Cessna T206H Especificaciones técnicas

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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Title

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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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and date.

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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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