Cessna T206H Caractéristiques techniques

SOLOY, LLC

450 Pat Kennedy Way S.W.

Olympia, WA 98501

PILOT’S OPERATING HANDBOOK

SUPPLEMENT

AND

FAA APPROVED AIRPLANE FLIGHT MANUAL

FOR

CESSNA T206H/206H

SERIAL NO.: ___________________________

KIT SERIAL NO.: ________________________

REGISTRATION NO.: ____________________

This Supplement must be attached to the Pilot’s Operating Handbook (POH) when a

Soloy, LLC Turbine Pac engine is installed in accordance with S.T.C. SA2353NM.

Information contained herein supplements or supersedes the basic POH only in those

areas listed herein. For limitations, procedures and performance information not

contained in this Supplement, consult the basic POH.

F.A.A. Approved __________________________________________

Manager, Seattle Aircraft Certification Office

Date:

Publication Number: S2001A

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SOLOY TURBINE PAC

POHS CESSNA T206H/206H

F.A.A. Approved May 23, 2003

CONGRATULATIONS . . . . .

Your airplane is SPECIAL! A Soloy Corporation Turbine Pac

engine has been installed for those whose operation requires extra

performance and greater utility than is available with the basic engine.

This Pilot’s Operating Handbook Supplement has been

prepared to specify the difference in operating procedures and

performance. In some cases, only a specific item is changed while in

others, the entire paragraph or checklist is rewritten. For information

not included in this Supplement, consult the basic POH.

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SOLOY TURBINE PAC

POHS CESSNA T206H/206H

F.A.A. Approved November 17, 2015

LOG OF EFFECTIVE PAGES

This handbook supplement will be kept current with revisions

distributed to the last known owner of each airplane equipped with a

Soloy Turbine Pac engine.

It is the responsibility of the owner to maintain this handbook in a

current status when it is being used for operational purposes.

Owners should contact the Soloy Product Support Department

whenever the revision status of their handbook is in question.

A revision bar will extend the full length of new or revised text

and/or illustrations added on new or presently existing pages. This bar

will be located adjacent to the applicable revised area on the outer

margin of the page.

LOG OF EFFECTIVE PAGES

Dates of issue for original and revised pages are:

Original ...................... 5/23/03

Revision 1 .................. 11/14/14

Revision 2 .................. 11/17/15

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NOTE: Revised text is indicated by a revision bar in the margin.

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POHS CESSNA T206H/206H

F.A.A. Approved November 17, 2015

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POHS CESSNA T206H/206H

iii

F.A.A. Approved November 17, 2015

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POHS CESSNA T206H/206H

F.A.A. Approved November 17, 2015

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SOLOY TURBINE PAC

POHS CESSNA T206H/206H

F.A.A. Approved November 14, 2014

LOG OF REVISIONS

Revision

Pages

Revised

Comments

FAA Approval

No.

Date

5/23/03

Original

Original of

Manual.

Jeffery A. Morfitt

for Manager, Seattle

Aircraft Certification

Office, ANM-100S

Renton, WA 98055-

4056

Date: May 23, 2003

11/14/14

Cover

Removed prev.

revision signature

and date.

________________

for Manager, Seattle

Aircraft Certification

Office, ANM-100S

Renton, WA 98057-

3356

Date: (Rev 1 Date)

i-v

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revision log

pages, no

content change.

Added Rev 16.

2-12

Corrected cold

weather fuel

spec. number.

2-13

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Oil Specs.

6-7, 7-19

Added provisions

for optional

battery.

8-1, 8-2,

8-6 - 8-9

Updated Engine

Oil, Fuel specs.

(8-8 - 8-12)

Entire contents of

8-8 deleted. All

following pages

shifted up as a

result.

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SOLOY TURBINE PAC

POHS CESSNA T206H/206H

F.A.A. Approved November 17, 2015

Revision

Pages

Revised

Comments

FAA Approval

No.

Date

11/17/15

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Table of Contents

moved from pg. vii

to pg. viii.

Added propeller

RPM speed avoid

range.

Updated Fuel

section formatting.

Updated Oil

Specifications.

Updated Table of

Contents.

Updated to extend

flaps in preflight.

Updated engine

start procedures.

Updated Auto

feather procedure.

Updated amplified

start procedures.

Updated amplified

prop avoid speed

procedures.

Updated Table of

Contents.

Corrected battery

rack installation

weights.

Updated Table of

Contents.

Updated Section

Title.

Updated Caution

Note.

Updated nose gear

shock strut fill

procedure.

for Manager, Seattle

Aircraft Certification

Office, ANM-100S

Renton, WA 98055-

4056

Date:

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SOLOY TURBINE PAC PERFORMANCE

POHS CESSNA T206H/206H SPECIFICATIONS

vii

F.A.A. Approved November 17, 2015

PERFORMANCE –SPECIFICATIONS

RATE OF CLIMB AT SEA LEVEL (3600 LBS)

MCP

1,447 FPM

APPROVED CEILING

20,000 FT.

TAKEOFF PERFORMANCE:

Ground Roll

Total Distance Over a 50’ Obstacle

570 FT.

1,063 FT.

LANDING PERFORMANCE:

Ground Roll

Total Distance Over a 50’ Obstacle

553 FT.

1,094 FT.

STALL SPEEDS (CAS):

Flaps Up, Power Off

58 KNOTS

Flaps Down, Power Off

52 KNOTS

MAXIMUM WEIGHT

3,617 LBS.

TAKEOFF WEIGHT

3,600 LBS.

STANDARD EMPTY WEIGHT

2,274 LBS.

MAXIMUM USEFUL LOAD

1,343 LBS.

BAGGAGE ALLOWANCE

180 LBS.

WING LOADING

20.7 PSF

POWER LOADING

8.61 LBS/SHP

FUEL CAPACITY: TOTAL

92 GAL.

OIL CAPACITY

9 U.S. QTS.

ENGINE: Soloy Turbine Pac

418 SHP @ 1810 RPM (5 Minute Takeoff

Rating)

321 SHP @ 1810 RPM (Maximum

Continuous Rating)

780-1000-1

PROPELLER: 3-Bladed, Auto-Feather, Full

Feathering, Constant Speed

95 IN. DIA.

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SOLOY TURBINE PAC PERFORMANCE

POHS CESSNA T206H/206H SPECIFICATIONS

viii

F.A.A. Approved November 17, 2015

TABLE OF CONTENTS

SECTION

GENERAL ...............................................................................1

LIMITATIONS ..........................................................................2

EMERGENCY PROCEDURES................................................3

NORMAL PROCEDURES .......................................................4

PERFORMANCE ....................................................................5

WEIGHT & BALANCE/EQUIPMENT LIST............................... 6

AIRPLANE & SYSTEMS DESCRIPTION ................................7

AIRPLANE HANDLING, SERVICE & MAINTENANCE............8

SUPPLEMENTS

(Optional Systems Description & Operating Procedures) ....9

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Autres manuels pour T206H

Ce manuel convient aux modèles suivants

Table des matières

Autres manuels Cessna Aéronef

Cessna

Cessna 150 1969 Manuel utilisateur

Cessna

Cessna 170 52 Manuel utilisateur

Cessna

Cessna 206 Guide d'installation

Cessna

Cessna 560XL Manuel de référence

Cessna

Cessna 150G Manuel utilisateur

Cessna

Cessna SKYMASTER 336 1964 Manuel utilisateur

Cessna

Cessna 172N 1979 Manuel du propriétaire

Cessna

Cessna SKYCATCHER 162 Manuel utilisateur

Cessna

Cessna 152 Guide de configuration rapide

Cessna

Cessna 182 Manuel utilisateur

Cessna

Cessna 560 Manuel de référence

Cessna

Cessna SkyHawk 172 1966 Manuel utilisateur

Cessna

Cessna C182T Manuel utilisateur

Cessna

Cessna 172 Skyhawk SERIES Manuel utilisateur

Cessna

Cessna 525C Manuel utilisateur

Cessna

Cessna 310 1975 Manuel utilisateur

Cessna

Cessna 750 Manuel utilisateur

Cessna

Cessna 152 Guide de configuration rapide

Cessna

Cessna 152 1978 Manuel du propriétaire

Cessna

Cessna 150 1968 Manuel utilisateur

Cessna

Cessna Skywagon 185 Manuel utilisateur

Cessna

Cessna 1978 Skyhawk 172N Manuel

Cessna

Cessna 172S Nav III Manuel du propriétaire

Cessna

Cessna 680 Manuel utilisateur

Manuels Aéronef populaires d'autres marques

Cirrus

Cirrus SR22 Manuel utilisateur

Schleicher

Schleicher ASK 21 Instructions d'installation

Aircraft

Aircraft REIMS F152 Caractéristiques techniques

Skywalk

Skywalk Tequila 2 Manuel utilisateur

MAULE

MAULE M-7-235B Caractéristiques techniques

Ozone

Ozone Indy Manuel

Tecnam

Tecnam P92 Echo Super Manuel utilisateur

Wills Wing

Wills Wing HP II Mode d’emploi

Ozone

Ozone Roadster Manuel

Cirrus

Cirrus SR20 Manuel utilisateur

Niviuk

Niviuk KOYOT 3 Manuel utilisateur

Pipistrel

Pipistrel ALPHA Trainer Manuel utilisateur

REVELL

REVELL SnapTite BLUE ANGELS F-18 HORNET Manuel utilisateur

Sky

Sky EOLE Manuel utilisateur

Sabfoil

Sabfoil Surf Foil Manuel utilisateur

MAULE

MAULE MX-7-180B Caractéristiques techniques

Ozone

Ozone ZENO 2 Manuel

Boeing

Boeing 737 Manuel utilisateur