane Flight Manual 01.12.2012 Diamond Aircraft Flight Training Division Page 2
DA40 TDI G1000 NORMAL PROCEDURES CHECK BEFORE ENGINE START 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 Preflight check .COMPLETED Baggage and tow bar . SECURED Emergency fuel valve .NORMAL Power lever. IDLE Parking brake. SET Alternate Air . CLOSED (start key) Electric master . OFF Avionic master . OFF Essential bus. OFF Alternate static. CLOSED Engine master . OFF ECU swap .AUTO All light switches. OFF Emergency switch. OFF / GUARDED ELT .ARMED Circuit breakers . CHECKED IN Flap selector . UP Pitot heat . OFF Fuel transfer . OFF 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 (start key) Electric Master. ON (check avionic fan noise) Rudder pedals . ADJUSTED Passengers . INSTRUCTED Seat belts . FASTENED Rear door . CLOSED and LATCHED Front canopy.POS 1 or 2 G1000.POWERED, ACKNOWLEDGED MFD . ENGINE – FUEL Fuel Quantity .CHECKED, RESET/SET if requ. Fuel temperature . CHECKED Total time in service.NOTED MFD . ENGINE-SYSTEM, ENGINE-DEFAULT Power lever. IDLE STROBE. ON 20 21 22 23 24 25 26 27 28 29 30 31 32 33 End of Checklist 01.12.2012 Diamond Aircraft Flight Training Division Page 3 20.6.2013 Ilmailukerho ry Edition # 1Malmin 6 D o es not re pla c e the Ai r pl ane Fl i ght Ma nua l Edition #1 Does not replace the Airplane Flight Manual
DA40 TDI G1000 NORMAL PROCEDURES ENGINE START PROCEDURE Engine Master . ON Annunciations / Eng.Instr. . CHECKED Glow indication . OFF Propeller area . CLEAR Start key. START Oil pressure . OUTSIDE RED within 3 sec Voltage, Electrical load . CHECK INDICATION Annunciations / Eng.Instr. .CHECK CHECK AFTER ENGINE START 1 2 3 Oil pressure . CHECKED RPM 890 /- 20. CHECKED Warm up time . START 1 2 3 4 5 6 Pitot heat .ON, annunciation Amps checked Pitot heat . OFF Avionics master . ON 4 5 6 Warm up: Idle . 2 minutes 1400RPM . until Oil 50 C and Coolant 60 C FMS SETUP I nitialize profile (AUX 4, MAP, MFD FPL, PFD FPL) F light plan R adios (COM, NAV, ADF, DME, CDI, BRG 1/2) P erformance (speed bugs) 7 FMS setup .COMPLETED 7 AUTOPILOT TEST DISCONN press, check electric trim not working AP ON, check overpowering servos DISCONN press, check AP off 8 9 10 11 12 13 14 15 Autopilot test .COMPLETED Flood light . CHECKED, ON as required Position lights.ON as required Flaps. full travel CHECKED, then T/O Altimeters (3) . SET Standby horizon . CHECKED Transponder .CODE/MODE CHECKED Parking brake. RELEASED End of Checklist; see next page for “During taxi” – items 8 9 10 11 12 13 14 15 01.12.2012 Diamond Aircraft Flight Training Division Page 4 20.6.2013 Malmin Ilmailukerho ry Edition # 16 Does not replace the Airplane Flight Manual Edition #1 Does not replace the Airplane Flight Manual
DA40 TDI G1000 NORMAL PROCEDURES DURING TAXI DA40 TDI G1000 Check brakes Check flight instruments NORMAL PROCEDURES BEFORE TAKE OFF CHECK DURING TAXI 1 2 3 4 5 1 6 2 7 3 8 4 9 5 10 6 11 7 12 8 13 9 10 11 12 13 14 15 16 17 18 14 15 16 17 18 Check brakes Parking brake. SET Check flight instruments Seat belts . FASTENED Rear door . CLOSED LATCHED BEFORE TAKE OFF CHECK Front canopy. CLOSED LATCHED Door warning light . OFF Parking brake. SET Engine instruments . CHECKED Seat belts . FASTENED Fuel (Diesel min 5 ) . Rear Temperature door . CLOSED CHECKED LATCHED Circuit breakers . CHECKED Front canopy. CLOSED LATCHED Electric elevator trim . CHECKED, T/O OFF SET Door warning light . Flaps. CHECKED T/O Engine instruments . CHECKED Flight controls . Fuel Temperature (Diesel min 5 ) . CHECKED CHECKED Power lever. IDLE Circuit breakers . CHECKED ECU testelevator . Electric trim . CHECKED,PERFORM T/O SET ECU TEST Flaps. CHECKED T/O ECU test button. and hold Flight controls .press CHECKED ECU backup unsafe light . flashing Power lever. IDLE ECU A, B, Caution lights . flashing ECU B, Caution lights .flashing /PERFORM prop cycling ECU test . ECU A, Caution lights .flashing / prop cycling ECU TESTlights .extinguished All ECU caution ECU test button. press and hold ECU backup unsafe light .extinguished ECU unsafe light . flashing ECU backup test button. release ECU A, B, Caution lights . flashing MAX POWER TEST ECU B, Caution lights .flashing / prop cycling LEVER. MAX FOR 10 SECONDS ECU swap POWER . ECU B, ENGINE CHECKED ECU A, Caution lights .flashing / prop cycling PRESSURE. CHECK GREEN AUTO RANGE ECU swap OIL . All ECU caution lights .extinguished RPM. STABILIZES AT 2240-2300 RPM ECU backup unsafe light .extinguished Pitot heat LOAD. . AS REQUIRED . STABILIZES AT 90-100% ECU test button. release POWER LEVER.IDLE Transponder .CODE/MODE CHECKED 1 2 3 4 5 1 6 2 7 3 8 4 9 5 10 6 11 7 12 8 13 9 10 11 12 13 14 15 16 17 Parking brake. ECU swap . ECU B, ENGINERELEASED CHECKED 18 14 End of Checklist ECU swap . AUTO 15 For procedural items and take-off profile next page 16 Pitot heat . ASsee REQUIRED Transponder .CODE/MODE CHECKED 17 Parking brake. RELEASED 18 End of Checklist 01.12.2012 Diamond Aircraft Flight Training Division Page 5 20.6.2013 Malmin Ilmailukerho ry Edition # 16 Does not replace the Airplane Flight Manual page Edition #1 For procedural items and take-off Does notprofile replacesee the next Airplane Flight Manual
DA40 TDI G1000 NORMAL PROCEDURES LINE UP PROCEDURE DA40 TDI G1000 Landing light. ON Approach sector . CLEAR Runway.IDENTIFIED Power lever max (100% / 10 sec) . . CHECK LOAD / RPM /NORMAL FUEL FLOW /OP PROCEDURES LINE UP PROCEDURE Landing light. ON Approach sector . CLEAR Runway.IDENTIFIED Power lever max (100% / 10 sec) . . CHECK LOAD / RPM / FUEL FLOW /OP Rotate at 59 kt AFTER TAKE-OFF PROCEDURE After passing safe altitude: Flaps .UP Landing light. OFF Rotate at 59 kt AFTER TAKE-OFF PROCEDURE After passing safe altitude: Flaps .UP Landing light. OFF 01.12.2012 Diamond Aircraft Flight Training Division Page 6 20.6.2013 Malmin Ilmailukerho ry Edition # 16 Does not replace the Airplane Flight Manual Edition #1 Does not replace the Airplane Flight Manual
DA40 TDI G1000 NORMAL PROCEDURES CLIMB TO CRUISE CHECK 1 2 Flaps. CHECKED UP Landing light . CHECKED OFF End of Checklist 1 2 PERIODICALLY DURING CRUISE Fuel Radio Engine Direction Altitude Fuel transfer . repeat as required Maximum fuel unbalance - Long range tank: 9 USG DESCENT / APPROACH CHECK 1 2 3 4 5 Landing data . RECEIVED Altimeters (3) . SET COM / NAV / FMS . SET Seatbelts . FASTENED Fuel transfer . AS REQUIRED End of Checklist 1 2 3 4 5 BEFORE LANDING PROCEDURE Downwind, latest base leg: Flaps . T/O Landing light. ON On final: Flaps . LDG GO AROUND PROCEDURE Power . MAX Flaps . T/O Continue with take-off profile 01.12.2012 Diamond Aircraft Flight Training Division Page 7 20.6.2013 Malmin Ilmailukerho ry Edition # 16 Does not replace the Airplane Flight Manual Edition #1 Does not replace the Airplane Flight Manual
DA40 TDI G1000 NORMAL PROCEDURES AFTER LANDING CHECK 1 2 3 4 Flaps. UP Pitot heat . OFF Alternate air. CLOSED Landing/Taxi light . AS REQUIRED End of Checklist 1 2 3 4 PARKING CHECK 1 2 3 4 5 6 7 8 9 10 11 12 Parking brake. SET 1 Power lever. IDLE for 2 min. 2 ELT . 121,5 CHECKED 3 Engine / System page . CHECKED 4 Engine / Fuel page . TTL TIME IN SVC NOTED 5 Avionic master . OFF 6 Electrical consumers except STROBE .OFF 7 Engine Master . OFF 8 STROBE .OFF 9 (start key) Electric Master. OFF 10 Interior light . CHECKED OFF 11 Start key .REMOVED 12 End of Checklist OPERATING SPEEDS KIAS 850 kg 1000 kg 1150 kg Best gliding angle (Flaps UP 60 68 73 Best angle of climb (VX) Best rate of climb (VY) 54 60 66 Cruising climb speed 60 68 73 Rotating speed 49 55 59 Max. flap speed (VFE) T/O 108 Max. flap speed (VFE) LDG 91 Landing speed Flaps UP 60 68 73 Landing speed Flaps LDG 58 63 71 -980kg- Stalling speed (VS0) LDG 42 49 -980kg- Stalling speed (VS) T/O 44 51 -980kg- Stalling speed (VS) clean 47 52 Max. cruising speed (VNO) 129 Never exceed speed (VNE) 178 -980kg- Manoeuvring speed (VA) 94 108 Max. turbulence speed 129 Weights Empty weight 843 kg Max. TKOF weight 1150 kg Max. baggage weight 30 kg 01.12.2012MalminDiamond Aircraft Page 8 20.6.2013 Ilmailukerho ry Flight Training Division E d i t i o n # 1 6 D o e s n o t r e p l a c e t h e A i r p l a n e F l i g h t M anual Edition #1 Does not replace the Airplane Flight Manual
DA40 TDI G1000 EMERGENCY ABNORMAL CHECKLIST For conditions to use this Emergency Abnormal Checklist see page 1 of the Normal Checklist. All such conditions are fully applicable also for this checklist. G1000 WARNINGS ENG TEMP Pg. 2 Coolant temperature high (red range) OIL TEMP Pg. 2 Oil temperature high (red range) OIL PRES Pg. 2 Oil pressure low (red range) GBOX TEMP Pg. 3 Gearbox temperature high (red range) L/R FUEL TEMP Pg. 3 Fuel temperature high (red range) ALTN AMPS High Current (red range) ALTN FAIL Pg. 3 Pg. 3 STARTER Pg. 3 Starter not disengaging DOOR OPEN Pg. 3 Unlocked doors Alternator fail For other parameters “out of green range” see Abnormal Checklist Abnormal Checklist starts at page 9 Emergency landing . page 4 Engine Rough engine and/or power loss . page 4 Windmill engine start . page 5 Powered engine start. page 5 Fluctuating RPM. page 6 RPM overspeed . page 6 RPM underspeed . page 6 Electric System Under/over voltage . page 5 Total electrical fail . page 8 Smoke and Fire Fire / smoke on ground . page 7 Fire / smoke in continued TKOF. page 7 Electric fire / smoke in flight . page 7 Engine fire in flight . page 8 Other Emergencies Fuel transfer pump u/s . page 4 Suspicion of carbon monoxide . page 8 01.12.2012 Diamond Page 1 20.6.2013 Malmin Ilmailukerho ryAircraft Flight Training Division Edition # 16 Does not replace the Airplane Flight Manual Edition #1 Does not replace the Airplane Flight Manual
DA40 TDI G1000 ENG TEMP ¾ OIL TEMPERATURE HIGH Check oil pressure If too low: Reduce power Be prepared for loss of oil and engine fail; be prepared for emergency landing If in green range: Reduce power Increase airspeed OIL PRES ¾ ¾ COOLANT TEMPERATURE HIGH Check COOL LVL caution light If “COOL LVL” OUT: During climb: Reduce power 10% Increase airspeed 10 KIAS If not returning to green range within 60 seconds: reduce power as far as possible and increase airspeed During cruise: Reduce power Increase airspeed Check coolant temperature in green range If not returning to green range: land ASAP If “COOL LVL” ON: Reduce power Expect loss of coolant fluid Be prepared for emergency landing OIL TEMP ¾ EMERGENCY PROCEDURES OIL PRESSURE LOW Reduce power Be prepared for loss of oil and engine fail; be prepared for emergency landing 01.12.2012 Diamond Page 2 20.6.2013 Malmin Ilmailukerho ryAircraft Flight Training Division Edition # 16 Does not replace the Airplane Flight Manual Edition #1 Does not replace the Airplane Flight Manual
DA40 TDI G1000 GBOX TEMP ¾ ¾ GEARBOX TEMPERATURE HIGH Reduce power Increase airspeed L/R FUEL TEMP ¾ ¾ EMERGENCY PROCEDURES FUEL TEMPERATURE HIGH Reduce power Increase airspeed ALTN AMPS HIGH CURRENT Consumption of electrical power is too high ¾ Switch off electrical equipment to reduce electrical load x If problem not cleared: Land ASAP ALTN FAIL ALTERNATOR FAIL Batteries will last for about 30 minutes ¾ Check circuit breakers ¾ ¾ ¾ ESSENTIAL BUS: ON Switch off unnecessary electrical equipment Land ASAP Be prepared for engine fail and emergency landing x If all CBs OK: STARTER ¾ ¾ ¾ Power lever IDLE Engine master OFF Electric master OFF DOOR OPEN ¾ ¾ STARTER NOT DISENGAGING UNLOCKED DOORS Reduce airspeed Check canopy and rear door visually x If canopy and/or rear door unlocked: Airspeed below 140 KIAS Land ASAP Do not try to lock the rear door in fligh 01.12.2012 Diamond Page 3 20.6.2013 Malmin Ilmailukerho ryAircraft Flight Training Division Edition # 16 Does not replace the Airplane Flight Manual Edition #1 Does not replace the Airplane Flight Manual
DA40 TDI G1000 EMERGENCY PROCEDURES EMERGENCY LANDING 1 2 3 4 Airspeed. 73/68/60 kts ATC . INFORM Emergency fuel valve. OFF Engine Master . OFF On final: 5 Flaps .LDG 6 Electric master switch . OFF 1 2 3 4 5 6 FUEL TRANSFER PUMP U/S 7 8 9 10 Emergency fuel valve. EMERG. TRANSFER AUX fuel quantity . CHECK min 1 USG MAIN fuel quantity.CHECK max 15 USG Emergency fuel valve. Reset to NORMAL 1 2 3 4 ROUGH ENGINE AND/OR POWER LOSS 1 Airspeed.73/68/60 KIAS 2 Power lever . MAX 3 G1000 annunciations . CHECK If ON: go to appropriate checklist 4 Alternate air . in icing conditions: OPEN 5 Main tank fuel quantity . CHECK 6 Fuel transfer pump . ON 7 Emergency fuel valve. CHECK NORMAL 8 ECU swap. ECU B ECU reset: 9 Engine master. OFF – ON 1 2 3 4 5 6 7 8 9 If no success: 10 ECU swap. AUTO 10 If no success and insufficient power: Land ASAP 01.12.2012 Diamond Page 4 20.6.2013 Malmin Ilmailukerho ryAircraft Flight Training Division Edition # 16 Does not replace the Airplane Flight Manual Edition #1 Does not replace the Airplane Flight Manual
DA40 TDI G1000 EMERGENCY PROCEDURES WINDMILL ENGINE START 1 2 3 4 5 6 7 8 9 10 Airspeed. 73 - max 110 KIAS 1 Pressure Altitude .max 6000 ft 2 Power lever . IDLE 3 Emergency fuel valve. CHECK NORMAL 4 Alternate air . OPEN 5 Fuel transfer pump . ON 6 Avionic master . OFF 7 Electric master . ON 8 Engine master. OFF, then ON 9 Avionic master . ON 10 POWERED ENGINE START 1 2 3 4 5 6 7 8 9 10 11 12 13 Gliding airspeed .73/68/60 KIAS Pressure Altitude .max 6000 ft Engine master. OFF Power lever . IDLE Emergency fuel valve. CHECK NORMAL Alternate air . OPEN Fuel transfer pump . ON Avionic master . OFF Electric master . ON Engine master. ON Glow indication . CHECK ON, wait for OFF Electric master . START Avionic master . ON 1 2 3 4 5 6 7 8 9 10 11 12 13 UNDER / OVER VOLTAGE 1 Essential bus . ON Land ASAP 1 01.12.2012 Diamond Page 5 20.6.2013 Malmin Ilmailukerho ryAircraft Flight Training Division Edition # 16 Does not replace the Airplane Flight Manual Edition #1 Does not replace the Airplane Flight Manual
DA40 TDI G1000 EMERGENCY PROCEDURES FLUCTUATING RPM 1 Power lever . CHANGE SETTING If no success: 2 ECU swap. ECU B If no success: 3 ECU swap. AUTO If no success: Land ASAP 1 2 3 RPM OVERSPEED 1 2 3 4 Power lever . ADJUST to max. 2300 RPM Flaps . UP Airspeed. 73 KIAS Power lever . AS REQUIRED but do not exceed 2300 RPM 5 ECU swap. ECU B x If no success: 6 ECU swap. AUTO Land ASAP 1 3 2 5 7 If increased climb rate required: 7 Flaps . T/O 8 8 Airspeed. 66 KIAS 9 9 Power lever . ADJUST to max. 2300 RPM 10 RPM UNDERSPEED 1 Power lever . AS REQUIRED 2 ECU swap. ECU B x If no success: 3 ECU swap. AUTO Land ASAP 1 2 3 01.12.2012 Diamond Page 6 20.6.2013 Malmin Ilmailukerho ryAircraft Flight Training Division Edition # 16 Does not replace the Airplane Flight Manual Edition #1 Does not replace the Airplane Flight Manual
DA40 TDI G1000 EMERGENCY PROCEDURES FIRE / SMOKE ON GROUND 1 2 3 4 5 6 Power lever . IDLE Cabin heat. OFF Emergency fuel valve. OFF Fuel transfer pump . OFF Engine master. OFF Electric master . OFF When engine stopped: 7 Canopy . OPEN Evacuate 1 2 3 4 5 6 7 FIRE / SMOKE DURING CONTINUED TKOF 1 Cabin heat. OFF Land ASAP When landing assured: 2 Emergency fuel valve. OFF 3 Fuel transfer pump . OFF 4 Engine master. OFF 5 Electric master . OFF 6 Emergency window. OPEN as necessary 7 Canopy .UNLATCH as necessary 1 2 3 4 5 6 7 ELECTRIC FIRE / SMOKE IN FLIGHT 1 2 3 4 5 6 Emergency switch . ON Avionic master . OFF Electric master . OFF Cabin heat. OFF Emergency window. OPEN as necessary Canopy .UNLATCH as necessary Land ASAP 1 2 3 4 5 6 01.12.2012 Diamond Page 7 20.6.2013 Malmin Ilmailukerho ryAircraft Flight Training Division Edition # 16 Does not replace the Airplane Flight Manual Edition #1 Does not replace the Airplane Flight Manual
DA40 TDI G1000 EMERGENCY PROCEDURES ENGINE FIRE IN FLIGHT 1 2 3 4 5 6 7 8 9 10 11 Cabin heat. OFF 1 Emergency landing . PREPARE 2 Airspeed.73/68/60 KIAS 3 ATC .
1 Check Aircraft papers 2 Remove pitot cover 3 Check interior for foreign objects 4 Check flight controls free 5 Check circuit breakers 6 Emergency Fuel Valve NORMAL 7 Engine Master OFF 8 ECU SWAP AUTO 9 Essential bus OFF 10 Avionic Master electrics OFF 11 Electric Master ON Check battery voltage 12 Check fuel quantity temp 13 External light.
TDI 2.5L 140/150/165 TDI 150‑5/TDI 150‑5 D/TDI 165‑5 EXVWM004 R4 TD; TDI 1.9L 75 TDI 75‑4 EXVWM006 TDI 3.0L 230/260 TDI 230‑6/TDI 260‑6 EXVWM007 TDI 4.2L 285/350 TDI 285‑8/TDI 350‑8 EXVWM008 Essential requirements Standards Other normative document/ method Technical file Please specify in more detail (* mandatory standard)
DA40 VARIANTS (Images from top to bottom) DA40 NG, DA40 Tundra Star, DA40 XLT Lycoming. "Taking delivery of a brand new DA40 NG was a dream come true. I have been the happy owner of a DA42 and had long wanted to add a sister single engine plane alongside the twin - for my owner-run rental business. I took the plunge and ordered the DA40 NG .
DA40 VARIANTS (Images from top to bottom) DA40 NG, DA40 Tundra Star, DA40 XLT Lycoming. "Taking delivery of a brand new DA40 NG was a dream come true. I have been the happy owner of a DA42 and had long wanted to add a sister single engine plane alongside the twin - for my owner-run rental business. I took the plunge and ordered the DA40 NG .
the airplane's design We think Diamond can rightly claim the best safety record in light aircraft GA." Aviation Consumer Diamond DA40 Used Aircraft Guide "The DA40 XLS was designed to be the best plane a new pilot could buy - and it truly is. No one should buy a plane in this category without first flying the DA40 XLS.
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2.0L TDI (CBEA) All All All Golf, Jetta, Jetta SportWagen 2010-2013 2.0L TDI (CJAA) All All All Passat 2012-2013 2.0L TDI (CKRA) All All All Touareg 2009-2010 3.0L TDI (CKRA) All All All Touareg 2011-2013 3.0L TDI (CNRB) All All All Beetle 2013 2.0L TDI (CJAA) All All All Condition
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190-00324-07 Rev. A Garmin G1000 Cockpit Reference Guide for the DA40/40F WARNINGS, CAUTIONS, & NOTES WARNING: The Garmin G1000, as installed in the Diamond DA40 aircraft, has a very high degree of functional integrity. However, the pilot must recognize that providing monitoring and/or self-test capability for all
