Cessna 206 Owner's manual

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