Daher TBM 930MSFS 2024 Startup Checklist · 183 steps
Daher TBM 930
MSFS 2024 - 0/183 STEPS
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AIRCRAFT BRIEF
The Daher TBM 930 is a single-engine pressurized turboprop that represents the pinnacle of the TBM family. First delivered in 2016, it upgraded the TBM 900 with the Garmin G3000 touchscreen avionics suite, an autothrottle system, and full FIKI (Flight Into Known Icing) certification as standard. Built in Tarbes, France, the TBM series is renowned for combining near-jet speeds (330 kts TAS) with turboprop economics, making it the world's fastest single-engine turboprop.
RANGE VISUALIZER
SPECIFICATIONS
manufacturerDaher (formerly SOCATA)
first Flight2016 (TBM 930)
rolePressurized single-engine turboprop / Executive transport
crew1-2 pilots + up to 5 passengers
engines1x Pratt and Whitney Canada PT6A-66D (850 shp)
max Speed611 km/h (330 kts TAS)
range3,519 km (1,900 nmi)
ceiling31,000 ft
weight3,354 kg (MTOW)
PHS 1 — Pre-Flight Planning8 steps
| 01 | Weather Briefing (METAR / TAF)NOTE: 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. | REVIEWED | |
| 02 | NOTAMsNOTE: Check for runway closures, TFRs, airspace restrictions. Note any SIGMET for turbulence or icing on route. | REVIEWED | |
| 03 | Fuel RequiredNOTE: 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. | CALCULATED | |
| 04 | Weight and BalanceCAUTION: 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. | WITHIN LIMITS | |
| 05 | Takeoff and Landing DistancesNOTE: Sea level MTOW takeoff roll approximately 2,500 ft. Landing roll approximately 2,400 ft. Adjust for density altitude, runway slope, and surface condition. | CALCULATED | |
| 06 | V-Speeds CalculatedNOTE: Note Vr, Vy, Vx, and Vref for actual takeoff and landing weights. Garmin G3000 avionics will display computed speeds when weight is entered. | NOTED | |
| 07 | G3000 Flight PlanNOTE: Prepare route for entry into the Garmin G3000 touchscreen avionics. Load SID, enroute waypoints, STAR, and approach. | PLANNED | |
| 08 | Flight Plan | FILED |
PHS 2 — Before Start25 steps
| 01 | Parking Brake | SET | |
| 02 | Battery 1 and Battery 2 SwitchesNOTE: Both batteries on. Avionics will begin to power up. Verify voltages on the electrical synoptic. | ON | |
| 03 | External PowerNOTE: Use GPU to conserve battery during avionics initialization on extended ground operations. | CONNECT (if available) | |
| 04 | Avionics - G3000NOTE: Allow G3000 displays to fully boot. MFD and PFDs require 60-90 seconds to initialize databases. | INITIALIZING | |
| 05 | G3000 - Aircraft ConfigurationNOTE: Enter actual ZFW on the G3000 MFD to enable computed V-speeds and performance data. | CONFIRM WEIGHT ENTERED | |
| 06 | Flight Plan - G3000NOTE: Load route on G3000 FPL page. Verify departure, SID, route, STAR, and approach. Confirm correct runway and transition. | ENTERED AND VERIFIED | |
| 07 | Fuel QuantityNOTE: Usable fuel 282 USG (1,880 lbs). Verify quantity on fuel synoptic page. Cross-check with physical sight gauges. | CHECK - SUFFICIENT | |
| 08 | Fuel SelectorNOTE: Verify fuel selector is in the ON/MAIN position, not OFF. | ON (MAIN TANKS) | |
| 09 | Condition LeverNOTE: Condition lever must be in FUEL CUTOFF before starter engagement. | FUEL CUTOFF (Full Aft) | |
| 10 | Power Lever (Throttle)NOTE: Power lever at idle stop before start. | GROUND IDLE (Idle Detent) | |
| 11 | Generator SwitchNOTE: Generator switch ON. It will come online after engine reaches self-sustaining speed. | ON | |
| 12 | Ice Protection SwitchesNOTE: All FIKI switches verify OFF for start. Plan anti-ice use based on weather briefing. | OFF - CHECK CONDITIONS | |
| 13 | Pitot / Static HeatNOTE: Pitot and static heating should be ON prior to flight in any IMC conditions. Leave on for all flights as standard practice. | ON | |
| 14 | Circuit BreakersNOTE: Verify all circuit breakers are set. Check panel for any popped breakers. | CHECK IN | |
| 15 | Flight ControlsNOTE: Verify full deflection of ailerons, elevator, and rudder. Confirm correct sense of movement against stick inputs on G3000 controls page. | FREE AND CORRECT | |
| 16 | Elevator TrimNOTE: Set elevator trim to appropriate takeoff position per weight and balance. Typically 3-5 units nose-up. | SET FOR TAKEOFF (5 deg nose up typical) | |
| 17 | Rudder Trim | NEUTRAL | |
| 18 | FlapsNOTE: Set flaps to TO detent for normal takeoff. Verify on flap position indicator. | TO (Takeoff position) | |
| 19 | Pressurization - Cabin AltitudeNOTE: Set destination field elevation on pressurization controller. Verify AUTO mode selected. | SET DESTINATION ELEVATION | |
| 20 | Oxygen SystemNOTE: Crew oxygen pressure check. TBM 930 is pressurized to FL310 but carry oxygen per regulations. | CHECK - PRESSURE ADEQUATE | |
| 21 | Passenger BriefingNOTE: Brief passengers on seatbelts, emergency exits, no smoking, pressurization, and sterile cockpit during critical phases. | COMPLETE | |
| 22 | Doors and BaggageCAUTION: 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. | CLOSED AND LOCKED | |
| 23 | Seatbelts | FASTENED - PILOT AND PASSENGERS | |
| 24 | Beacon LightNOTE: Turn on rotating beacon to signal imminent engine start to ground personnel. | ON | |
| 25 | GSX - Fuel TruckNOTE: GSX menu: Refuel Aircraft. Set desired fuel load before confirming. | REFUEL COMPLETE |
PHS 3 — Engine Start11 steps
| 01 | Propeller AreaCAUTION: Confirm no persons or objects within propeller arc before engaging starter. Call CLEAR PROP. | CLEAR - VERIFY | |
| 02 | Ignition SwitchNOTE: Set ignition to AUTO for normal start. Ignitors will fire automatically when fuel is introduced. | AUTO | |
| 03 | Starter SwitchNOTE: Engage starter. Monitor Ng (gas generator speed) winding up toward 13% before introducing fuel. | ENGAGE (Hold) | |
| 04 | Ng RisingNOTE: Watch Ng climb. PT6A-66D starter will crank the gas generator. Normal motoring time 5-10 seconds before fuel introduction. | MONITOR - INCREASING | |
| 05 | Condition LeverCAUTION: 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. | LOW IDLE (at 13% Ng) | |
| 06 | ITT - Monitor RiseWARNING: 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. | RISING - WATCH CAREFULLY | |
| 07 | Starter - ReleaseNOTE: Release starter at 50% Ng or when engine is clearly self-sustaining. Starter is rated for maximum 30-second cranking. | RELEASE at 50% Ng | |
| 08 | Ng - Idle StabilizationNOTE: Engine stabilizes at ground idle. Allow 30-60 seconds for parameters to settle before checking gauges. | STABILIZE ~68-72% GROUND IDLE | |
| 09 | Oil PressureWARNING: If oil pressure does not rise within 30 seconds of fuel introduction, immediately return condition lever to CUTOFF and investigate before attempting another start. | IN GREEN (within 30 seconds) | |
| 10 | ITT at IdleNOTE: Ground idle ITT typically 600-700 deg C. Max continuous ITT is 770 deg C. | WITHIN LIMITS (600-700 deg C typical) | |
| 11 | Oil TemperatureNOTE: Oil temperature should begin rising from ambient toward normal operating range of 10-104 deg C. | RISING - NORMAL |
PHS 4 — After Start13 steps
| 01 | Generator - OnlineNOTE: Verify generator came online and is charging. Check bus voltage on electrical synoptic page. Should read 28V DC. | CHECK CHARGING | |
| 02 | External Power | DISCONNECT (if used) | |
| 03 | Avionics - G3000NOTE: Verify all G3000 displays are fully initialized. PFD attitude, airspeed, altitude should all be valid. MFD showing map and engine data. | FULLY INITIALIZED - CHECK | |
| 04 | AHRS / ADCNOTE: Attitude Heading Reference System and Air Data Computer should show valid data. Cross-check PFD attitude with standby attitude indicator. | ALIGNED AND VALID | |
| 05 | Flight Plan - Verify ActiveNOTE: Verify correct route is active on G3000. Confirm first waypoint, SID, and destination are loaded correctly. | CONFIRM ROUTE ACTIVE | |
| 06 | Altimeter (PFD)NOTE: Set altimeter to current QNH from ATIS. Verify altitude reading matches field elevation. | SET QNH | |
| 07 | Standby AltimeterNOTE: Set standby altimeter to same QNH. Cross-check with PFD. | SET QNH | |
| 08 | Heading IndicatorNOTE: Verify HSI/heading on PFD agrees with magnetic standby compass. | ALIGNED TO MAGNETIC COMPASS | |
| 09 | TransponderNOTE: Enter ATC squawk code and set transponder to STBY until cleared for taxi. | SET SQUAWK CODE - STBY | |
| 10 | Radios - COM1 / COM2 | SET ATIS AND GROUND FREQUENCIES | |
| 11 | ATISNOTE: Note altimeter setting, winds, runway in use, and NOTAM info from ATIS. Confirm matches pre-flight weather. | RECEIVED AND NOTED | |
| 12 | Condition LeverNOTE: 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. | HIGH IDLE (after engine warm) | |
| 13 | Engine Parameters - Cross-CheckNOTE: 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. | ALL WITHIN LIMITS |
PHS 5 — Taxi10 steps
| 01 | Clearance DeliveryNOTE: Contact clearance delivery with aircraft type, departure airport, destination, requested altitude, and squawk. Read back clearance. | DEPARTURE CLEARANCE RECEIVED | |
| 02 | Taxi Light | ON | |
| 03 | Navigation Lights | ON | |
| 04 | Parking Brake | RELEASE | |
| 05 | BrakesNOTE: Apply brakes gently as aircraft begins to roll to verify proper function before increasing taxi speed. | CHECK - during first movement | |
| 06 | PowerNOTE: The PT6A-66D responds well to power inputs. Use modest power to achieve walking pace taxi speed. | ADVANCE SMOOTHLY - TAXI POWER | |
| 07 | Taxi SpeedNOTE: Maintain walking pace appropriate to ramp conditions. Reduce speed before turns. | WALKING PACE | |
| 08 | Flight InstrumentsNOTE: Verify attitude indicator stays level, compass and HSI track heading changes during taxi turns. | CHECK DURING TURNS | |
| 09 | Nosewheel SteeringNOTE: Verify nosewheel steering response is normal. TBM 930 uses differential braking plus rudder pedal steering. | RESPONSIVE ON TURNS | |
| 10 | TransponderNOTE: Many airports now require transponder ON (or ALT) while moving on surface. | ALT (as required by local procedures) |
PHS 6 — Before Takeoff20 steps
| 01 | Parking Brake | SET (run-up position) | |
| 02 | Condition Lever | HIGH IDLE - CONFIRM | |
| 03 | Power LeverNOTE: Advance to approximately 1,000 ft-lbs torque or per POH run-up power. Verify ITT within limits during power increase. | ADVANCE TO 1,000 FT-LBS TORQUE for run-up | |
| 04 | Ignition CheckNOTE: Select LEFT then RIGHT ignition individually. Brief ITT rise is normal. Verify ITT and Ng remain stable. | CHECK BOTH - VERIFY NO EXCESSIVE ITT RISE | |
| 05 | Prop CycleNOTE: Cycle prop governor to circulate warm oil. RPM should reduce then return to governed RPM when lever advanced. | CYCLE - pull prop lever to MIN RPM then return | |
| 06 | Torque / ITT / NgNOTE: Verify torque, ITT, and Ng are within limits at run-up power before reducing to idle. | CHECK - WITHIN LIMITS | |
| 07 | Power Lever | REDUCE TO IDLE after run-up | |
| 08 | Flight Controls | FREE AND CORRECT - FULL TRAVEL | |
| 09 | Elevator Trim | CONFIRM TAKEOFF SETTING | |
| 10 | Flaps | TO (Takeoff) - CONFIRM | |
| 11 | Pressurization ModeNOTE: Confirm pressurization is in AUTO mode and destination elevation is set. | AUTO - DESTINATION SET | |
| 12 | Ice ProtectionNOTE: If icing conditions exist at or after departure, arm engine inlet, windshield, and prop FIKI prior to takeoff. | AS REQUIRED - FIKI ON if icing conditions | |
| 13 | Fuel QuantityNOTE: Final fuel check. Verify quantity against flight plan fuel requirement. | VERIFY SUFFICIENT | |
| 14 | Autopilot / Flight DirectorNOTE: Pre-select autopilot modes if desired (heading, altitude). Autopilot should not be engaged for takeoff. | VERIFY MODES SET | |
| 15 | Transponder | ALT (Mode C) | |
| 16 | Lights | STROBE ON, LANDING LIGHT ON | |
| 17 | Doors and Windows | CLOSED AND LOCKED - CONFIRM | |
| 18 | Seatbelts | FASTENED - ALL ABOARD | |
| 19 | Departure BriefingNOTE: Brief departure procedure, initial altitude, engine failure action (land straight ahead below Vr, return if above Vr with altitude), abort criteria. | COMPLETE | |
| 20 | ATC ClearanceNOTE: Contact tower for takeoff clearance. Read back runway, any crossing restrictions, and initial altitude restriction. | RECEIVED |
PHS 7 — Takeoff9 steps
| 01 | Runway AlignmentNOTE: Cross-check runway heading with HSI/PFD magnetic heading. Confirm runway number visible. | CONFIRM ASSIGNED RUNWAY | |
| 02 | Power LeverNOTE: Smoothly advance power lever to maximum takeoff torque (2,000 ft-lbs). Avoid abrupt power application which can cause propeller overspeed or ITT spike. | ADVANCE SMOOTHLY TO MAX TORQUE | |
| 03 | Torque and ITTWARNING: Do not exceed 2,000 ft-lbs torque or 850 deg C ITT during takeoff roll. Reduce power immediately if limits are approached. | MONITOR - MAX 2,000 FT-LBS / 850 DEG C | |
| 04 | Prop RPMNOTE: Prop governor should maintain 2,000 RPM throughout takeoff roll at full power. | CHECK 2,000 RPM (governed) | |
| 05 | RudderNOTE: PT6A torque effect and P-factor require right rudder on the roll. Apply progressively as power is added. | RIGHT RUDDER - MAINTAIN CENTERLINE | |
| 06 | Rotation Speed (Vr)NOTE: 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. | 113 KIAS (typical) - ROTATE | |
| 07 | Positive Rate of ClimbNOTE: Once VSI shows positive climb, call POSITIVE RATE and raise gear. | CONFIRM - GEAR UP | |
| 08 | Landing GearCAUTION: Raise gear only after positive rate confirmed. Verify gear lights transition from green to out (gear up and locked). | UP - 3 LIGHTS TRANSIT THEN OFF | |
| 09 | FlapsNOTE: Retract flaps once clear of obstacles and above 400 ft AGL. Do not retract below 200 ft AGL. | RETRACT ABOVE 400 FT AGL |
PHS 8 — Climb13 steps
| 01 | Climb SpeedNOTE: 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. | 124 KIAS (Vy) OR AS DESIRED | |
| 02 | PowerNOTE: Maximum continuous torque for climb. Reduce power as required to keep ITT within continuous limits. | MAX CONTINUOUS (2,000 FT-LBS / 850 DEG C MAX) | |
| 03 | Condition Lever | HIGH IDLE - VERIFY | |
| 04 | Prop RPM | 2,000 RPM (governed) | |
| 05 | Flaps | UP - VERIFY RETRACTED | |
| 06 | Gear | UP - VERIFY (3 LIGHTS OUT) | |
| 07 | AutopilotNOTE: Engage autopilot after initial climb established. Select NAV mode for lateral guidance, VS or FLC for vertical. | ENGAGE (if desired above 400 ft AGL) | |
| 08 | PressurizationNOTE: Verify cabin altitude is climbing at 300-500 fpm toward cruise cabin altitude. Check differential pressure is normal. | CHECK - CABIN CLIMBING NORMALLY | |
| 09 | AltimeterNOTE: Set standard pressure at transition altitude (18,000 ft in US). Coordinate with ATC. | SET 29.92 AT TRANSITION ALTITUDE | |
| 10 | Landing Light | OFF ABOVE 10,000 FT (optional) | |
| 11 | Engine GaugesNOTE: Monitor ITT, torque, Ng, oil temp, and oil pressure regularly during climb. | MONITOR EVERY 5 MINUTES | |
| 12 | Ice ProtectionNOTE: Engage engine inlet anti-ice when OAT is below +5 deg C in visible moisture. Prop and windshield FIKI as needed. | ACTIVATE AS REQUIRED | |
| 13 | 10,000 ft CheckNOTE: At 10,000 ft: review engine instruments, check fuel, brief passengers if seatbelt sign changes. | LANDING LIGHT AND SEATBELT SIGN AS REQUIRED |
PHS 9 — Cruise12 steps
| 01 | Cruise AltitudeNOTE: Typical cruise altitudes FL250-FL310 (max FL310). Set altitude bug, autopilot captures altitude. | LEVEL OFF - VERIFY ON ALTITUDE | |
| 02 | Power LeverNOTE: 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. | REDUCE TO CRUISE TORQUE | |
| 03 | Prop RPMNOTE: Reduce prop RPM from 2,000 to 1,700-1,800 RPM for cruise efficiency and reduced cabin noise. | REDUCE TO CRUISE RPM (1,700-1,800 RPM) | |
| 04 | ITTNOTE: Typical cruise ITT 650-720 deg C. Adjust power lever as needed to stay within limits. | MONITOR - MAX 770 DEG C CONTINUOUS | |
| 05 | Altimeter | 29.92 IN HG - VERIFY (above transition) | |
| 06 | PressurizationNOTE: Verify cabin altitude is stable at cruise differential. Max differential is 6.0 PSI, providing sea-level equivalent cabin to approximately FL270. | CHECK - CABIN ALTITUDE STABLE | |
| 07 | Fuel QuantityNOTE: Check fuel burn rate vs plan. Typical cruise burn 45-55 USG/hr at FL280. Verify sufficient fuel to destination plus reserves. | CHECK - BURN RATE CONSISTENT | |
| 08 | RadiosNOTE: Monitor ATC frequency. Keep ATIS or ASOS for destination on COM2. | SET ENROUTE FREQUENCIES | |
| 09 | Transponder | ALT - VERIFY SQUAWK CORRECT | |
| 10 | NavigationNOTE: Verify G3000 is tracking correctly. Monitor fuel burn to ETA. Note any alternate diversion if needed. | CHECK GPS COURSE, WAYPOINTS, ETA | |
| 11 | Ice ProtectionNOTE: Monitor for icing. FIKI system provides full ice protection. Engine anti-ice ON below +5 deg C in visible moisture. | AS REQUIRED FOR CONDITIONS | |
| 12 | Top of DescentNOTE: Use 3:1 ratio (3 nmi per 1,000 ft). From FL310 begin descent approximately 93 nmi from destination. | CALCULATE |
PHS 10 — Descent11 steps
| 01 | ATIS / Destination WeatherNOTE: Get destination ATIS at top of descent. Note altimeter setting, winds, runway in use, and any special conditions. | OBTAIN | |
| 02 | G3000 - ArrivalNOTE: Activate STAR in the G3000 flight plan. Load expected approach procedure. Confirm IAF, approach minimums, and missed approach. | ENTER STAR AND APPROACH | |
| 03 | AltimeterNOTE: Set altimeter to destination QNH when below transition altitude. | SET DESTINATION QNH | |
| 04 | Descent SpeedNOTE: Typical descent speed 175-200 KIAS. Do not exceed Vmo 266 KIAS. | 175-200 KIAS TYPICAL | |
| 05 | Power LeverNOTE: 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. | REDUCE FOR DESCENT | |
| 06 | ITT During DescentCAUTION: 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. | MONITOR - MAINTAIN ABOVE 500 DEG C | |
| 07 | PressurizationNOTE: Verify cabin altitude is descending toward destination elevation. Check descent rate is comfortable for passengers. | CHECK - CABIN DESCENDING | |
| 08 | Prop RPMNOTE: Advance prop RPM toward takeoff setting during descent in preparation for approach. | ADVANCE TO 1,900 RPM | |
| 09 | FuelNOTE: Verify fuel remaining vs required. Confirm sufficient for approach, missed approach, and alternate if required. | CHECK QUANTITY | |
| 10 | Seatbelt Sign | ON - NOTIFY PASSENGERS | |
| 11 | Ice ProtectionNOTE: Monitor for icing during descent. Engage FIKI as required. Be aware that icing may be more prevalent at lower altitudes in certain weather conditions. | AS REQUIRED |
PHS 11 — Before Landing12 steps
| 01 | Approach BriefingNOTE: Brief approach type, DA/MDA, MAP, missed approach procedure, expected runway, taxi route, and engine failure plan. | COMPLETE | |
| 02 | Altimeter | SET QNH - CROSS-CHECK STANDBY | |
| 03 | Autopilot Approach ModeNOTE: For ILS approach, verify G3000 is in APR mode and LOC/GS are captured. Monitor flight director deviation. | COUPLE TO APPROACH (if flying coupled) | |
| 04 | Condition Lever | HIGH IDLE - CONFIRM | |
| 05 | Prop RPMNOTE: Advance prop lever to full forward for maximum RPM available for go-around. Do this before entering the approach sequence. | FULL FORWARD (2,000 RPM) | |
| 06 | Landing GearNOTE: Extend gear at or below 178 KIAS. Verify 3 green gear-down lights illuminate. | DOWN - 3 GREEN | |
| 07 | Gear - Down and LockedCAUTION: Verify all three gear lights show green. If any light fails to illuminate, execute missed approach and follow abnormal gear procedure. | 3 GREEN LIGHTS CONFIRMED | |
| 08 | FlapsNOTE: Select LDG flaps at or below 122 KIAS. Verify on flap position indicator. | LDG (Landing Position) | |
| 09 | Landing Speed VrefNOTE: Vref at typical landing weight approximately 88-95 KIAS. Add gust additive of half steady wind plus full gust increment. | CHECK - APPROX 88-95 KIAS (weight dep.) | |
| 10 | Landing Light | ON | |
| 11 | Strobe Lights | ON | |
| 12 | Seatbelts | FASTENED - VERIFY ALL |
PHS 12 — Landing10 steps
| 01 | Pattern AltitudeNOTE: Join circuit at 1,000 ft AGL. Downwind at 110-120 KIAS. | 1,000 FT AGL | |
| 02 | Speed - Downwind | 110-120 KIAS | |
| 03 | Speed - Base Leg | 100-110 KIAS | |
| 04 | Final Approach SpeedNOTE: Stabilized approach at Vref + wind additive from 500 ft AGL to touchdown. Typical final speed 90-100 KIAS. | VREF + GUST ADDITIVE | |
| 05 | Approach - Stable by 500 ft AGLCAUTION: 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. | SPEED, SINK RATE, ALIGNMENT CONFIRMED | |
| 06 | PowerNOTE: 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. | AS REQUIRED FOR GLIDEPATH | |
| 07 | FlareNOTE: Begin flare at 20-30 ft AGL. Smoothly reduce power to idle. Aim for main gear touchdown. | GENTLE AT 20-30 FT AGL - REDUCE POWER | |
| 08 | TouchdownNOTE: Let mains touch first, then ease nosewheel down gently. Avoid hard nosewheel arrivals which stress the nose gear. | MAIN GEAR FIRST - ON CENTERLINE | |
| 09 | BrakesNOTE: Apply steady firm brake pressure after weight settles on main gear. Avoid locking brakes. Antiskid protects against wheel lockup. | APPLY FIRMLY AFTER WEIGHT ON MAINS | |
| 10 | Propeller BetaNOTE: On short runways, reverse pitch (beta) may be used to assist deceleration. Avoid aggressive beta below 60 kts to prevent propeller blade issues. | AS AVAILABLE - POWER BACK |
PHS 13 — After Landing9 steps
| 01 | Power LeverNOTE: Do not adjust anything until the aircraft is clear of the active runway. | IDLE - CONFIRM AFTER RUNWAY CLEAR | |
| 02 | FlapsNOTE: Retract flaps to UP after clearing runway. | UP (RETRACT) | |
| 03 | Landing GearNOTE: Confirm gear down indication again after landing as a habit check. | VERIFY DOWN - 3 GREEN | |
| 04 | Lights | LANDING LIGHT OFF - TAXI LIGHT ON | |
| 05 | Strobe Lights | OFF | |
| 06 | Transponder | STBY (or as instructed) | |
| 07 | Condition LeverNOTE: Maintain HIGH IDLE for taxi. Engine needs time to cool before shutdown - do not reduce to CUTOFF while hot. | HIGH IDLE FOR TAXI | |
| 08 | Ice Protection | AS REQUIRED for ground conditions | |
| 09 | Taxi Clearance | RECEIVE - CONTACT GROUND |
PHS 14 — Shutdown / Securing20 steps
| 01 | Parking Brake | SET | |
| 02 | LightsNOTE: Turn off landing light, strobes, and taxi light. Keep beacon on while engine is running. | OFF (except Beacon and Nav Lights) | |
| 03 | Avionics MasterNOTE: Turn off avionics master to protect avionics from voltage transients during shutdown. Do this before condition lever to CUTOFF. | OFF (before cutting generator) | |
| 04 | Ice Protection | OFF | |
| 05 | Pitot Heat | OFF | |
| 06 | Engine CoolingCAUTION: 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. | IDLE 2 MINUTES MINIMUM | |
| 07 | Condition LeverNOTE: Move condition lever to CUTOFF to shut down engine. Do not use any other method to stop the engine. | FUEL CUTOFF (Full Aft) | |
| 08 | Ng / ITTNOTE: Monitor Ng and ITT as engine winds down. ITT will typically peak briefly on cutoff before declining. | MONITOR - WATCH WIND-DOWN | |
| 09 | PropellerCAUTION: Never approach the propeller arc until the prop has come to a complete stop. Turbine engines can restart unexpectedly if fuel is present. | OBSERVE - FULL STOP BEFORE APPROACHING | |
| 10 | GeneratorNOTE: Turn generator off once Ng has wound down below 15% to prevent electrical anomalies. | OFF (when N1 below 15%) | |
| 11 | Battery SwitchesNOTE: Turn off both battery switches. Verify all electrical loads are off first. | OFF | |
| 12 | Beacon Light | OFF (after prop stops) | |
| 13 | Navigation Lights | OFF | |
| 14 | Fuel Selector | OFF (if long-term parking) | |
| 15 | Chocks and Tie-DownNOTE: Install wheel chocks. If overnight or prolonged parking, tie down aircraft per local procedures. | SET AS REQUIRED | |
| 16 | Flight Log / Journey LogNOTE: Record flight time, landings, and any discrepancies in the aircraft log or journey log. | UPDATE | |
| 17 | SecuringNOTE: Install pitot tube cover, engine intake covers if available, and aircraft cover if stored outside. | COMPLETE - PITOT COVER, INTAKE PLUG | |
| 18 | Cabin DoorsNOTE: Secure both cabin door and baggage door. Set lock if leaving aircraft unattended. | CLOSED AND LOCKED | |
| 19 | External InspectionNOTE: Perform post-flight walk-around to check for any leaks, damage, or bird strike evidence. | WALK-AROUND COMPLETE | |
| 20 | GSX - Ground ServicesNOTE: GSX menu: Request fuel truck or ground power if returning to base. | AS REQUIRED |