Cessna T206H Technical specifications

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
UNCONTROLLED
COPY

SOLOY TURBINE PAC
POHS CESSNA T206H/206H
A
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.
UNCONTROLLED
COPY

SOLOY TURBINE PAC
POHS CESSNA T206H/206H
i
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
Page
Revision
Page
Revision
Title
2
1-3
0
A
0
1-4
0
i
2
1-5
0
ii
2
1-6
0
iii
2
1-7
0
iv
2
1-8
0
v
1
1-9
0
vi
2
1-10
0
vii
2
1-11
0
viii
2
1-12
0
1-1
0
2-1
0
1-2
0
2-2
0
NOTE: Revised text is indicated by a revision bar in the margin.
UNCONTROLLED
COPY

SOLOY TURBINE PAC
POHS CESSNA T206H/206H
ii
F.A.A. Approved November 17, 2015
LOG OF EFFECTIVE PAGES (Continued)
Page
Revision
Page
Revision
2-3
0
3-10
0
2-4
0
3-11
0
2-5
0
3-12
0
2-6
0
3-13
0
2-7
2
3-14
0
2-8
2
3-15
0
2-9
0
3-16
0
2-10
0
3-17
0
2-11
2
3-18
0
2-12
2
3-19
0
2-13
2
3-20
0
2-14
0
3-21
0
2-15
0
3-22
0
2-16
0
4-1
2
2-17
0
4-2
2
2-18
0
4-3
0
2-19
0
4-4
2
2-20
0
4-5
0
2-21
0
4-6
0
2-22
0
4-7
0
2-23
0
4-8
2
2-24
0
4-9
2
2-25
0
4-10
2
2-26
0
4-11
2
3-1
0
4-12
2
3-2
0
4-13
2
3-3
0
4-14
0
3-4
0
4-15
0
3-5
0
4-16
0
3-6
0
4-17
2
3-7
0
4-18
2
3-8
0
4-19
2
3-9
0
4-20
2
NOTE: Revised text is indicated by a revision bar in the margin.
UNCONTROLLED
COPY

SOLOY TURBINE PAC
POHS CESSNA T206H/206H
iii
F.A.A. Approved November 17, 2015
LOG OF EFFECTIVE PAGES (Continued)
Page
Revision
Page
Revision
4-21
0
5-23
0
4-22
0
5-24
0
4-23
2
5-25
0
4-24
0
5-26
0
4-25
0
5-27
0
4-26
0
5-28
0
4-27
0
5-29
0
4-28
0
5-30
0
4-29
0
6-1
2
4-30
0
6-2
0
4-31
0
6-3
0
4-32
0
6-4
0
5-1
0
6-5
0
5-2
0
6-6
0
5-3
0
6-7
2
5-4
0
6-8
0
5-5
0
7-1
0
5-6
0
7-2
0
5-7
0
7-3
0
5-8
0
7-4
0
5-9
0
7-5
0
5-10
0
7-6
0
5-11
0
7-7
0
5-12
0
7-8
0
5-13
0
7-9
0
5-14
0
7-10
0
5-15
0
7-11
0
5-16
0
7-12
0
5-17
0
7-13
0
5-18
0
7-14
0
5-19
0
7-15
0
5-20
0
7-16
0
5-21
0
7-17
0
5-22
0
7-18
0
NOTE: Revised text is indicated by a revision bar in the margin.
UNCONTROLLED
COPY

SOLOY TURBINE PAC
POHS CESSNA T206H/206H
iv
F.A.A. Approved November 17, 2015
LOG OF EFFECTIVE PAGES (Continued)
Page
Revision
Page
Revision
7-19
1
7-20
0
7-21
0
7-22
0
7-23
0
7-24
0
7-25
0
7-26
0
8-1
1
8-2
1
8-3
0
8-4
0
8-5
0
8-6
2
8-7
1
8-8
2
8-9
1
8-10
1
8-11
2
8-12
1
8-13
Deleted
8-14
Deleted
9-1
0
9-2
0
9-3
0
9-4
0
NOTE: Revised text is indicated by a revision bar in the margin.
UNCONTROLLED
COPY

SOLOY TURBINE PAC
POHS CESSNA T206H/206H
v
F.A.A. Approved November 14, 2014
LOG OF REVISIONS
Revision
Pages
Revised
Comments
FAA Approval
No.
Date
0
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
1
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
Reformatted
revision log
pages, no
content change.
Added Rev 16.
2-12
Corrected cold
weather fuel
spec. number.
2-13
Updated Engine
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.
UNCONTROLLED
COPY

SOLOY TURBINE PAC
POHS CESSNA T206H/206H
vi
F.A.A. Approved November 17, 2015
Revision
Pages
Revised
Comments
FAA Approval
No.
Date
2
11/17/15
Cover
i - viii
2-7 - 2-8
2-11 –2-12
2-13
4-1 - 4-2
4-4
4-8 - 4-9
4-10 - 4-13
4-17 - 4-20
4-23
6-1
6-7
8-1
8-6
8-8
8-11
Removed prev.
revision signature
and date.
Corrected
company name.
Added Rev 2.
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:
UNCONTROLLED
COPY

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.
UNCONTROLLED
COPY

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
UNCONTROLLED
COPY