MSFS 2024 · General Aviation
Daher TBM 930 Startup Checklist
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Daher TBM 930 Startup Notes
First quirk: the red crash lever on the left console must be up or the airplane plays dead, and it catches almost everyone once. The start itself is a single-lever affair. With ignition and auxiliary boost pump in AUTO, hit the starter, watch Ng rise, and only at 13 percent move the throttle from cutoff into low idle. From there your job is pure ITT monitoring, because the PT6 will happily cook itself if the battery is weak or fuel came in early.
The classic mistakes are all about heat and electrons. Introducing fuel below 13 percent Ng is the fastest route to a hot start, and so is starting on a tired battery, so check voltage and use ground power if it is marginal. When ITT does surge, sim pilots tend to freeze and watch; the correct move is throttle back to cutoff immediately while the starter keeps motoring to cool the engine. And again: crash lever up before you blame the sim.
Common mistakes
- Introducing fuel below 13 percent Ng
- Forgetting the crash lever and finding a dead cockpit
- Starting on a weak battery instead of ground power
Related Aircraft
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FLIGHT2.4.0Checklist
Daher TBM 930MSFS 2024 · Startup Checklist · 183 steps · 14 phases
PHS 1 — Pre-Flight Planning8 steps
| 01 | Weather Briefing (METAR / TAF)REVIEWEDNOTE: Check departure, enroute, destination, and alternate weather. The TBM 930 is FIKI certified but icing awareness is critical - verify ISA conditions and forecast icing layers. | |
| 02 | NOTAMsREVIEWEDNOTE: Check for runway closures, TFRs, airspace restrictions. Note any SIGMET for turbulence or icing on route. | |
| 03 | Fuel RequiredCALCULATEDNOTE: TBM 930 burns approx 55-65 USG/hr (360-420 lbs/hr). Usable fuel capacity 282 USG (1,880 lbs). Include IFR alternate fuel plus 45-min reserve. | |
| 04 | Weight and BalanceWITHIN LIMITSCAUTION: MTOW is 7,394 lbs (3,354 kg). Verify passenger and baggage weights. CG must remain within envelope throughout the flight as fuel burns off. | |
| 05 | Takeoff and Landing DistancesCALCULATEDNOTE: Sea level MTOW takeoff roll approximately 2,500 ft. Landing roll approximately 2,400 ft. Adjust for density altitude, runway slope, and surface condition. | |
| 06 | V-Speeds CalculatedNOTEDNOTE: Note Vr, Vy, Vx, and Vref for actual takeoff and landing weights. Garmin G3000 avionics will display computed speeds when weight is entered. | |
| 07 | G3000 Flight PlanPLANNEDNOTE: Prepare route for entry into the Garmin G3000 touchscreen avionics. Load SID, enroute waypoints, STAR, and approach. | |
| 08 | Flight PlanFILED |
PHS 2 — Before Start25 steps
| 01 | Parking BrakeSET | |
| 02 | Battery 1 and Battery 2 SwitchesONNOTE: Both batteries on. Avionics will begin to power up. Verify voltages on the electrical synoptic. | |
| 03 | External PowerCONNECT (if available)NOTE: Use GPU to conserve battery during avionics initialization on extended ground operations. | |
| 04 | Avionics - G3000INITIALIZINGNOTE: Allow G3000 displays to fully boot. MFD and PFDs require 60-90 seconds to initialize databases. | |
| 05 | G3000 - Aircraft ConfigurationCONFIRM WEIGHT ENTEREDNOTE: Enter actual ZFW on the G3000 MFD to enable computed V-speeds and performance data. | |
| 06 | Flight Plan - G3000ENTERED AND VERIFIEDNOTE: Load route on G3000 FPL page. Verify departure, SID, route, STAR, and approach. Confirm correct runway and transition. | |
| 07 | Fuel QuantityCHECK - SUFFICIENTNOTE: Usable fuel 282 USG (1,880 lbs). Verify quantity on fuel synoptic page. Cross-check with physical sight gauges. | |
| 08 | Fuel SelectorON (MAIN TANKS)NOTE: Verify fuel selector is in the ON/MAIN position, not OFF. | |
| 09 | Condition LeverFUEL CUTOFF (Full Aft)NOTE: Condition lever must be in FUEL CUTOFF before starter engagement. | |
| 10 | Power Lever (Throttle)GROUND IDLE (Idle Detent)NOTE: Power lever at idle stop before start. | |
| 11 | Generator SwitchONNOTE: Generator switch ON. It will come online after engine reaches self-sustaining speed. | |
| 12 | Ice Protection SwitchesOFF - CHECK CONDITIONSNOTE: All FIKI switches verify OFF for start. Plan anti-ice use based on weather briefing. | |
| 13 | Pitot / Static HeatONNOTE: Pitot and static heating should be ON prior to flight in any IMC conditions. Leave on for all flights as standard practice. | |
| 14 | Circuit BreakersCHECK INNOTE: Verify all circuit breakers are set. Check panel for any popped breakers. | |
| 15 | Flight ControlsFREE AND CORRECTNOTE: Verify full deflection of ailerons, elevator, and rudder. Confirm correct sense of movement against stick inputs on G3000 controls page. | |
| 16 | Elevator TrimSET FOR TAKEOFF (5 deg nose up typical)NOTE: Set elevator trim to appropriate takeoff position per weight and balance. Typically 3-5 units nose-up. | |
| 17 | Rudder TrimNEUTRAL | |
| 18 | FlapsTO (Takeoff position)NOTE: Set flaps to TO detent for normal takeoff. Verify on flap position indicator. | |
| 19 | Pressurization - Cabin AltitudeSET DESTINATION ELEVATIONNOTE: Set destination field elevation on pressurization controller. Verify AUTO mode selected. | |
| 20 | Oxygen SystemCHECK - PRESSURE ADEQUATENOTE: Crew oxygen pressure check. TBM 930 is pressurized to FL310 but carry oxygen per regulations. | |
| 21 | Passenger BriefingCOMPLETENOTE: Brief passengers on seatbelts, emergency exits, no smoking, pressurization, and sterile cockpit during critical phases. | |
| 22 | Doors and BaggageCLOSED AND LOCKEDCAUTION: The TBM 930 has a single cabin door and a separate baggage door. Both must be confirmed locked before start. A door ajar will illuminate the master warning. | |
| 23 | SeatbeltsFASTENED - PILOT AND PASSENGERS | |
| 24 | Beacon LightONNOTE: Turn on rotating beacon to signal imminent engine start to ground personnel. | |
| 25 | GSX - Fuel TruckREFUEL COMPLETENOTE: GSX menu: Refuel Aircraft. Set desired fuel load before confirming. |
PHS 3 — Engine Start11 steps
| 01 | Propeller AreaCLEAR - VERIFYCAUTION: Confirm no persons or objects within propeller arc before engaging starter. Call CLEAR PROP. | |
| 02 | Ignition SwitchAUTONOTE: Set ignition to AUTO for normal start. Ignitors will fire automatically when fuel is introduced. | |
| 03 | Starter SwitchENGAGE (Hold)NOTE: Engage starter. Monitor Ng (gas generator speed) winding up toward 13% before introducing fuel. | |
| 04 | Ng RisingMONITOR - INCREASINGNOTE: Watch Ng climb. PT6A-66D starter will crank the gas generator. Normal motoring time 5-10 seconds before fuel introduction. | |
| 05 | Condition LeverLOW IDLE (at 13% Ng)CAUTION: Do not introduce fuel (move condition lever) before 13% Ng. Risk of hot start if compressor airflow is insufficient.NOTE: At 13% Ng, move condition lever from CUTOFF to LOW IDLE. This introduces fuel and starts the combustion process. | |
| 06 | ITT - Monitor RiseRISING - WATCH CAREFULLYWARNING: ITT limit during start is 1,000 deg C. If ITT approaches 1,000 deg C, immediately return condition lever to CUTOFF and motor engine to cool. An ITT exceedance requires maintenance inspection. | |
| 07 | Starter - ReleaseRELEASE at 50% NgNOTE: Release starter at 50% Ng or when engine is clearly self-sustaining. Starter is rated for maximum 30-second cranking. | |
| 08 | Ng - Idle StabilizationSTABILIZE ~68-72% GROUND IDLENOTE: Engine stabilizes at ground idle. Allow 30-60 seconds for parameters to settle before checking gauges. | |
| 09 | Oil PressureIN GREEN (within 30 seconds)WARNING: If oil pressure does not rise within 30 seconds of fuel introduction, immediately return condition lever to CUTOFF and investigate before attempting another start. | |
| 10 | ITT at IdleWITHIN LIMITS (600-700 deg C typical)NOTE: Ground idle ITT typically 600-700 deg C. Max continuous ITT is 770 deg C. | |
| 11 | Oil TemperatureRISING - NORMALNOTE: Oil temperature should begin rising from ambient toward normal operating range of 10-104 deg C. |
PHS 4 — After Start13 steps
| 01 | Generator - OnlineCHECK CHARGINGNOTE: Verify generator came online and is charging. Check bus voltage on electrical synoptic page. Should read 28V DC. | |
| 02 | External PowerDISCONNECT (if used) | |
| 03 | Avionics - G3000FULLY INITIALIZED - CHECKNOTE: Verify all G3000 displays are fully initialized. PFD attitude, airspeed, altitude should all be valid. MFD showing map and engine data. | |
| 04 | AHRS / ADCALIGNED AND VALIDNOTE: Attitude Heading Reference System and Air Data Computer should show valid data. Cross-check PFD attitude with standby attitude indicator. | |
| 05 | Flight Plan - Verify ActiveCONFIRM ROUTE ACTIVENOTE: Verify correct route is active on G3000. Confirm first waypoint, SID, and destination are loaded correctly. | |
| 06 | Altimeter (PFD)SET QNHNOTE: Set altimeter to current QNH from ATIS. Verify altitude reading matches field elevation. | |
| 07 | Standby AltimeterSET QNHNOTE: Set standby altimeter to same QNH. Cross-check with PFD. | |
| 08 | Heading IndicatorALIGNED TO MAGNETIC COMPASSNOTE: Verify HSI/heading on PFD agrees with magnetic standby compass. | |
| 09 | TransponderSET SQUAWK CODE - STBYNOTE: Enter ATC squawk code and set transponder to STBY until cleared for taxi. | |
| 10 | Radios - COM1 / COM2SET ATIS AND GROUND FREQUENCIES | |
| 11 | ATISRECEIVED AND NOTEDNOTE: Note altimeter setting, winds, runway in use, and NOTAM info from ATIS. Confirm matches pre-flight weather. | |
| 12 | Condition LeverHIGH IDLE (after engine warm)NOTE: Once oil temperature is in the green arc (above 10 deg C) and all parameters stable, advance condition lever to HIGH IDLE for ground operations. | |
| 13 | Engine Parameters - Cross-CheckALL WITHIN LIMITSNOTE: Verify: Ng 68-75%, ITT 600-700 deg C, Oil Pressure 90-130 PSI, Oil Temp 10-104 deg C, Prop RPM 1,600-1,700 RPM at high idle. |
PHS 5 — Taxi10 steps
| 01 | Clearance DeliveryDEPARTURE CLEARANCE RECEIVEDNOTE: Contact clearance delivery with aircraft type, departure airport, destination, requested altitude, and squawk. Read back clearance. | |
| 02 | Taxi LightON | |
| 03 | Navigation LightsON | |
| 04 | Parking BrakeRELEASE | |
| 05 | BrakesCHECK - during first movementNOTE: Apply brakes gently as aircraft begins to roll to verify proper function before increasing taxi speed. | |
| 06 | PowerADVANCE SMOOTHLY - TAXI POWERNOTE: The PT6A-66D responds well to power inputs. Use modest power to achieve walking pace taxi speed. | |
| 07 | Taxi SpeedWALKING PACENOTE: Maintain walking pace appropriate to ramp conditions. Reduce speed before turns. | |
| 08 | Flight InstrumentsCHECK DURING TURNSNOTE: Verify attitude indicator stays level, compass and HSI track heading changes during taxi turns. | |
| 09 | Nosewheel SteeringRESPONSIVE ON TURNSNOTE: Verify nosewheel steering response is normal. TBM 930 uses differential braking plus rudder pedal steering. | |
| 10 | TransponderALT (as required by local procedures)NOTE: Many airports now require transponder ON (or ALT) while moving on surface. |
PHS 6 — Before Takeoff20 steps
| 01 | Parking BrakeSET (run-up position) | |
| 02 | Condition LeverHIGH IDLE - CONFIRM | |
| 03 | Power LeverADVANCE TO 1,000 FT-LBS TORQUE for run-upNOTE: Advance to approximately 1,000 ft-lbs torque or per POH run-up power. Verify ITT within limits during power increase. | |
| 04 | Ignition CheckCHECK BOTH - VERIFY NO EXCESSIVE ITT RISENOTE: Select LEFT then RIGHT ignition individually. Brief ITT rise is normal. Verify ITT and Ng remain stable. | |
| 05 | Prop CycleCYCLE - pull prop lever to MIN RPM then returnNOTE: Cycle prop governor to circulate warm oil. RPM should reduce then return to governed RPM when lever advanced. | |
| 06 | Torque / ITT / NgCHECK - WITHIN LIMITSNOTE: Verify torque, ITT, and Ng are within limits at run-up power before reducing to idle. | |
| 07 | Power LeverREDUCE TO IDLE after run-up | |
| 08 | Flight ControlsFREE AND CORRECT - FULL TRAVEL | |
| 09 | Elevator TrimCONFIRM TAKEOFF SETTING | |
| 10 | FlapsTO (Takeoff) - CONFIRM | |
| 11 | Pressurization ModeAUTO - DESTINATION SETNOTE: Confirm pressurization is in AUTO mode and destination elevation is set. | |
| 12 | Ice ProtectionAS REQUIRED - FIKI ON if icing conditionsNOTE: If icing conditions exist at or after departure, arm engine inlet, windshield, and prop FIKI prior to takeoff. | |
| 13 | Fuel QuantityVERIFY SUFFICIENTNOTE: Final fuel check. Verify quantity against flight plan fuel requirement. | |
| 14 | Autopilot / Flight DirectorVERIFY MODES SETNOTE: Pre-select autopilot modes if desired (heading, altitude). Autopilot should not be engaged for takeoff. | |
| 15 | TransponderALT (Mode C) | |
| 16 | LightsSTROBE ON, LANDING LIGHT ON | |
| 17 | Doors and WindowsCLOSED AND LOCKED - CONFIRM | |
| 18 | SeatbeltsFASTENED - ALL ABOARD | |
| 19 | Departure BriefingCOMPLETENOTE: Brief departure procedure, initial altitude, engine failure action (land straight ahead below Vr, return if above Vr with altitude), abort criteria. | |
| 20 | ATC ClearanceRECEIVEDNOTE: Contact tower for takeoff clearance. Read back runway, any crossing restrictions, and initial altitude restriction. |
PHS 7 — Takeoff9 steps
| 01 | Runway AlignmentCONFIRM ASSIGNED RUNWAYNOTE: Cross-check runway heading with HSI/PFD magnetic heading. Confirm runway number visible. | |
| 02 | Power LeverADVANCE SMOOTHLY TO MAX TORQUENOTE: Smoothly advance power lever to maximum takeoff torque (2,000 ft-lbs). Avoid abrupt power application which can cause propeller overspeed or ITT spike. | |
| 03 | Torque and ITTMONITOR - MAX 2,000 FT-LBS / 850 DEG CWARNING: Do not exceed 2,000 ft-lbs torque or 850 deg C ITT during takeoff roll. Reduce power immediately if limits are approached. | |
| 04 | Prop RPMCHECK 2,000 RPM (governed)NOTE: Prop governor should maintain 2,000 RPM throughout takeoff roll at full power. | |
| 05 | RudderRIGHT RUDDER - MAINTAIN CENTERLINENOTE: PT6A torque effect and P-factor require right rudder on the roll. Apply progressively as power is added. | |
| 06 | Rotation Speed (Vr)113 KIAS (typical) - ROTATENOTE: Apply steady back pressure at Vr. Rotate smoothly to approximately 10 deg nose up. Avoid over-rotation which can cause tail strike or reduced climb performance. | |
| 07 | Positive Rate of ClimbCONFIRM - GEAR UPNOTE: Once VSI shows positive climb, call POSITIVE RATE and raise gear. | |
| 08 | Landing GearUP - 3 LIGHTS TRANSIT THEN OFFCAUTION: Raise gear only after positive rate confirmed. Verify gear lights transition from green to out (gear up and locked). | |
| 09 | FlapsRETRACT ABOVE 400 FT AGLNOTE: Retract flaps once clear of obstacles and above 400 ft AGL. Do not retract below 200 ft AGL. |
PHS 8 — Climb13 steps
| 01 | Climb Speed124 KIAS (Vy) OR AS DESIREDNOTE: Vy 124 KIAS at sea level gives best rate of climb. Use Vx 104 KIAS for obstacle clearance. High-speed cruise climb 160-175 KIAS reduces engine temperatures. | |
| 02 | PowerMAX CONTINUOUS (2,000 FT-LBS / 850 DEG C MAX)NOTE: Maximum continuous torque for climb. Reduce power as required to keep ITT within continuous limits. | |
| 03 | Condition LeverHIGH IDLE - VERIFY | |
| 04 | Prop RPM2,000 RPM (governed) | |
| 05 | FlapsUP - VERIFY RETRACTED | |
| 06 | GearUP - VERIFY (3 LIGHTS OUT) | |
| 07 | AutopilotENGAGE (if desired above 400 ft AGL)NOTE: Engage autopilot after initial climb established. Select NAV mode for lateral guidance, VS or FLC for vertical. | |
| 08 | PressurizationCHECK - CABIN CLIMBING NORMALLYNOTE: Verify cabin altitude is climbing at 300-500 fpm toward cruise cabin altitude. Check differential pressure is normal. | |
| 09 | AltimeterSET 29.92 AT TRANSITION ALTITUDENOTE: Set standard pressure at transition altitude (18,000 ft in US). Coordinate with ATC. | |
| 10 | Landing LightOFF ABOVE 10,000 FT (optional) | |
| 11 | Engine GaugesMONITOR EVERY 5 MINUTESNOTE: Monitor ITT, torque, Ng, oil temp, and oil pressure regularly during climb. | |
| 12 | Ice ProtectionACTIVATE AS REQUIREDNOTE: Engage engine inlet anti-ice when OAT is below +5 deg C in visible moisture. Prop and windshield FIKI as needed. | |
| 13 | 10,000 ft CheckLANDING LIGHT AND SEATBELT SIGN AS REQUIREDNOTE: At 10,000 ft: review engine instruments, check fuel, brief passengers if seatbelt sign changes. |
PHS 9 — Cruise12 steps
| 01 | Cruise AltitudeLEVEL OFF - VERIFY ON ALTITUDENOTE: Typical cruise altitudes FL250-FL310 (max FL310). Set altitude bug, autopilot captures altitude. | |
| 02 | Power LeverREDUCE TO CRUISE TORQUENOTE: Typical cruise: 1,400-1,600 ft-lbs torque at FL280. Adjust for desired speed vs fuel efficiency. TAS 300+ kts possible at high altitude. | |
| 03 | Prop RPMREDUCE TO CRUISE RPM (1,700-1,800 RPM)NOTE: Reduce prop RPM from 2,000 to 1,700-1,800 RPM for cruise efficiency and reduced cabin noise. | |
| 04 | ITTMONITOR - MAX 770 DEG C CONTINUOUSNOTE: Typical cruise ITT 650-720 deg C. Adjust power lever as needed to stay within limits. | |
| 05 | Altimeter29.92 IN HG - VERIFY (above transition) | |
| 06 | PressurizationCHECK - CABIN ALTITUDE STABLENOTE: Verify cabin altitude is stable at cruise differential. Max differential is 6.0 PSI, providing sea-level equivalent cabin to approximately FL270. | |
| 07 | Fuel QuantityCHECK - BURN RATE CONSISTENTNOTE: Check fuel burn rate vs plan. Typical cruise burn 45-55 USG/hr at FL280. Verify sufficient fuel to destination plus reserves. | |
| 08 | RadiosSET ENROUTE FREQUENCIESNOTE: Monitor ATC frequency. Keep ATIS or ASOS for destination on COM2. | |
| 09 | TransponderALT - VERIFY SQUAWK CORRECT | |
| 10 | NavigationCHECK GPS COURSE, WAYPOINTS, ETANOTE: Verify G3000 is tracking correctly. Monitor fuel burn to ETA. Note any alternate diversion if needed. | |
| 11 | Ice ProtectionAS REQUIRED FOR CONDITIONSNOTE: Monitor for icing. FIKI system provides full ice protection. Engine anti-ice ON below +5 deg C in visible moisture. | |
| 12 | Top of DescentCALCULATENOTE: Use 3:1 ratio (3 nmi per 1,000 ft). From FL310 begin descent approximately 93 nmi from destination. |
PHS 10 — Descent11 steps
| 01 | ATIS / Destination WeatherOBTAINNOTE: Get destination ATIS at top of descent. Note altimeter setting, winds, runway in use, and any special conditions. | |
| 02 | G3000 - ArrivalENTER STAR AND APPROACHNOTE: Activate STAR in the G3000 flight plan. Load expected approach procedure. Confirm IAF, approach minimums, and missed approach. | |
| 03 | AltimeterSET DESTINATION QNHNOTE: Set altimeter to destination QNH when below transition altitude. | |
| 04 | Descent Speed175-200 KIAS TYPICALNOTE: Typical descent speed 175-200 KIAS. Do not exceed Vmo 266 KIAS. | |
| 05 | Power LeverREDUCE FOR DESCENTNOTE: Reduce power to achieve desired descent rate (500-1,000 fpm). Avoid prolonged flight at very low power - ITT should stay above 500 deg C to maintain engine efficiency. | |
| 06 | ITT During DescentMONITOR - MAINTAIN ABOVE 500 DEG CCAUTION: Avoid reducing ITT too low during descent. Set power so ITT remains above 500 deg C to keep engine warm and avoid thermal shock on power addition. | |
| 07 | PressurizationCHECK - CABIN DESCENDINGNOTE: Verify cabin altitude is descending toward destination elevation. Check descent rate is comfortable for passengers. | |
| 08 | Prop RPMADVANCE TO 1,900 RPMNOTE: Advance prop RPM toward takeoff setting during descent in preparation for approach. | |
| 09 | FuelCHECK QUANTITYNOTE: Verify fuel remaining vs required. Confirm sufficient for approach, missed approach, and alternate if required. | |
| 10 | Seatbelt SignON - NOTIFY PASSENGERS | |
| 11 | Ice ProtectionAS REQUIREDNOTE: Monitor for icing during descent. Engage FIKI as required. Be aware that icing may be more prevalent at lower altitudes in certain weather conditions. |
PHS 11 — Before Landing12 steps
| 01 | Approach BriefingCOMPLETENOTE: Brief approach type, DA/MDA, MAP, missed approach procedure, expected runway, taxi route, and engine failure plan. | |
| 02 | AltimeterSET QNH - CROSS-CHECK STANDBY | |
| 03 | Autopilot Approach ModeCOUPLE TO APPROACH (if flying coupled)NOTE: For ILS approach, verify G3000 is in APR mode and LOC/GS are captured. Monitor flight director deviation. | |
| 04 | Condition LeverHIGH IDLE - CONFIRM | |
| 05 | Prop RPMFULL FORWARD (2,000 RPM)NOTE: Advance prop lever to full forward for maximum RPM available for go-around. Do this before entering the approach sequence. | |
| 06 | Landing GearDOWN - 3 GREENNOTE: Extend gear at or below 178 KIAS. Verify 3 green gear-down lights illuminate. | |
| 07 | Gear - Down and Locked3 GREEN LIGHTS CONFIRMEDCAUTION: Verify all three gear lights show green. If any light fails to illuminate, execute missed approach and follow abnormal gear procedure. | |
| 08 | FlapsLDG (Landing Position)NOTE: Select LDG flaps at or below 122 KIAS. Verify on flap position indicator. | |
| 09 | Landing Speed VrefCHECK - APPROX 88-95 KIAS (weight dep.)NOTE: Vref at typical landing weight approximately 88-95 KIAS. Add gust additive of half steady wind plus full gust increment. | |
| 10 | Landing LightON | |
| 11 | Strobe LightsON | |
| 12 | SeatbeltsFASTENED - VERIFY ALL |
PHS 12 — Landing10 steps
| 01 | Pattern Altitude1,000 FT AGLNOTE: Join circuit at 1,000 ft AGL. Downwind at 110-120 KIAS. | |
| 02 | Speed - Downwind110-120 KIAS | |
| 03 | Speed - Base Leg100-110 KIAS | |
| 04 | Final Approach SpeedVREF + GUST ADDITIVENOTE: Stabilized approach at Vref + wind additive from 500 ft AGL to touchdown. Typical final speed 90-100 KIAS. | |
| 05 | Approach - Stable by 500 ft AGLSPEED, SINK RATE, ALIGNMENT CONFIRMEDCAUTION: If approach is not stable by 500 ft AGL (IMC) or 300 ft AGL (VMC), execute go-around. Do not attempt to salvage an unstable approach. | |
| 06 | PowerAS REQUIRED FOR GLIDEPATHNOTE: The TBM 930 is relatively clean. Maintain some power on approach. Do not chop to idle on final. Anticipate long float if excess energy is carried across threshold. | |
| 07 | FlareGENTLE AT 20-30 FT AGL - REDUCE POWERNOTE: Begin flare at 20-30 ft AGL. Smoothly reduce power to idle. Aim for main gear touchdown. | |
| 08 | TouchdownMAIN GEAR FIRST - ON CENTERLINENOTE: Let mains touch first, then ease nosewheel down gently. Avoid hard nosewheel arrivals which stress the nose gear. | |
| 09 | BrakesAPPLY FIRMLY AFTER WEIGHT ON MAINSNOTE: Apply steady firm brake pressure after weight settles on main gear. Avoid locking brakes. Antiskid protects against wheel lockup. | |
| 10 | Propeller BetaAS AVAILABLE - POWER BACKNOTE: On short runways, reverse pitch (beta) may be used to assist deceleration. Avoid aggressive beta below 60 kts to prevent propeller blade issues. |
PHS 13 — After Landing9 steps
| 01 | Power LeverIDLE - CONFIRM AFTER RUNWAY CLEARNOTE: Do not adjust anything until the aircraft is clear of the active runway. | |
| 02 | FlapsUP (RETRACT)NOTE: Retract flaps to UP after clearing runway. | |
| 03 | Landing GearVERIFY DOWN - 3 GREENNOTE: Confirm gear down indication again after landing as a habit check. | |
| 04 | LightsLANDING LIGHT OFF - TAXI LIGHT ON | |
| 05 | Strobe LightsOFF | |
| 06 | TransponderSTBY (or as instructed) | |
| 07 | Condition LeverHIGH IDLE FOR TAXINOTE: Maintain HIGH IDLE for taxi. Engine needs time to cool before shutdown - do not reduce to CUTOFF while hot. | |
| 08 | Ice ProtectionAS REQUIRED for ground conditions | |
| 09 | Taxi ClearanceRECEIVE - CONTACT GROUND |
PHS 14 — Shutdown / Securing20 steps
| 01 | Parking BrakeSET | |
| 02 | LightsOFF (except Beacon and Nav Lights)NOTE: Turn off landing light, strobes, and taxi light. Keep beacon on while engine is running. | |
| 03 | Avionics MasterOFF (before cutting generator)NOTE: Turn off avionics master to protect avionics from voltage transients during shutdown. Do this before condition lever to CUTOFF. | |
| 04 | Ice ProtectionOFF | |
| 05 | Pitot HeatOFF | |
| 06 | Engine CoolingIDLE 2 MINUTES MINIMUMCAUTION: Never shut down the PT6A-66D immediately after high-power operations. Thermal shock to the turbine section can cause premature failure and costly repairs.NOTE: Allow engine to cool at ground idle for a minimum of 2 minutes (ideally 5 minutes) after high-power flight. This prevents hot-section damage from heat soak. | |
| 07 | Condition LeverFUEL CUTOFF (Full Aft)NOTE: Move condition lever to CUTOFF to shut down engine. Do not use any other method to stop the engine. | |
| 08 | Ng / ITTMONITOR - WATCH WIND-DOWNNOTE: Monitor Ng and ITT as engine winds down. ITT will typically peak briefly on cutoff before declining. | |
| 09 | PropellerOBSERVE - FULL STOP BEFORE APPROACHINGCAUTION: Never approach the propeller arc until the prop has come to a complete stop. Turbine engines can restart unexpectedly if fuel is present. | |
| 10 | GeneratorOFF (when N1 below 15%)NOTE: Turn generator off once Ng has wound down below 15% to prevent electrical anomalies. | |
| 11 | Battery SwitchesOFFNOTE: Turn off both battery switches. Verify all electrical loads are off first. | |
| 12 | Beacon LightOFF (after prop stops) | |
| 13 | Navigation LightsOFF | |
| 14 | Fuel SelectorOFF (if long-term parking) | |
| 15 | Chocks and Tie-DownSET AS REQUIREDNOTE: Install wheel chocks. If overnight or prolonged parking, tie down aircraft per local procedures. | |
| 16 | Flight Log / Journey LogUPDATENOTE: Record flight time, landings, and any discrepancies in the aircraft log or journey log. | |
| 17 | SecuringCOMPLETE - PITOT COVER, INTAKE PLUGNOTE: Install pitot tube cover, engine intake covers if available, and aircraft cover if stored outside. | |
| 18 | Cabin DoorsCLOSED AND LOCKEDNOTE: Secure both cabin door and baggage door. Set lock if leaving aircraft unattended. | |
| 19 | External InspectionWALK-AROUND COMPLETENOTE: Perform post-flight walk-around to check for any leaks, damage, or bird strike evidence. | |
| 20 | GSX - Ground ServicesAS REQUIREDNOTE: GSX menu: Request fuel truck or ground power if returning to base. |