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
Page: 3 of 36
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

ISSUED:
DATE: 8/4/2017
AFMS No.: 55186-5
Rev.: 1
Page: 4 of 36
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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Rev.: 1
Page: 5 of 36
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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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
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
Page: 9 of 36
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