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Cessna 400 Corvalis TT Startup Checklist
FLIGHT2.25.0Checklist
Cessna 400 Corvalis TTMSFS 2024 · Startup Checklist · 260 steps · 20 phases
PHS 1 - Pre-Flight Planning8 steps
| 01 | Weather Briefing (METAR / TAF)REVIEWEDNOTE: Flight into known icing is prohibited (POH Section 2). Hot weather and high altitude raise the chance of fuel vapor, so plan on Vapor Suppression use. | |
| 02 | NOTAMsREVIEWED | |
| 03 | Cruise Altitude and OxygenPLANNEDCAUTION: POH limit: 25,000 ft MSL maximum with an approved oxygen installation, 14,000 ft MSL without. Flaps may not be extended above 14,000 ft PA. | |
| 04 | Fuel RequiredCALCULATEDCAUTION: The POH copy used gives two usable figures: 98 US gal (Section 1) and 102 US gal (Section 2). The red line at zero on each gauge marks 2 gal that cannot be used safely in flight. Plan on the lower figure.NOTE: 106 US gal total, 53 per tank. Normal fuel flow 13 to 25 GPH. Cruise at 85% (2,500 RPM, 31.5 in.) burns about 23 to 25 GPH; 65% (2,500 RPM, 25 in.) about 16 to 18 GPH. | |
| 05 | Weight and BalanceWITHIN LIMITSCAUTION: Max ramp and takeoff weight 3,600 lbs, max landing weight 3,420 lbs, max baggage 120 lbs (hat rack 20 lbs). Load baggage Zone A first. | |
| 06 | Takeoff and Landing PerformanceCALCULATEDNOTE: POH Section 5 short field charts: takeoff with 12 deg flaps, rotate 64 to 75 KIAS by weight; landing with 40 deg flaps, minimum approach 73 to 82 KIAS. Max demonstrated crosswind 23 kts (not limiting). | |
| 07 | Flight Plan / G1000 RoutePREPARED | |
| 08 | Passenger BriefingCOMPLETENOTE: Gull wing doors, seat belts, oxygen masks and cannulas, and the passenger briefing card. Max four occupants. |
PHS 2 - Preflight - Cabin (Area 1)20 steps
| 01 | Pitot Tube CoverREMOVE AND STORE | |
| 02 | Required Aircraft DocumentsAVAILABLE IN THE AIRPLANE | |
| 03 | Ignition SwitchOFF | |
| 04 | MixtureIDLE CUTOFF | |
| 05 | Avionics Master SwitchOFF | |
| 06 | Crosstie SwitchOFF | |
| 07 | Left Battery SwitchONNOTE: Press the right side of the split rocker switch. | |
| 08 | Right Battery SwitchONNOTE: Press the right side of the split rocker switch. | |
| 09 | A/P Trim System Switch (Overhead)CHECK ON | |
| 10 | FlapsTAKEOFF THEN LANDING POSITION | |
| 11 | Trim TabsNEUTRAL | |
| 12 | Fuel Quantity IndicatorsCHECK FUEL QUANTITY | |
| 13 | Fuel AnnunciationNOT DISPLAYED | |
| 14 | Oxygen System (If Required)CHECKNOTE: Avionics switch ON, oxygen system ON, check quantity, ensure the system retains pressure and verify flow at all breathing devices, then oxygen system OFF. | |
| 15 | Pitot Heat, Propeller Heat and Exterior LightsON AS REQUIRED, CHECK OPERATIONWARNING: The pitot tube can get hot within one minute. Do not run pitot heat for more than one to two minutes on the ground. | |
| 16 | Induction Heated AirCYCLE THEN OFF | |
| 17 | Stall Warning VaneCHECK WARNING HORN | |
| 18 | Pitot Heat, Propeller Heat, Exterior LightsOFF | |
| 19 | Left and Right Battery SwitchesOFF | |
| 20 | Circuit BreakersCHECK IN |
PHS 3 - Preflight - Exterior (Areas 2 to 8)49 steps
| 01 | Left FlapCHECKNOTE: Area 2. Proper extension and security of hardware. | |
| 02 | Left Wing Tie-DownREMOVE | |
| 03 | Left Aileron and Servo TabCHECKNOTE: Movement, condition and security of hardware; servo tab for proper operation. | |
| 04 | Left Static Wicks (2) and Wing TipCHECKNOTE: Wing tip for damage, position and anti-collision lights secure. | |
| 05 | Left Leading Edge, Tapes and Stall StripsCHECKCAUTION: All leading edge devices (stall strips, leading edge tape, flat triangular tape, zig zag tape) must be installed and in good condition for flight.NOTE: Area 3. Look for damage. | |
| 06 | Left Fuel VentCHECK FOR OBSTRUCTIONS | |
| 07 | Landing LightCHECKNOTE: Lens cracks and security. | |
| 08 | Left Fuel QuantityCHECK VISUALLY AND SECURE FILLER CAP | |
| 09 | Stall Warning VaneCHECK FREE MOVEMENT, NOT BENT | |
| 10 | Left Wing Fuel DrainCHECK FOR CONTAMINATIONNOTE: Before the first flight of the day or after refueling. | |
| 11 | Left Main Strut and TireCHECKNOTE: Remove chocks, tire inflation, strut for damage, bushing in place. | |
| 12 | Main Fuel DrainCHECK FOR CONTAMINATIONNOTE: Before the first flight of the day or after refueling. | |
| 13 | Gascolator Access Door and Inspection PanelsCHECK SECURE | |
| 14 | Left Windscreen, Cowl and ExhaustCHECKNOTE: Area 4 (nose). | |
| 15 | Engine OilCHECK LEVELNOTE: Maintain 6 to 8 quarts; fill to 8 for extended flights. | |
| 16 | Oil Filler Cap and Accessory DoorSECURE | |
| 17 | Propeller and SpinnerCHECKNOTE: Nicks, security, oil leakage. | |
| 18 | Alternator BeltCHECKNOTE: Condition and tension. | |
| 19 | Nose Wheel StrutCHECK INFLATIONNOTE: About 3 to 4 inches of chrome strut visible. | |
| 20 | Nose TireCHECKNOTE: Remove chocks, check inflation. | |
| 21 | Right Windscreen, Cowl, Cabin Air Inlet and ExhaustCHECKNOTE: Air inlet duct connected, no obstructions. | |
| 22 | Right Wing Fuel DrainCHECK FOR CONTAMINATIONNOTE: Area 5. | |
| 23 | Right Main Strut and TireCHECK | |
| 24 | Right Leading Edge, Tapes and Stall StripsCHECK | |
| 25 | Right Fuel QuantityCHECK VISUALLY AND SECURE FILLER CAP | |
| 26 | Right Fuel VentCHECK FOR OBSTRUCTIONS | |
| 27 | Pitot TubeCHECK FOR OBSTRUCTIONS | |
| 28 | Right Wing TipCHECKNOTE: Area 6. Damage, position and anti-collision lights secure. | |
| 29 | Right AileronCHECK | |
| 30 | Aileron Trim TabCHECK NEUTRAL | |
| 31 | Right Static Wicks (2)CHECK | |
| 32 | Right Wing Tie-DownREMOVE | |
| 33 | Right FlapCHECK | |
| 34 | Antennas (Bottom of Fuselage)CHECK SECURE | |
| 35 | Static PortCHECK FOR BLOCKAGE | |
| 36 | Horizontal and Vertical Leading EdgesCHECKNOTE: Area 7 (tail). Look for damage. | |
| 37 | Leading Edge Tape and Zig Zag TapeCHECK ATTACHED, GOOD CONDITION | |
| 38 | Antennas (Vertical Stabilizer)CHECK SECURE | |
| 39 | Rudder / Elevator HardwareCHECK | |
| 40 | Rudder SurfaceCHECK FREEDOM OF MOVEMENT | |
| 41 | Fixed Elevator SurfacesCHECK SECURE, CLEARANCE TO RUDDER AT FULL DEFLECTION | |
| 42 | Elevator SurfaceCHECK FREEDOM OF MOVEMENT | |
| 43 | Elevator Trim TabCHECK NEUTRAL | |
| 44 | Ventral FinCHECK SECURE, NO LOWER EDGE DAMAGE | |
| 45 | Tail Static Wicks (5)CHECK | |
| 46 | Tail Tie-DownREMOVE | |
| 47 | Baggage DoorCHECK CLOSED AND LOCKEDNOTE: Area 8 (aft fuselage and cabin). | |
| 48 | Fire ExtinguisherCHECK PRESENT AND SECURE | |
| 49 | Crash Ax / HatchetCHECK PRESENT AND SECURE |
PHS 4 - Before Starting Engine10 steps
| 01 | Preflight InspectionCOMPLETE | |
| 02 | Fresh Air VentsCLOSED FOR ENGINE START | |
| 03 | Seat Belts and Shoulder HarnessSECURENOTE: Stow all unused seat belts. | |
| 04 | Fuel SelectorLEFT OR RIGHT TANK | |
| 05 | Avionics Master SwitchOFFCAUTION: The start draws a large current. The avionics master must be OFF during starting to prevent serious damage to the avionics. | |
| 06 | Crosstie SwitchVERIFY OFF | |
| 07 | BrakesTESTED AND SET | |
| 08 | Circuit BreakersCHECK IN | |
| 09 | Oxygen Masks and CannulasCHECKNOTE: Kinks in hose, rips or tears. | |
| 10 | Passenger Briefing CardADVISE PASSENGERS TO REVIEW |
PHS 5 - Starting Engine (Cold)14 steps
| 01 | MixtureRICH | |
| 02 | PropellerHIGH RPM | |
| 03 | Vapor SuppressionOFF | |
| 04 | Induction Heated AirOFF | |
| 05 | ThrottleCLOSED, THEN OPEN APPROX. 1 INCH | |
| 06 | Left and Right Battery SwitchesON | |
| 07 | Anti-Collision / Position LightsON AS REQUIRED | |
| 08 | Primer SwitchPUSH IN (APPROX. 5 SEC)NOTE: Hot engine (POH Starting Hot Engine): mixture IDLE CUTOFF, throttle CLOSED, Vapor Suppression ON for 30 to 60 seconds then OFF, mixture RICH, prime about 3 seconds, throttle open about 1/4 inch. | |
| 09 | ThrottleCLOSED, THEN OPEN 1/8 TO 1/4 INCH | |
| 10 | Propeller AreaCLEAR | |
| 11 | Ignition SwitchSTART | |
| 12 | ThrottleADJUST IDLE 900 - 1,000 RPM | |
| 13 | Oil PressureCHECK 30 - 60 PSIWARNING: If no oil pressure is noted within 30 seconds, shut down the engine and investigate. | |
| 14 | Left and Right Alternator SwitchesONNOTE: Listed as the final item of the POH Starting Hot Engine checklist. |
PHS 6 - After Engine Start12 steps
| 01 | Avionics Master SwitchON | |
| 02 | Engine Indication SystemsCHECK | |
| 03 | AmmetersCHECKNOTE: No alternator annunciation; both alternators charging. | |
| 04 | MFD Fuel RemainingINITIALIZE | |
| 05 | COM RadiosSET | |
| 06 | NAV RadiosSET | |
| 07 | PFD and Backup AltimetersSET | |
| 08 | FMS Flight PlanLOADED | |
| 09 | Altitude and Heading BugsSET | |
| 10 | TransponderSET | |
| 11 | Oxygen QuantityNOTE | |
| 12 | Rudder HoldON, VERIFY OVERRIDE BY PEDAL FORCE, THEN OFF |
PHS 7 - SpeedBrake and Autotrim Checks14 steps
| 01 | SpeedBrake SwitchON / UP | |
| 02 | SPEED BRAKES AnnunciationDISPLAYED | |
| 03 | SpeedBrake SwitchOFF / DOWNCAUTION: If a SpeedBrake stays slightly extended it has failed; pull the SpeedBrake circuit breaker.NOTE: Ensure both SpeedBrakes are retracted. Functionally check before flight to synchronise the clutches. | |
| 04 | SPEED BRAKES AnnunciationCLEARS | |
| 05 | AutopilotENGAGE | |
| 06 | Control StickFORWARD PRESSURE - TRIM RUNS NOSE UP AFTER 3 SEC | |
| 07 | Control StickAFT PRESSURE - TRIM RUNS NOSE DOWN AFTER 3 SEC | |
| 08 | Electric Trim SwitchMOVE UP AND DOWN, AUTOPILOT DISCONNECTSNOTE: Trim should run in the commanded direction. | |
| 09 | AutopilotENGAGE | |
| 10 | HDG BugSYNC | |
| 11 | AutopilotSELECT HDG MODE | |
| 12 | HDG BugVERIFY CONTROL STICK MOVEMENT | |
| 13 | A/P Disconnect / Trim Interrupt SwitchPRESS, AUTOPILOT DISCONNECTS | |
| 14 | TrimSET FOR TAKEOFFWARNING: If autotrim fails any part of this check, do not use the autopilot until the fault is corrected.NOTE: Check all controls free and the autopilot disconnected. |
PHS 8 - Before Taxi7 steps
| 01 | Engine InstrumentsCHECK WITHIN RANGES | |
| 02 | Fuel GaugesCHECK PROPER INDICATION | |
| 03 | AmmetersCHARGING | |
| 04 | Wing FlapsTAKEOFF, THEN UP (CRUISE) | |
| 05 | Radio ClearanceAS REQUIRED | |
| 06 | Taxi LightAS REQUIRED | |
| 07 | BrakesRELEASE |
PHS 9 - Taxiing4 steps
| 01 | BrakesCHECK | |
| 02 | PFD and Backup Flight InstrumentsCHECK | |
| 03 | Turn Coordinator (PFD)CHECK | |
| 04 | Directional Gyro (PFD)CHECK |
PHS 10 - Before Takeoff (Runup)38 steps
| 01 | Runup PositionMAXIMUM HEADWIND COMPONENT | |
| 02 | Parking Brake / Foot BrakesSET OR HOLD | |
| 03 | Flight ControlsFREE AND CORRECT | |
| 04 | Crosstie SwitchVERIFY OFF | |
| 05 | A/P Trim System (Overhead)VERIFY ON | |
| 06 | AutopilotVERIFY DISENGAGED | |
| 07 | Trim TabsSET FOR TAKEOFF | |
| 08 | PFD and Backup Flight InstrumentsCROSSCHECK AND SET | |
| 09 | Fuel SelectorSET OUT OF DETENTNOTE: The aural warning should play 2 seconds after the annunciation appears. | |
| 10 | ALERTS Softkey (PFD)PRESSNOTE: Aural warning stops. | |
| 11 | Fuel SelectorFULLER TANK | |
| 12 | Cabin DoorsCLOSED AND LATCHEDNOTE: Red door annunciation not displayed. | |
| 13 | Passenger Side Door LockUNLOCKED POSITION | |
| 14 | Oil TemperatureABOVE 100 DEG F | |
| 15 | Throttle1,700 RPM | |
| 16 | Ignition SwitchLNOTE: 25 RPM drop minimum, 150 RPM maximum; EGTs should rise. | |
| 17 | Ignition SwitchRWARNING: No RPM drop may mean a hot (ungrounded) magneto. The engine could start if the propeller is moved by hand. Correct before operating.NOTE: 25 RPM drop minimum, 150 RPM maximum; EGTs should rise. | |
| 18 | Ignition SwitchR/L (BOTH)NOTE: EGTs should drop. | |
| 19 | PropellerCYCLE 2 - 3 TIMESNOTE: 300 to 500 RPM drop. | |
| 20 | Engine Instruments and AmmeterCHECK WITHIN RANGES | |
| 21 | BatteriesVERIFY CHARGENOTE: At 1,700 RPM the charge rate should be under 10 amps for each battery. | |
| 22 | ThrottleVERIFY IDLE, THEN 900 - 1,000 RPM | |
| 23 | Illuminated Switch Bulb TestALL LAMPS ILLUMINATED | |
| 24 | RadiosSET, CROSSCHECK NAV INDICATORS | |
| 25 | Flight DirectorAS REQUIRED | |
| 26 | TransponderVERIFY CODE | |
| 27 | Wing FlapsTAKEOFF POSITION (12 DEG) | |
| 28 | Rudder Hold SystemDISENGAGED | |
| 29 | SpeedBrake SwitchVERIFY OFF / DOWN | |
| 30 | DoorsLATCHED AND DETENTED | |
| 31 | PFD Annunciator WindowALL MESSAGES ADDRESSED | |
| 32 | Door SealsON | |
| 33 | Backup Fuel PumpARMED | |
| 34 | Oxygen SystemON (IF REQUIRED) | |
| 35 | Mask or CannulaDON (IF REQUIRED) | |
| 36 | FlowmetersSET FOR PLANNED CRUISE ALTITUDE | |
| 37 | TimeNOTE | |
| 38 | BrakesRELEASE |
PHS 11 - Normal Takeoff9 steps
| 01 | Landing / Taxi LightsAS REQUIRED | |
| 02 | Wing FlapsTAKEOFF POSITION | |
| 03 | MixtureFULL RICH | |
| 04 | Backup Fuel PumpARMED | |
| 05 | Pitot Heat and Propeller HeatAS REQUIRED | |
| 06 | ThrottleADVANCE SLOWLY TO FULL POWER (2,600 RPM)CAUTION: Watch manifold pressure for overboost. Limit 35.5 in. Hg. | |
| 07 | Elevator ControlLIFT NOSE AT 75 KIASNOTE: Short field: brakes held to full power, level nose attitude, rotate 64 to 75 KIAS (5 deg nose up) and climb 74 to 84 KIAS by weight until clear of obstacles. | |
| 08 | Climb SpeedACCELERATE TO 110 KIAS (Vy) | |
| 09 | Wing FlapsRETRACT AT 400 FT AGL AND 95 KIAS OR ABOVE |
PHS 12 - Climb8 steps
| 01 | Airspeed110 KIAS (BEST RATE)NOTE: Cruise climb above 115 KIAS gives better visibility and cooling for long climbs. Do not lean in the climb. | |
| 02 | Power SettingsADJUST AS NECESSARYNOTE: Maximum performance climb: 2,600 RPM and full throttle at 110 KIAS. | |
| 03 | Fuel SelectorLEFT OR RIGHT TANK AS APPROPRIATE | |
| 04 | MixtureFULL RICH ABOVE 85% POWER | |
| 05 | Backup Fuel PumpARMED | |
| 06 | Vapor SuppressionON ABOVE 18,000 FTCAUTION: Also required ON if TIT rises above 1,460 deg F at full power with the mixture full rich, at any altitude. | |
| 07 | Rudder Hold SystemSET RUDDER AND ENGAGE | |
| 08 | Landing / Taxi LightsAS REQUIRED |
PHS 13 - Cruise13 steps
| 01 | Rudder Hold SystemAS REQUIRED | |
| 02 | ThrottleSET FOR 85% POWER OR LESSNOTE: Refer to the cruise performance tables. At 25,000 ft ISA, 2,500 RPM and 31.5 in. gives 85% for about 235 KTAS at 25 GPH. | |
| 03 | PropellerSET FOR 85% POWER OR LESSCAUTION: To increase power: mixture, then RPM, then manifold pressure. To decrease: manifold pressure, then RPM. Monitor TIT for the 1,750 deg F limit. | |
| 04 | MixtureLEAN AS REQUIREDCAUTION: Above 18,000 ft do not pull the throttle to idle without leaning; the over-rich mixture can flood and stop the engine. Minimum above 18,000 ft: 15 in. Hg and 2,200 RPM.NOTE: Use the TIT gauge: 1,625 deg F for best power. Above 75% power only rich of peak is permitted (65% in the amplified procedures); below 65% the engine may run 50 deg F lean of peak. | |
| 05 | Backup Fuel PumpOFF | |
| 06 | Vapor Suppression (Tank Change)ON DURING FUEL TANK CHANGEOVERNOTE: Turn it off again once the engine runs normally, except above 18,000 ft where it stays on. | |
| 07 | Fuel SelectorCHANGE AS REQUIREDCAUTION: Maximum fuel imbalance 10 US gal. | |
| 08 | Landing / Taxi LightsAS REQUIRED | |
| 09 | Oxygen QuantityCHECK EVERY ~20 MIN | |
| 10 | Oxygen Outlet PressureCHECK EVERY ~20 MIN | |
| 11 | Flowmeter / Flow IndicatorCHECK FLOW EVERY ~10 MIN | |
| 12 | Altitude ChangeADJUST FLOW DEVICES TO NEW ALTITUDE | |
| 13 | Physiological RequirementADJUST FLOW DEVICE TO HIGHER ALTITUDE |
PHS 14 - Descent8 steps
| 01 | Fuel SelectorLEFT OR RIGHT TANK AS APPROPRIATE | |
| 02 | Power SettingsAS REQUIREDNOTE: Reduce power gradually and enrich gradually. Do not let CHT drop below 240 deg F for more than five minutes. For a long fast descent use the SpeedBrakes rather than a large power cut. Expedited descent: 2,400 RPM, about 25 in., SpeedBrake ON, 165 KIAS. | |
| 03 | MixtureAS REQUIRED | |
| 04 | Backup Fuel PumpOFFCAUTION: Keep it OFF in descent: at very low power the fuel pressure can drop below 5.5 psi, the armed pump then switches on and can flood and stop the engine. | |
| 05 | Vapor SuppressionOFF BELOW 18,000 FT | |
| 06 | PFD and Backup AltimetersSET | |
| 07 | Altitude BugSET | |
| 08 | Landing / Taxi LightsAS REQUIRED |
PHS 15 - Approach9 steps
| 01 | ApproachLOADED INTO FLIGHT PLAN | |
| 02 | PFD Baro MinimumsSET | |
| 03 | GPS RAIM / Map IntegrityVERIFY | |
| 04 | PFD OBS / SUSP SoftkeyREVIEW AND BRIEF | |
| 05 | PFD CDI ButtonSELECT NAV SOURCENOTE: Passing the FAF a new course may be needed. | |
| 06 | Nav AidsTUNED AND IDENTIFIED | |
| 07 | Approach CourseSET | |
| 08 | PFD and Backup AltimetersSET | |
| 09 | MixtureFULL RICH |
PHS 16 - Before Landing7 steps
| 01 | Seat Belts and Shoulder HarnessesSECURE | |
| 02 | MixtureFULL RICH | |
| 03 | Fuel SelectorLEFT OR RIGHT TANK AS APPROPRIATE | |
| 04 | Backup Fuel PumpOFF | |
| 05 | PropellerHIGH RPM | |
| 06 | Rudder Hold SystemDISENGAGED | |
| 07 | AutopilotDISENGAGED (IF APPLICABLE)NOTE: Coupled approaches: disconnect at 200 ft AGL. Avoid 1,800 to 1,850 RPM on an ILS; it can interfere with glideslope reception. |
PHS 17 - Normal Landing5 steps
| 01 | Approach AirspeedAS REQUIRED FOR CONFIGURATIONCAUTION: Vfe full flaps 117 KIAS; takeoff flaps 127 KIAS.NOTE: Flaps cruise 95 - 100 KIAS, flaps takeoff 90 - 95 KIAS, flaps landing 85 - 90 KIAS. Short field: flaps landing, 90 KIAS initial, 73 - 82 KIAS minimum by weight. | |
| 02 | Trim TabsADJUST AS REQUIRED | |
| 03 | TouchdownMAIN WHEELS FIRST | |
| 04 | Landing RollGENTLY LOWER NOSE WHEEL | |
| 05 | BrakingAS REQUIRED |
PHS 18 - Balked Landing (Go-Around)7 steps
| 01 | ThrottleFULL (2,600 RPM) | |
| 02 | SpeedBrake SwitchOFF / DOWN | |
| 03 | Wing FlapsTAKEOFF POSITION | |
| 04 | Airspeed82 KIAS | |
| 05 | ClimbPOSITIVE RATE | |
| 06 | Backup Fuel PumpARM | |
| 07 | Wing FlapsRETRACT AT 400 FT AGL AND 95 KIAS OR ABOVE |
PHS 19 - After Landing6 steps
| 01 | Wing FlapsUP (CRUISE) | |
| 02 | SpeedBrake SwitchOFF / DOWN | |
| 03 | Door Seal, Pitot Heat and Propeller HeatOFF | |
| 04 | TransponderVERIFY STANDBY / GROUND | |
| 05 | Landing / Taxi LightsAS REQUIRED | |
| 06 | TimeNOTE |
PHS 20 - Shutdown12 steps
| 01 | Parking BrakeSET | |
| 02 | ThrottleIDLE (900 RPM) | |
| 03 | Oxygen SystemOFF | |
| 04 | ELTCHECK NOT ACTIVATED | |
| 05 | Trim TabsSET TO NEUTRAL | |
| 06 | CooldownCOMPLETECAUTION: Idle at 900 RPM for 5 minutes before shutdown to cool the turbochargers. Taxi time counts. | |
| 07 | Avionics Master SwitchOFF | |
| 08 | Electrical / Environmental EquipmentOFF | |
| 09 | MixtureIDLE CUTOFF | |
| 10 | Left and Right Master SwitchesOFF | |
| 11 | Ignition SwitchOFF (AFTER ENGINE STOPS) | |
| 12 | Anti-Collision / Position LightsOFF |