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

Revised Noise

Characteristics to

add ICAO

statement.

11 of 36

ISSUED:

DATE: 8/4/2017

AFMS No.: 55186-5

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

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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.

AFMS No.: 55186-5

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 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

AFMS No.: 55186-5

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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

AFMS No.: 55186-5

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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

AFMS No.: 55186-5

Rev.: 1

Page: 8 of 36

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

AFMS No.: 55186-5

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

AFMS No.: 55186-5

Rev.: 1

Page: 10 of 36

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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