Cessna 206 Betriebsanleitung

ISSUE DATE:

PO Box 2119

265 Shannon Lane

Priest River ID 83856

Page

1 of 38

8/23/10

INCORPORATED

FILE NO.

REVISION

DATE

TITLE: Supplemental Airplane Flight Manual

A-10060

03/04/15

SUBTITLE:

Cessna 206 on Model 3400 Floats

REVISION: D

FAA APPROVED

SUPPLEMENTAL AIRPLANE FLIGHT MANUAL

FOR

CESSNA 206 SERIES FLOATPLANES

MODELS: 206, P206, P206A-E, U206, U206A-G,

TU206A-G, TP206A-E, T206H

Equipped With AEROCET 3400 Amphibious Seaplane Floats

Registration No.__________________

Serial No._________________

The information contained in this document is FAA approved material

which must be applied together with the basic FAA approved airplane

placards and markings and/or FAA approved Airplane Flight Manual. This

supplemental manual must be carried in the airplane when it is modified by

the installation of the Aerocet Model 3400 amphibious seaplane floats in

accordance with Supplemental Type Certificate (STC) No. SA01257SE.

The information contained in this document supersedes the basic airplane

markings and placards and/or Flight Manual covered in the items contained

herein. For Limitations, Procedures, and Performance information not

contained in this supplement, consult the basic airplane markings and

placards, and/or Flight Manual.

FAA Approved: ________________________

Manager, Seattle Aircraft Certification Office

Date: ______________

ISSUE DATE:

PO Box 2119

265 Shannon Lane

Priest River ID 83856

Page

3 of 38

8/23/10

INCORPORATED

FILE NO.

REVISION

DATE

TITLE: Supplemental Airplane Flight Manual

A-10060

03/04/15

SUBTITLE:

Cessna 206 on Model 3400 Floats

REVISION: D

FAA Approved

SECTION 1. GENERAL

This supplemental manual, applicable to those Cessna Model 206 Series

airplanes equipped with Aerocet Model 3400 Amphibious Seaplane Floats,

provides information and limitations not included in the basic FAA

approved markings and placards, and/or Airplane Flight Manual. Whenever

the words "Not Applicable" (NA) appear in this supplemental manual, they

are used to indicate that the related information may not be the same as that

shown in the Cessna markings and placards, and/or Flight Manual and are

not required by the airplane certification basis and, therefore, should not be

referenced. The aircraft is to be operated under the "NORMAL

CATEGORY" only.

PERFORMANCE – SPECIFICATIONS

(for model T206H see Section 5 for additional performance information)

SPEED: NA

CRUISE: NA

RATE OF CLIMB AT SEA LEVEL: EXCEEDS 550 FPM (CAR 3.85a)

SERVICE CEILING: NA

TAKEOFF PERFORMANCE ON WATER: NA

LANDING PERFORMANCE ON WATER: NA

TAKEOFF PERFORMANCE ON LAND: Increase take-off roll distance

by 10% factored @ 3600 Gross Weight Pounds using Hartzell PHC-C3YF-

1RF/F8468A-6R propeller

LANDING PERFORMANCE ON LAND: Increase landing roll distance

by 16% factored @ 3600 Gross Weight Pounds

STALL SPEED (POWER OFF, FORWARD CG @ 3744 lbs):

FLAPS UP: 61 KCAS

FLAPS DOWN 30º: 54 KCAS

MAXIMUM WEIGHT:

RAMP or DOCK: 3755 LBS.

TAKE-OFF FLOATS: 3744 LBS.

LANDING FLOATS: 3661 LBS.

TAKE-OFF WHEELS: 3735 LBS.

LANDING WHEELS: 3550 LBS.

EMPTY WEIGHT: SEE ACTUAL WT. & BALANCE FORM FOR

AIRCRAFT

MAXIMUM USEFUL LOAD: REF. ACTUAL WT. & BALANCE FORM

FOR A/C

ISSUE DATE:

PO Box 2119

265 Shannon Lane

Priest River ID 83856

Page

4 of 38

8/23/10

INCORPORATED

FILE NO.

REVISION

DATE

TITLE: Supplemental Airplane Flight Manual

A-10060

03/04/15

SUBTITLE:

Cessna 206 on Model 3400 Floats

REVISION: D

FAA Approved

PERFORMANCE – SPECIFICATIONS (Cont’d)

BAGGAGE ALLOWANCE:

IN AIRPLANE: NO CHANGE

IN EACH FLOAT: 100 LBS.

(CAUTION: ASSURE CG RANGE IS PROPER WHEN LOADING)

WING LOADING: NA

POWER LOADING: NA

RANGE: NA

FUEL CAPACITY: NO CHANGE

OIL CAPACITY: NO CHANGE

ENGINE: NO CHANGE

PROPELLER: One of the following propellers is required.

Models A through G:

The propeller installation is not covered by this STC and must be FAA

approved by a separate FAA approval, (such as TCDS, STC, or 337).

•Hartzell PHC-C3YF-1RF/F8468A-6R or greater in approved

diameter

•Hartzell PHC-C3YF-1RF/F8068-2 (-0 ok)

•Hartzell PHC-J3YF-1RF/F8068-2 (-0 ok)

•McCauley D3A34C401/90DFA-2 (-4,-8,-10 ok)

•McCauley D3A34C402/90DFA-2 (-4,-8,-10 ok)

Models H only:

•Hartzell HC-F3YR-1RF/F8468A-2R (-4R, -6R ok)

i.a.w. Aerocet STC

•McCauley B3D36C432/80VSA -1 (not less than 77.5")

i.a.w. Cessna TCDS

ISSUE DATE:

PO Box 2119

265 Shannon Lane

Priest River ID 83856

Page

5 of 38

8/23/10

INCORPORATED

FILE NO.

REVISION

DATE

TITLE: Supplemental Airplane Flight Manual

A-10060

03/04/15

SUBTITLE:

Cessna 206 on Model 3400 Floats

REVISION: D

FAA Approved

SECTION 2. LIMITATIONS

CENTER OF GRAVITY LIMITS:

Center of Gravity Range: (inches aft of reference datum –front face of

firewall)

(+42.1) to (+47.4) at 3744 lbs. Maximum G.W.

(+36.5) to (+47.4) at 2600 lbs. or less with a straight line

variation between points given.

WEIGHT LIMITS:

Maximum Ramp or Dock: 3755 lbs.

Maximum Take-off Floats: 3744 lbs.

Maximum Landing Floats: 3661 lbs.

Maximum Take-off Wheels: 3735 lbs.

Maximum Landing Wheels: 3550 lbs.

Maximum Weight in Baggage Compartment: NO CHANGE

Maximum Weight in Float Baggage Compartment: 100 lbs. each

AIRSPEED LIMITS:

KC AS KIAS

MPH

CAS

MPH

IAS

Never Exceed Speed (Vne)

No Change No Change No Change No Change

Max St ruct ur al Cruising (Vno )

No Change No Change No Change No Change

Max Maneuvering Speed (Va)

No Change No Change No Change No Change

Max. Speed with Flaps (Vfe)

No Change No Change No Change No Change

Max Ldg. Gear Operating Speed (Vlo) 118 120 136 138

Max Ldg. Gear Extended Speed (Vle) 148 150 170 172

ISSUE DATE:

PO Box 2119

265 Shannon Lane

Priest River ID 83856

Page

6 of 38

8/23/10

INCORPORATED

FILE NO.

REVISION

DATE

TITLE: Supplemental Airplane Flight Manual

A-10060

03/04/15

SUBTITLE:

Cessna 206 on Model 3400 Floats

REVISION: D

FAA Approved

MANEUVER LIMITS

The maneuver limits defined in the basic handbook are applicable to the

amphibian.

“Avoid slips with wing flaps extended”

FLAP LIMITATIONS

Approved Takeoff Range: 0° to 20°.

Approved Runway Landing Range: 0° to 30°.

Approved Water Landing Range: 0° to 30°.

NOTE: Wing flaps must be retracted to 20° immediately

following power application for a balked landing go-around.

AIR SPEED INDICATOR MARKINGS:

The airspeed indicator markings are the same as shown in the basic

markings/Flight manual. Due to differences in airspeed calibration and

speeds with floats installed, the indicated stall speeds and maximum

structural cruising speed vary slightly from airspeed indicator markings.

PLACARDS:

1. Aerocet P/N 35A-59330 Placard is located in plain view of the pilot:

“EMERGENCY

LANDING GEAR OPERATION

If electric driven hydraulic pump fails, use hand

operated pump to retract and extend landing gear.

Land on sod if gear position is unknown.

DO NOT LAND ON WATER UNLESS

GEAR IS FULLY RETRACTED”

ISSUE DATE:

PO Box 2119

265 Shannon Lane

Priest River ID 83856

Page

7 of 38

8/23/10

INCORPORATED

FILE NO.

REVISION

DATE

TITLE: Supplemental Airplane Flight Manual

A-10060

03/04/15

SUBTITLE:

Cessna 206 on Model 3400 Floats

REVISION: D

FAA Approved

PLACARDS: (Cont’d)

2. Aerocet P/N 36-15605 Placard is located near the emergency gear hand

pump:

“EMERGENCY HAND PUMP

OPERATING INSTRUCTIONS

1. Pull landing gear motor circuit breaker.

2. Move landing gear position switch to

desired position.

3. Rotate emergency gear selector valve to

desired position.

4. Pump emergency gear hydraulic pump until

gear lights show for desired position and

there is significant force on the pump

handle.

Always keep gear selector valve in OFF

position (detent engaged –handle pointed

toward pilot seat) except for emergency

operation.”

3.Aerocet P/N 35A-59332 Placard is located on the instrument panel:

“IN FLOATPLANE, AMPHIBIAN AND SKIPLANE RETRACT

FLAPS TO 20° IMMEDIATELY AFTER APPLYING POWER FOR

BALKED LANDING GO-AROUND.”

4. Refer to Cessna type data for required fuel placards.

ISSUE DATE:

PO Box 2119

265 Shannon Lane

Priest River ID 83856

Page

8 of 38

8/23/10

INCORPORATED

FILE NO.

REVISION

DATE

TITLE: Supplemental Airplane Flight Manual

A-10060

03/04/15

SUBTITLE:

Cessna 206 on Model 3400 Floats

REVISION: D

FAA Approved

PLACARDS: (Cont’d)

5. Aerocet P/N 35A-59334 Placard on instrument panel:

“IN FLOATPLANE, AMPHIBIAN AND SKIPLANE AVOID SLIPS

WITH FLAPS EXTENDED.”

6. Aerocet P/N 35-70006 Placard is located on aft part of console near

water rudder handle in the "RETRACT" position:

"WATER RUDDER

ALWAYS UP

EXCEPT

WATER TAXIING"

7. Aerocet P/N 35-70011 Placard is located in plain view of the pilot:

"AVOID TAIL-LOW TAKEOFFS AND LANDINGS

WITH FLOATPLANE STINGER INSTALLED

DURING OPERATIONS AS A LANDPLANE

8. Aerocet P/N 36-15601 Placard is located inside the float locker panels:

"MAX BAGGAGE: 100 LBS.

ARM: 32.4 in. AFT DATUM

9. Circuit Breaker Placards:

“PUMP PWR”, “PUMP RELAYS”, “GR. ADV. ELEC.”

ISSUE DATE:

PO Box 2119

265 Shannon Lane

Priest River ID 83856

Page

9 of 38

8/23/10

INCORPORATED

FILE NO.

REVISION

DATE

TITLE: Supplemental Airplane Flight Manual

A-10060

03/04/15

SUBTITLE:

Cessna 206 on Model 3400 Floats

REVISION: D

FAA Approved

SECTION 3. EMERGENCY PROCEDURES:

Emergency procedures in the FAA approved airplane placards and/or Flight

Manual generally apply except for airspeeds which may be different.

Emergency landings on water should be done with water rudders up,

aircraft slightly tail low on touchdown, and control wheel held full aft as the

floatplane decelerates on the water. Emergency landings on land should be

done with water rudders up, aircraft in a level attitude on touchdown, and

the control wheel full aft after contact. If damage occurs to the floats

causing compartments to flood, aggressively shift the weight (people &

baggage) in the opposite direction of damage in order to balance the aircraft

over the buoyant compartments.

EMERGENCY OPERATIONAL CHECKLISTS

ENGINE FAILURE

ENGINE FAILURE DURING TAKEOFF RUN (ON WATER)

1. Throttle -- IDLE.

2. Control Wheel -- FULL AFT.

3. Mixture -- IDLE CUT-OFF.

4. Ignition Switch -- OFF.

5. Master Switch -- OFF.

ENGINE FAILURE DURING TAKEOFF RUN (ON LAND)

1. Throttle -- IDLE.

2. Brakes -- APPLY.

3. Wing Flaps -- RETRACT.

4. Mixture -- IDLE CUT-OFF.

5. Ignition Switch -- OFF.

6. Master Switch -- OFF.

ISSUE DATE:

PO Box 2119

265 Shannon Lane

Priest River ID 83856

Page

10 of 38

8/23/10

INCORPORATED

FILE NO.

REVISION

DATE

TITLE: Supplemental Airplane Flight Manual

A-10060

03/04/15

SUBTITLE:

Cessna 206 on Model 3400 Floats

REVISION: D

FAA Approved

FORCED LANDINGS

EMERGENCY LANDING ON WATER WITHOUT ENGINE POWER

1. Landing Gear -- UP.

2. Airspeed -- 79 KIAS (flaps UP) 72 KIAS (flaps DOWN).

3. Mixture -- IDLE CUT-OFF.

4. Fuel Shutoff Valve -- OFF.

5. Ignition Switch -- OFF.

6. Master Switch -- OFF.

7. Water Rudders -- UP.

8. Wing Flaps -- AS REQUIRED.

9. Doors -- UNLATCH PRIOR TO TOUCHDOWN.

10. Touchdown -- SLIGHTLY TAIL LOW.

11. Control Wheel -- HOLD FULL AFT as amphibian decelerates.

EMERGENCY LANDING ON LAND WITHOUT ENGINE POWER

1. Landing Gear -- UP on soft or rough ground. DOWN on firm and

smooth ground.

2. Airspeed -- 79 KIAS (flaps UP) 72 KIAS (flaps DOWN).

3. Mixture -- IDLE CUT-OFF.

4. Fuel Shutoff Valve -- OFF.

5. Ignition Switch -- OFF.

6. Master Switch -- OFF.

7. Water Rudders -- UP.

8. Wing Flaps -- AS REQUIRED (30° recommended).

9. Doors -- UNLATCH PRIOR TO TOUCHDOWN.

10. Touchdown -- LEVEL ATTITUDE (if gear is up). SLIGHTLY TAIL

LOW (if gear is down).

11. Control Wheel -- FULL AFT (after contact if gear is up).

12. Brakes -- APPLY HEAVILY (if gear is down).

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