Cessna T206H Owner's manual

AFMS No.: 55186-5
Rev.: 1
Page: 1 of 36
FAA APPROVED
DATE: 8/4/2017
Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for Cessna T206H
PILOT’S OPERATING HANDBOOK
AND FAA APPROVED
AIRPLANE FLIGHT MANUAL SUPPLEMENT
FOR
CESSNA T206H
REGISTRATION NO.:_________________
SERIAL NO.:________________________
This Supplement must be attached to the Cessna T206H “Pilot’s Operating Handbook
and FAA Approved Airplane Flight Manual” when the maximum takeoff weight is
increased to 3,789 lbs. in accordance with Supplemental Type Certificate SA09860AC.
The information contained herein supplements or supercedes the information in the
basic manual only in those areas listed. For limitations, procedures, performance and
loading information not contained in this supplement, consult the basic “Pilot’s Operating
Handbook and FAA Approved Airplane Flight Manual”.

AFMS No.: 55186-5
Rev.: 1
Page: 2 of 36
FAA APPROVED
DATE: 8/4/2017
Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for Cessna T206H
LOG OF REVISIONS
Revision
Number
Change Description Pages
Affected
FAA Approval and Date
IR Initial Release All
1
Revised Noise
Characteristics to
add ICAO
statement.
11 of 36

ISSUED:
DATE: 8/4/2017
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Rev.: 1
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Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for Cessna T206H
INTRODUCTION
PERFORMANCE SPECIFICATIONS
*SPEED
Maximum at 17,000 Feet…………………………………………… 176 KNOTS
Cruise, 75% Power at 20,000 Feet………………………………… 161 KNOTS
Cruise, 75% Power at 10,000 Feet………………………………… 148 KNOTS
CRUISE – Recommended lean mixture with fuel allowance for engine start, taxi,
Takeoff, climb and 45 minute reserve.
75% Power at 20,000 Feet……………………………………… Range – 546 NM
87 Gallons Usable Fuel……………………………………. Time – 3.6 HOURS
75% Power at 10,000 Feet……………………………………… Range – 527 NM
87 Gallons Usable Fuel……………………………………. Time – 3.6 HOURS
Max Range at 20,000 Feet……………………………………… Range – 608 NM
87 Gallons Usable Fuel………………………………… Time – 4.9 HOURS
Max Range at 10,000 Feet……………………………………… Range – 676 NM
87 Gallons Usable Fuel……………………………………. Time – 6.3 HOURS
RATE OF CLIMB AT SEA LEVEL…………………………………………. 960 FPM
SERVICE CEILING…………………………………………………….. 26,000 FEET
TAKEOFF PERFORMANCE:
Ground Roll…………………………………………………………….. 1060 FEET
Total Distance Over 50 Foot Obstacle………………………………. 1970 FEET
STALL SPEED (KCAS):
Flaps UP, Power Idle……………………………………………………. 69 KCAS
Flaps FULL, Power Idle…………………………………………………. 58 KCAS
MAXIMUM WEIGHT:
Ramp……………………………………………………………….. 3806 POUNDS
Takeoff………………………………………………………………3789 POUNDS
Landing…………………………………………………………….. 3600 POUNDS
MAXIMUM USEFUL LOAD…………………………………………. 1492 POUNDS
WING LOADING…………………………………………………………21.8 lbs/sq.ft
POWER LOADING:………………………………………………………. 12.2 lbs/HP

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Rev.: 1
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Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for Cessna T206H
NOTE
*Speed performance and range are shown for an airplane equipped with the standard
wheel and brake fairings. These fairings increase the speeds approximately 3 knots
over an airplane without the fairings. Heavy duty wheels, tires and brakes are available
and when installed with the appropriate wheel and brake fairings, result in no significant
change in performance.

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Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for Cessna T206H
FAA APPROVED:
DATE: 8/4/2017
SECTION 1
GENERAL
DESCRIPTIVE DATA
MAXIMUM CERTIFICATED WEIGHTS
Ramp Weight…………………………………………………………….3806 POUNDS
Takeoff Weight…………………………………………………………..3789 POUNDS
Landing Weight………………………………………………………….3600 POUNDS
Maximum Weight in Baggage Compartment:
Baggage Area – Station 109 to 145……………………………180 POUNDS
NOTE
Refer to section 6 of the Basic POH/AFM for loading
arrangements with one or more seats removed for cargo
accommodations.
SPECIFIC LOADINGS
Wing Loading…………………………………………………………….21.8 lbs./sq. ft.
Power Loading…………………………………………………………..12.2 lbs./hp

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Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for Cessna T206H
FAA APPROVED:
DATE: 8/4/2017
SECTION 2
OPERATING LIMITATIONS
AIRSPEED LIMITATIONS
Airspeed limitations and their operational significance are shown in Figure 2-1.
AIRSPEED LIMITATIONS
SYMBOL SPEED KCAS KIAS REMARKS
VAManeuvering Speed:
3789 POUNDS 123 125
Do not make full or abrupt
control movements above
this speed.
Figure 2-1
AIRSPEED INDICATOR MARKINGS
Airspeed indicator markings and their color code significance are shown in Figure
2-2.
AIRSPEED INDICATOR MARKINGS
MARKING KIAS VALUE OR
RANGE SIGNIFICANCE
Red Arc* 20 - 53 Low airspeed warning.
White Arc 53 - 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 65 - 149
Normal Operating Range. Lower limit is
maximum weight VSat 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 is smooth air.
Red Line 182 Maximum speed for all operations.
*G1000 airspeed indicator only
Figure 2-2

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Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for Cessna T206H
FAA APPROVED:
DATE: 8/4/2017
WEIGHT LIMITS
Maximum Ramp Weight………………………………………………..3806 POUNDS
Maximum Takeoff Weight………………………………………………3789 POUNDS
Maximum Landing Weight…………………………………….………. 3600 POUNDS
Maximum Weight in Baggage Compartment:
Baggage Area – Station 109 to 145…………………………….180 POUNDS
NOTE
Refer to section 6 for loading arrangements with one or more
seats removed for cargo accommodations.
CENTER OF GRAVITY LIMITS
CENTER OF GRAVITY RANGE:
Forward: 33.0 inches aft of datum at 2500 pounds or less,
with straight line variation to 44.1 inches aft of
datum at 3789 pounds.
Aft: 49.7 inches aft of datum at all weights.
Reference Datum: Front face of lower firewall
FLIGHT LOAD FACTOR LIMITS
Flight Load Factors (Maximum Takeoff Weight – 3789 POUNDS):
Flaps UP……………………………………………………………….+3.8g, -1.52g
Flaps FULL……………………………………………………………………..+2.0g

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Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for Cessna T206H
FAA APPROVED:
DATE: 8/4/2017
SECTION 3
EMERGENCY PROCEDURES
AIRSPEEDS FOR EMERGENCY OPERATIONS
MANEUVERING SPEED
3789 POUNDS…………………………………………………125 KIAS
MAXIMUM GLIDE
3789 POUNDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .82 KIAS
EMERGENCY DESCENT
Rough Air:
3789 POUNDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .125 KIAS
EMERGENCY PROCEDURES
ENGINE FAILURES
ENGINE FAILURE DURING FLIGHT (Restart Procedures)
1. Airspeed - 82 KIAS (best glide speed)
EMERGENCY DESCENT
ROUGH AIR
6. Weights and Airspeeds:
3789 POUNDS - 125 KIAS
AMPLIFIED EMERGENCY PROCEDURES
ENGINE FAILURE
MAXIMUM GLIDE
Best Glide Speed
Weight KIAS
3789 Pounds 82

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Rev.: 1
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Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for Cessna T206H
FAA APPROVED:
DATE: 8/4/2017
SECTION 4
NORMAL PROCEDURES
AIRSPEEDS FOR NORMAL OPERATION
The following speeds are based on a maximum weight of 3789 pounds. Consult
the basic POH/AFM for speeds at lesser weights.
Serials T20608450 thru T20608681 and T20608683 thru
T20608704 not incorporating MK206-34-10;
T20608682 and T20608705 thru T20608882 not
incorporating SB09-34-11
Short Field Takeoff, Flaps 20°, Speed at 50 Feet . . . . . . . . .76 KIAS
Serials T20608450 thru T20608681 and T20608683 thru T20608704
incorporating MK206-34-10;
Serials T20608682 and T20608705 thru T20608882 incorporating
SB09-34-11 and Serials T20608883 and On
Short Field Takeoff, Flaps 20°, Speed at 50 Feet . . . . . . . . .71 KIAS
ENROUTE CLIMB, FLAPS UP
Normal, Sea Level. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .95 KIAS
Best Rate of Climb, Sea Level to 17,000 Feet . . . . . . . . . . ..88 KIAS
Best Rate of Climb, 24,000 Feet . . . . . . . . . . . . . . . . . . . . . .80 KIAS
Best Angle of Climb, Sea Level. . . . . . . . . . . . . . . . . . . . . . .70 KIAS
Best Angle of Climb, 10,000 Feet . . . . . . . . . . . . . . . . . . . . .73 KIAS
MAXIMUM RECOMMENDED TURBULENT AIR
PENETRATION SPEED
3789 POUNDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 125 KIAS

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Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for Cessna T206H
FAA APPROVED:
DATE: 8/4/2017
NORMAL PROCEDURES
TAKEOFF
NORMAL TAKEOFF
5. Elevator Control - LIFT NOSEWHEEL (at 56 KIAS)
SHORT FIELD TAKEOFF
Serials T20608450 thru T20608681 and T20608683 thru
T20608704 not incorporating MK206-34-10;
T20608682 and T20608705 thru T20608882 not
incorporating SB09-34-11
8. Climb Airspeed - 76 KIAS (until all obstacles are cleared)
Serials T20608450 thru T20608681 and T20608683 thru T20608704
incorporating MK206-34-10;
Serials T20608682 and T20608705 thru T20608882 incorporating
SB09-34-11 and Serials T20608883 and On
8. Climb Airspeed - 71 KIAS (until all obstacles are cleared)
MAXIMUM PERFORMANCE CLIMB
1. Airspeed - 88 KIAS
AMPLIFIED NORMAL PROCEDURES
WING FLAP SETTINGS
Serials T20608450 thru T20608681 and T20608683 thru T20608704 not
incorporating MK206-34-10; T20608682 and T20608705 thru T20608882 not
incorporating SB09-34-11
Short field takeoffs are performed with wing flaps set at 20° and an obstacle
clearance speed of 76 KIAS
Serials T20608450 thru T20608681 and T20608683 thru T20608704
incorporating MK206-34-10; Serials T20608682 and T20608705 thru
T20608882 incorporating SB09-34-11 and Serials T20608883 and On
Short field takeoffs are performed with wing flaps set at 20° and an obstacle
clearance speed of 71 KIAS

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Page: 11 of 36
Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for Cessna T206H
FAA APPROVED:
DATE: 8/4/2017
ENROUTE CLIMB
If it is necessary to climb more rapidly to clear mountains or reach favorable winds
at higher altitudes, the best rate of climb speed should be used with MCP. This
speed is 88 KIAS from seal level to 17,000 feet, decreasing to 80 KIAS at 24,000
feet.
If an obstruction dictates the use of a steep climb angle, the best angle of climb
speed is 70 KIAS at sea-level, increasing to 73 KIAS at 10,000 feet. This type of
climb should be of the minimum duration and engine temperatures should be
carefully monitored due to the low climb speed.
NOISE CHARACTERISTICS
The certificated takeoff noise level for the Cessna Model T206H at 3789 pounds
maximum weight is 82.6 dB(A) per 14 CFR 36 Appendix G (through Amendment
36-30) and ICAO Annex 16 chapter 10 (through Amendment 11-B).
This noise level was established at a maximum weight of 3789 pounds with wing
flaps set at 20 degrees for Takeoff and flaps Up for climb at a speed of 88 KIAS
and takeoff power. No determination has been made by the Federal Aviation
Administration that the noise levels of this airplane are or should be acceptable or
unacceptable for operation at, into, or out of, any airport.

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Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for Cessna T206H
FAA APPROVED:
DATE: 8/4/2017
SECTION 5
PERFORMANCE
STALL SPEEDS AT 3789 POUNDS
Serials T20608450 thru T20608681 and T20608683 thru
T20608704 not incorporating MK206-34-10;
T20608682 and T20608705 thru T20608882 not
incorporating SB09-34-11
CONDITIONS:
Power Idle
MOST REARWARD CENTER OF GRAVITY
Flap ANGLE OF BANK
Settings 0° 30° 45° 60°
KIAS KCAS KIAS KCAS KIAS KCAS KIAS KCAS
UP 59 64 66 69 75 76 90 91
20° 58 58 63 62 71 69 84 82
FULL 49 55 55 59 63 65 78 78
MOST FORWARD CENTER OF GRAVITY
Flap ANGLE OF BANK
Settings 0° 30° 45° 60°
KIAS KCAS KIAS KCAS KIAS KCAS KIAS KCAS
UP 65 69 73 74 82 82 99 98
20° 63 62 69 67 76 74 89 88
FULL 53 58 60 62 68 69 82 82
NOTE
Altitude loss during a stall recovery may be as much as 400 feet
KIAS values are approximate
Figure 5-4

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Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for Cessna T206H
FAA APPROVED:
DATE: 8/4/2017
STALL SPEEDS AT 3789 POUNDS
Serials T20608450 thru T20608681 and T20608683 thru T20608704
incorporating MK206-34-10;
Serials T20608682 and T20608705 thru T20608882 incorporating
SB09-34-11 and Serials T20608883 and On
CONDITIONS:
Power Idle
MOST REARWARD CENTER OF GRAVITY
Flap ANGLE OF BANK
Settings 0° 30° 45° 60°
KIAS KCAS KIAS KCAS KIAS KCAS KIAS KCAS
UP 59 64 66 69 75 76 90 91
20° 51 58 56 62 65 69 81 82
FULL 49 55 55 59 63 65 78 78
MOST FORWARD CENTER OF GRAVITY
Flap ANGLE OF BANK
Settings 0° 30° 45° 60°
KIAS KCAS KIAS KCAS KIAS KCAS KIAS KCAS
UP 65 69 73 74 82 82 99 98
20° 56 62 63 67 71 74 89 88
FULL 53 58 60 62 68 69 82 82
NOTE
Altitude loss during a stall recovery may be as much as 400 feet
KIAS values are approximate
Figure 5-4A

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Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for Cessna T206H
ISSUED:
DATE: 8/4/2017
SHORT FIELD TAKEOFF DISTANCE
AT 3789 POUNDS
Serials T20608450 thru T20608681 and T20608683 thru
T20608704 not incorporating MK206-34-10;
T20608682 and T20608705 thru T20608882 not
incorporating SB09-34-11
CONDITIONS:
Flaps 20°
2500 RPM, 39 in. hg. and mixture set at 34 GPH prior to brake release.
Cowl Flaps OPEN
Paved, Level, Dry Runway Lift Off: 65 KIAS
Zero Wind Speed at 50 Feet: 76 KIAS
Pressure
Altitude -
Feet
0°C 10°C 20°C 30°C 40°C
Gnd
Roll
Feet
Total
Feet
To
Clear
50
Foot
Obst
Gnd
Roll
Feet
Total
Feet
To
Clear
50
Foot
Obst
Gnd
Roll
Feet
Total
Feet
To
Clear
50
Foot
Obst
Gnd
Roll
Feet
Total
Feet
To
Clear
50
Foot
Obst
Gnd
Roll
Feet
Total
Feet
To
Clear
50
Foot
Obst
Sea-
Level 960 1785 1025 1905 1095 2035 1180 2175 1260 2325
1000 1015 1875 1090 2025 1170 2160 1255 2305 1340 2455
2000 1085 2002 1165 2140 1245 2290 1335 2455 1425 2615
3000 1160 2115 1240 2270 1335 2430 1425 2590 1525 2735
4000 1235 2245 1330 2410 1420 2575 1520 2770 1625 2975
5000 1315 2380 1415 2550 1520 2750 1625 2940 1740 3170
6000 1410 2535 1515 2710 1630 2920 1745 3150 1875 3380
7000 1505 2690 1630 2915 1750 3135 1880 3375 2010 3600
8000 1625 2890 1750 3110 1880 3360 2015 3600 2160 3865
NOTE
Short field technique as specified in Section 4.
Decrease distances by 10% for each 10 knots headwind.
For operation with tail winds up to 10 knots, increase distances by 10%
for each 2.5 knots.
For operation on dry, grass runway, increase distances by 15% of the
“ground roll” figure.
Figure 5-6 (Sheet 1)

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Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for Cessna T206H
ISSUED:
DATE: 8/4/2017
SHORT FIELD TAKEOFF DISTANCE
AT 3789 POUNDS
Serials T20608450 thru T20608681 and T20608683 thru T20608704
incorporating MK206-34-10;
Serials T20608682 and T20608705 thru T20608882 incorporating
SB09-34-11 and Serials T20608883 and On
CONDITIONS:
Flaps 20°
2500 RPM, 39 in. hg. and mixture set at 34 GPH prior to brake release.
Cowl Flaps OPEN
Paved, Level, Dry Runway Lift Off: 58 KIAS
Zero Wind Speed at 50 Feet: 71 KIAS
Pressure
Altitude -
Feet
0°C 10°C 20°C 30°C 40°C
Gnd
Roll
Feet
Total
Feet
To
Clear
50
Foot
Obst
Gnd
Roll
Feet
Total
Feet
To
Clear
50
Foot
Obst
Gnd
Roll
Feet
Total
Feet
To
Clear
50
Foot
Obst
Gnd
Roll
Feet
Total
Feet
To
Clear
50
Foot
Obst
Gnd
Roll
Feet
Total
Feet
To
Clear
50
Foot
Obst
Sea-
Level 960 1785 1025 1905 1095 2035 1180 2175 1260 2325
1000 1015 1875 1090 2025 1170 2160 1255 2305 1340 2455
2000 1085 2002 1165 2140 1245 2290 1335 2455 1425 2615
3000 1160 2115 1240 2270 1335 2430 1425 2590 1525 2735
4000 1235 2245 1330 2410 1420 2575 1520 2770 1625 2975
5000 1315 2380 1415 2550 1520 2750 1625 2940 1740 3170
6000 1410 2535 1515 2710 1630 2920 1745 3150 1875 3380
7000 1505 2690 1630 2915 1750 3135 1880 3375 2010 3600
8000 1625 2890 1750 3110 1880 3360 2015 3600 2160 3865
NOTE
Short field technique as specified in Section 4.
Decrease distances by 10% for each 10 knots headwind.
For operation with tail winds up to 10 knots, increase distances
by 10% for each 2.5 knots.
For operation on dry, grass runway, increase distances by 15%
of the “ground roll” figure.
Figure 5-6 (Sheet 2)

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Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for Cessna T206H
ISSUED:
DATE: 8/4/2017
MAXIMUM RATE OF CLIMB
CONDITIONS:
Flaps UP
2500 RPM, Manifold Pressure and Mixture set to Minimum Fuel Flows
Maximum Continuous Power Placard
Cowl Flaps OPEN
Weight
Pounds
Pressure Alt
- Feet
Climb Speed -
KIAS
Rate of Climb - FPM
-20°C 0°C 20°C 40°C
3789
0 88 1210 1070 925 780
2000 88 1140 1000 860 710
4000 88 1080 935 795 650
6000 88 1010 865 725 580
8000 88 940 800 660 520
10000 88 880 740 600 465
12000 88 815 675 545 405
14000 88 745 610 480 350
16000 88 680 550 430 305
20000 82 435 320 205 -----
24000 80 155 ----- ----- -----
Figure 5-7

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ISSUED:
DATE: 8/4/2017
TIME FUEL AND DISTANCE TO CLIMB
AT 3789 LBS.
MAXIMUM RATE OF CLIMB
CONDITIONS:
FLAPS UP
2500 RPM, Manifold Pressure and Mixture set to Minimum Fuel Flows
Maximum Continuous Power Placard
Cowl Flaps OPEN
Standard Temperature
Pressure
Altitude
Feet
Climb
Speed
KIAS
Rate of
Climb
FPM
From Sea Level
Time
Minutes
Fuel Used
Gallons
Distance
NM
0 88 960 0 0 0
2000 88 920 2 1.2 3
4000 88 885 4 2.5 6
6000 88 845 7 3.8 10
8000 88 805 9 5.1 14
10000 88 775 12 6.6 18
12000 88 740 14 8.1 23
14000 88 700 17 9.7 28
16000 88 660 20 11.3 33
18000 83 560 23 13.0 39
20000 82 460 27 14.9 46
22000 81 335 32 17.2 56
24000 80 190 40 20.6 71
NOTE
Add 2.6 gallons of fuel for engine start, taxi and takeoff allowance.
Increase time, fuel and distance by 10% for each 10°C above standard
temperature.
Distances shown are based on zero wind.
Figure 5-8 (Sheet 1)

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ISSUED:
DATE: 8/4/2017
TIME FUEL AND DISTANCE TO CLIMB
AT 3789 LBS.
NORMAL CLIMB – 95 KIAS
CONDITIONS:
FLAPS UP Cowl Flaps OPEN
2400 RPM at 30.0 in. Hg. Standard Temperature
20 GPH Fuel Flow
WEIGHT
POUNDS
PRESSURE
ALTITUDE
FEET
RATE OF
CLIMB
FPM
FROM SEA LEVEL
TIME IN
MINUTES
FUEL
USED
GAL
DISTANCE
NM
3789
0 620 0 0 0
2000 600 3 1.1 5
4000 575 7 2.2 11
6000 550 10 3.4 17
8000 525 14 4.7 23
10000 490 18 6.0 30
12000 470 22 7.4 38
14000 445 26 8.8 46
16000 420 31 10.4 56
18000 395 36 12.0 66
NOTE
Add 2.6 gallons of fuel for engine start, taxi and takeoff allowance.
Increase time, fuel and distance by 10% for each 8°C above standard
temperature.
Distances shown are based on zero wind.
Figure 5-8 (Sheet 2)

ISSUED:
DATE: 8/4/2017
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Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for Cessna T206H
CRUISE PERFORMANCE
PRESSURE ALTITUDE 2000 FEET
CONDITIONS:
3789 Pounds
Recommended Lean Mixture Cowl Flaps CLOSED
RPM MP
(in. Hg.)
20°C BELOW
STANDARD TEMP
-9°C
STANDARD
TEMPERATURE
11°C
20°C ABOVE
STANDARD TEMP
31°C
% MCP KTAS GPH % MCP KTAS GPH % MCP KTAS GPH
2400
30 ----- ----- ----- 74 138 18.9 69 136 17.8
28 73
135 18.7 69 134 17.6 65 133 16.5
26 68
130 17.4 64 129 16.4 60 127 15.4
24 63
126 16.1 59 124 15.1 56 123 14.2
22 57
120 14.7 54 118 13.8 51 116 13
20 52
114 13.3 49 112 12.6 46 108 11.8
2300
30 75
136 19.2 71 136 18.1 67 134 17.0
28 70
132 17.9 66 131 16.8 62 129 15.8
26 64
127 16.4 61 126 15.5 57 124 14.5
24 59
122 15.1 56 121 14.2 52 118 13.3
22 54
116 13.8 51 115 13.0 48 112 12.2
20 49
110 12.5 46 107 11.8 43 103 11.1
2200
30 72
134 18.4 68 133 17.3 64 131 16.3
28 67
130 17.0 63 128 16.1 59 126 15.1
26 61
124 15.5 57 122 14.6 54 121 13.7
24 55
118 14.1 52 116 13.3 49 113 12.5
22 50
112 12.9 48 110 12.2 45 107 11.5
20 45
104 11.7 43 102 11.0 40 96 10.4
2100
30 69
131 17.6 65 130 16.6 61 128 15.5
28 64
127 16.3 60 125 15.3 56 123 14.4
26 58
121 14.9 55 120 14.0 51 116 13.1
24 53
115 13.5 50 113 12.7 47 110 12.0
22 48
109 12.3 45 106 11.7 42 100 11.0
2000
30 66
129 16.8 62 127 15.8 58 125 14.8
28 60
123 15.5 57 122 14.6 53 119 13.7
26 56
119 14.2 52 116 13.4 49 113 12.6
24 50
112 12.9 47 109 12.2 44 105 11.5
22 46
106 11.8 43 102 11.1 40 95 10.5
NOTE
For best economy, operate at peak T.I.T.
Some power settings may not be obtainable, but are listed to aid interpolation.
Power settings not approved for cruising are indicated by dashes.
Figure 5-9 (Sheet 1)

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DATE: 8/4/2017
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Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for Cessna T206H
CRUISE PERFORMANCE
PRESSURE ALTITUDE 4000 FEET
CONDITIONS:
3789 Pounds
Recommended Lean Mixture Cowl Flaps CLOSED
RPM MP
(in. Hg.)
20°C BELOW
STANDARD TEMP
-13°C
STANDARD
TEMPERATURE
7°C
20°C ABOVE
STANDARD TEMP
27°C
% MCP KTAS GPH % MCP KTAS GPH % MCP KTAS GPH
2400
30 ----- ----- ----- 75 141 19.1 70 139 17.9
28 74
138 18.9 70 137 17.8 65 135 16.7
26 69
133 17.6 65 132 16.6 61 130 15.6
24 64
129 16.3 60 127 15.4 56 124 14.4
22 58
123 14.9 55 121 14.0 51 117 13.2
20 53
117 13.5 50 115 12.8 47 111 12.0
2300
30 76
139 19.4 71 138 18.3 67 137 17.1
28 71
135 18.0 66 133 17.0 62 131 15.9
26 65
130 16.6 61 128 15.7 57 126 14.7
24 60
125 15.3 56 122 14.4 53 120 13.5
22 55
119 14.0 51 116 13.2 48 113 12.4
20 49
112 12.7 47 110 12.0 44 105 11.3
2200
30 72
136 18.5 68 135 17.4 64 134 16.4
28 67
132 17.1 63 130 16.1 59 128 15.1
26 61
126 15.7 58 125 14.8 54 122 13.8
24 56
120 14.3 53 119 13.5 49 114 12.7
22 51
114 13.1 48 111 12.3 45 107 11.6
20 46
107 11.8 43 103 11.2 41 98 10.6
2100
30 69
133 17.7 65 132 16.7 61 130 15.7
28 64
129 16.4 60 127 15.4 57 126 14.5
26 59
124 15.0 55 121 14.2 52 119 13.3
24 53
117 13.6 50 115 12.9 47 111 12.1
22 49
112 12.5 46 108 11.8 43 103 11.1
2000
30 66
131 16.9 62 129 16.0 59 128 15.0
28 61
126 15.6 57 124 14.7 54 122 13.8
26 56
120 14.4 53 119 13.5 50 115 12.7
24 51
114 13.0 48 111 12.3 45 107 11.6
22 46
107 11.9 44 105 11.3 41 98 10.7
NOTE
For best economy, operate at peak T.I.T.
Some power settings may not be obtainable, but are listed to aid interpolation.
Power settings not approved for cruising are indicated by dashes.
Figure 5-9 (Sheet 2)