cessna t206h differences general: engine – lycoming tio-540-aj1a 310 hp @ 2500 rpm/39”mp, mcp...

Cessna T206H DifferencesGeneral:Engine – Lycoming TIO-540-AJ1A310 HP @ 2500 rpm/39”mp, MCPTach -- 2000-2400 rpm, T/O 2500 rpmMP -- 15-39”CHT -- 200°-480° FTIT -- 1350°-1675°Oil: 11 qt. max, 6 qt. min.Oil Tmp -- 100°-245° FOil Pressure -- 50-90 lb.Fuel Flow -- 5-20 gph, T/O 34 gphFuel -- 100LL – 122.0 gal total

117.8 gal usableMain tanks 88 gal usableTip tanks 29.8 gal usable

Vacuum – 4.5 - 5.5 in.hg.Propeller – McCauley 3 Blade, 79 in.Weight: Takeoff – 3800 lb

Landing – 3600 lb Baggage – 180 lb

Wing Span – 39 ftLength – 28’ 3”Height – 9’ 3 ½ “Wing Area – 185 sq. f.tWing Loading – 20.5 lb sq. ft.Power Loading – 12.3 lb. hp.Min turning radius – 27’ 9”

Cessna T206H DifferencesV-speeds & Limitations: Vne -- 182 kts Vno -- 149 kts Va -- 125 kts @ 3800 lb 125 kts @ 3600 lb 120 kts @ 2950 lb 106 kts @ 2300 lb Vs -- 59 kts Vso -- 47 kts Vfe -- 140-100/10°, < 100 /10°- 40° Vy -- 89 kts Vx -- 69-72 kts

Load Factor Limits Flaps up +3.8g, -1.52g Flaps dn +2.0g Best Glide 80 kias @ 3800 lb 80 kias @ 3600 lb 75 “ @ 3200 lb 70 “ @ 2800 lb

Cessna T206H DifferencesAirspeeds:LIFT NOSE WHEEL (slightly) AT 55 KIASShort Fld T/O- Flaps 20°, lof 64, 74 kts @ 50’Climbout – 75-85, Cruise Climb – 95-105 (110 -115)

Landing – Flaps Up – 80-90 kts Flaps 40° – 70-80 kts

Short Fld – Flaps 40°- 67 ktsDemonstrated Crosswind – 20 kts

Performance: (30°c)Takeoff @ 5000’ – 1547’ gnd roll, 2817’ to 50’ obstLanding @ 5000’ – 930 gnd roll, 1675 ovr 50’ obstRoC @ 5000’ – 770 fpmCeiling – 27,000’Range @ 75% /8000’ – 350 nm (64 gal)

– 2.4 hr (64 gal)

Cessna T206H Differences

POWERPLANT / LIMITATIONSEngine Manufacturer: Textron LycomingEngine Model Number: TIO-540-AJ1AMaximum Power: 310 BHP ratingEngine Operating Limits for Takeoff and Continuous Operations:Maximum Continuous Power: . . . . . . . . . . . . . . . . . . 310 rated BHPat 39 in.hg. and 2500 RPMMaximum Cylinder Head Temperature: . . . . . . . . . . . 480°F (249°C)Maximum Oil Temperature: . . . . . . . . . . . . . . . . . . . . .245°F (118°C)Oil Pressure, Minimum: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .20 PSIOil Pressure, Maximum: . . . . . . . . . . . . . . . . . . . . . . . . . . . .115 PSI


AIRSPEED INDICATOR MARKINGS MARKING KIAS

White Arc 47 -100 Full Flap Operating Range. Lower limit is maximum weight VSO in landing configuration.Upper limit is maximum speed permissible with flaps extended.Green Arc 59 - 149 Normal Operating Range. Lower limit is maximum weight VS at most forward C.G. with flaps retracted. Upper limit is maximum structural cruising speed.Yellow Arc 149 - 182 Operations must be conducted with caution and only in

smooth air.Red Line 182 - Maximum speed for all operations

Cessna T206H DifferencesPOWERPLANT INSTRUMENT MARKINGS

INSTRUMENT Min Normal RedlineTachometer -- 2000 to 2400 2500ManifoldPressure --

15 to 30 in hg39 in hg

39 in hg

Cylinder HeadTemperature --

200 to 480°F 480°F

Oil Temperature --

100-245°F 245°F

Oil Pressure 20 PSI 50 to 90 PSI 115 PSI

Fuel Flow -- 0 to 20 GPH

34 GPH34 GPH

Vacuum Gage -- 4.5 to 5.5 in hg Turbine InletTemperature(TIT) (°F) --

1350 to 1675°F 1675°F


Center of Gravity Range:

Forward: 33.0 inches aft of datum at 2500 pounds or less, with straight line variation to 42.5 inches aft of datum at 3800 pounds.

Aft: 49.7 inches aft of datum at all weights.Reference Datum: Front face of lower firewall

Cessna T206H DifferencesAIRSPEEDS FOR NORMAL OPERATIONUnless otherwise noted, the following speeds are based on a maximum weight of 3800 pounds

and may be used for any lesser weight.TAKEOFFNormal Climb . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 75 - 85 KIASShort Field Takeoff, Flaps 20°, Speed at 50 Feet . . . . . . . . .74 KIASENROUTE CLIMB, FLAPS UPNormal, Sea Level. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .95 KIASBest Rate of Climb, Sea Level to 17,000 Feet . . . . . . . . . . .89 KIASBest Rate of Climb, 24,000 Feet . . . . . . . . . . . . . . . . . . . . . .79 KIASBest Angle of Climb, Sea Level. . . . . . . . . . . . .. . . . . . . . . . .69 KIASBest Angle of Climb, 10,000 Feet . . . . . . . . . . . . . . . . . . . . .72 KIASLANDING APPROACHNormal Approach, Flaps UP . . . . . . . . . . . . . . . . . . . . . 80 - 90 KIASNormal Approach, Flaps FULL . . . . . . . . . . . . . . . . . . . 70 - 80 KIASShort Field Approach, Flaps FULL . . . . . . . . . . . . . . . . . . . .67 KIASBALKED LANDINGMaximum Power, Flaps 20° . . . . . . . . . . . . . . . . . . . . . . . . .85 KIASMAXIMUM RECOMMENDED TURBULENT AIR PENETRATION SPEED3800 POUNDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .125 KIAS2950 POUNDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .120 KIAS2300 POUNDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .106 KIASMAXIMUM DEMONSTRATED CROSSWIND VELOCITYTakeoff or Landing. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .20 KNOTS

Cessna T206H DifferencesAIRSPEEDS FOR EMERGENCY OPERATIONSENGINE FAILURE AFTER TAKEOFFWing Flaps UP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .85 KIASWing Flaps 10° - FULL . . . . . . . . . . . . . . . . . . . . . . . . . . . . .75 KIASMANEUVERING SPEED3800 POUNDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .125 KIAS2950 POUNDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .120 KIAS2300 POUNDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .106 KIASMAXIMUM GLIDE3800 POUNDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .80 KIAS3200 POUNDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .75 KIAS2800 POUNDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .70 KIASPRECAUTIONARY LANDING WITH ENGINE POWER. . . . . .75 KIASLANDING WITHOUT ENGINE POWERWing Flaps UP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .85 KIASWing Flaps 10° - FULL . . . . . . . . . . . . . . . . . . . . . . . . . . . . .75 KIASEMERGENCY DESCENTSmooth Air . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .182 KIASRough Air:3800 POUNDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .125 KIAS2950 POUNDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .120 KIAS2300 POUNDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .106 KIAS


Engine Failures: Engine Failure On Takeoff Roll

Throttle – IDLEBrakes – APPLY

Engine Failure Immediately After

Takeoff85 KIAS (flaps UP)75 KIAS (flaps DOWN)

Engine Failure During Flight

(Restart Procedure)Airspeed --80 KIASFuel Selector – BOTHAuxiliary Fuel Pump – ONMixture Control - Rich

Emergency Landing Without Engine Power Passenger Seats - AS FAR FORWARD AS PRACTICAL Pilot and Passenger Seat Backs - MOST UPRIGHT POSITION Seats and Seat Belts – SECURE Airspeed - 85 KIAS - Flaps UP

75 KIAS - Flaps 10° - FULL Mixture Control - IDLE CUTOFF (pull full out) FUEL SELECTOR Valve - PUSH DOWN and ROTATE to OFF MAGNETOS Switch – OFF Wing Flaps - AS REQUIRED (FULL recommended) MASTER Switch (ALT and BAT) - OFF (when landing is assured) Doors - UNLATCH PRIOR TO TOUCHDOWN Touchdown - SLIGHTLY TAIL LOW Brakes - APPLY HEAVILY

Cessna T206H DifferencesFires: During Engine Start

Magneto Switch – STARTThrottle – FULL OPENMixture – IDLE CUT OFFFuel Selector Valve – OFFAuxiliary Fuel Pump – OFFMagneto Switch – OFFMaster Switch -- OFF

Engine Fire In Flight

Mixture – IDLE CUT OFFFuel Selector Valve – OFFAuxiliary Fuel Pump – OFFMaster Switch – OFF

Fires :

Electrical Fire In Flight Master Switch – OFF Vents/Cabin Air/Heat – CLOSED Fire Extinguisher – ACTIVATE Cabin Fire Master Switch – OFF Vents/Cabin Air/Heat – CLOSED Fire Extinguisher – ACTIVATE Wing Fire Landing/Taxi Light Switches – OFF Navigation Light Switch – OFF Strobe Light Switch – OFF Pitot Heat Switch – OFF Wing Tip Fuel Tank

Transfer Pumps – OFF

Cessna T206H DifferencesIcing: Turn Pitot Heat Switch – ON Turn Back or Change Altitude Pull Cabin Heat and Defrost Controls FULL OUT Static Source Blockage Alt Static Air Valve – PULL ON Excessive Fuel Vapor Fuel Flow Stabilization Procedure (If Fuel Flow Fluctuations of 1 GPH or More or Power Surges Occur)

Auxiliary Fuel Pump Switch – ON


MAXIMUM GLIDE

Cessna T206H DifferencesEngine Start(With Battery)1. Throttle Control - OPEN 1/4 INCH2. Propeller Control - HIGH RPM (push full in)3. Mixture Control - IDLE CUTOFF (pull full out)4. FUEL PUMP Switch – ON5. Mixture Control - FULL RICH (full forward) until stable fuel flow is indicated

(approximately 3 to 5 seconds), then set to IDLE CUTOFF (full aft) position.6. FUEL PUMP Switch - OFF7. MAGNETOS Switch - START (release when engine starts)8. Mixture Control - ADVANCE SMOOTHLY TO RICH (when engine starts)9. Mixture Control - Lean for ground operation

NOTEIf the engine is primed too much (flooded), place the mixture control in the IDLE

CUTOFF position, open the throttle control 1/2 to full, and engage the starter motor (START). When the engine starts, advance the mixture control to the FULL RICH position and retard the throttle control promptly.


LeaningRecommended lean operation is at 75°F rich of peak T.I.T.Do not continue to lean the mixture if T.I.T. reaches the red line before it peaks.

When T.I.T. reaches peak (or red line, which ever occurs first) monitor PEAK °F and FFLOW GPH , and enrichen the mixture by slowly rotating the mixture control clockwiseuntil T.I.T. drops to 75°F rich of peak or redline.

Cessna T206H DifferencesAt part throttle, the turbocharger is capable of maintaining cruise climb power of 2400 RPM and 30 in.hg. from sea level to 22,000 feet in standard temperatures, and from sea level to 17,000 feet under hot day conditions without changing the throttle position, once the power setting is established after takeoff. Under hot day conditions, this climb power setting is maintained above 17,000 feet by advancing the throttle as necessary to maintain 30 in.hg. in the same manner as a normally aspirated engine during climb.


Tip Tanks are not depicted on this diagram. Each tip tank has their own fuel pump and drain valve.


The electrical system is 28 Volt, with a 24 volt battery, and 95 amp alternator.

Cessna T206H DifferencesN7268Z Panel


Aspen Avionics Evolution 1000 PFD


Garmin GMA 340 Audio Panel


Bendix/King KLN-94 GPA


Bendix/King KX 155 Nav/Com


Bendix/King KT76C Transponder


Bendix/King KAP 140 Autopilot


Bendix/King ADF


Bendix/King KMD 550 Multi-function Display

cessna t206h differences general: engine – lycoming tio-540-aj1a 310 hp @ 2500 rpm/39”mp, mcp...

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