Cessna U206G STATIONAIR Owner's manual

SOLOY, LLC
450 Pat Kennedy Way S.W.
Olympia, WA 98501
PILOT’S OPERATING HANDBOOK
SUPPLEMENT
AND
FAA APPROVED AIRPLANE FLIGHT MANUAL
FOR
CESSNA U206G & TU206G STATIONAIR
SERIAL NOS. U20602589, U20603522 TO U20606846
1985 SERIAL NOS. U20606847 TO U20606920
1986 SERIAL NOS. U20606921 TO U20607020
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: S1016A
UNCONTROLLED
COPY

SOLOY TURBINE PAC CONGRATULATIONS
POHS CESSNA U/TU 206G
A
F.A.A. Approved October 4, 2005
CONGRATULATIONS . . . . .
Your airplane is SPECIAL! A Soloy, LLC 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 U/TU 206G
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 –1/4/85
Revision … 10 … 3/29/91
Revision … 1 … 1/11/85
Revision … 11 … 4/2/91
Revision … 2 … 1/18/85
Revision … 12 … 7/30/92
Revision … 3 … 4/15/85
Revision … 13 … 12/23/99
Revision … 4 … 1/27/86
Revision … 14 … 5/7/01
Revision … 5 … 4/11/86
Revision … 15 …10/4/05
Revision … 6 … 11/13/86
Revision … 16 … 11/14/14
Revision … 7 … 3/29/90
Revision … 17 … 11/17/15
Revision … 8 … 3/30/90
Revision … 9 … 5/11/90
Page
Revision
Page
Revision
Title
17
ix
16
A
15
x
17
i
17
xi
17
ii
17
xii
17
iii
17
1-1
16
iv
17
1-2
16
v
16
1-3
16
vi
16
1-4
16
vii
16
1-5
16
viii
16
1-6
16
NOTE: Revised text is indicated by a revision bar in the margin
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SOLOY TURBINE PAC
POHS CESSNA U/TU 206G
ii
F.A.A. Approved November 17, 2015
LOG OF EFFECTIVE PAGES (Continued)
Page
Revision
Page
Revision
1-7
16
3-6
15
1-8
16
3-7
15
1-9
16
3-8
15
1-10
16
3-9
15
2-1
17
3-10
15
2-2
16
3-11
15
2-3
16
3-12
15
2-4
16
3-13
15
2-5
16
3-14
15
2-6
16
3-15
15
2-7
17
3-16
15
2-8
17
3-17
15
2-9
16
3-18
15
2-10
16
3-19
15
2-11
17
3-20
15
2-12
17
4-1
17
2-13
16
4-2
17
2-14
16
4-3
15
2-15
16
4-4
15
2-16
16
4-5
15
2-17
16
4-6
15
2-18
16
4-7
17
2-19
16
4-8
17
2-20
16
4-9
15
2-21
16
4-10
17
2-22
16
4-11
15
3-1
15
4-12
15
3-2
15
4-13
15
3-3
15
4-14
15
3-4
15
4-15
17
3-5
15
4-16
15
NOTE: Revised text is indicated by a revision bar in the margin
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SOLOY TURBINE PAC
POHS CESSNA U/TU 206G
iii
F.A.A. Approved November 17, 2015
LOG OF EFFECTIVE PAGES (Continued)
Page
Revision
Page
Revision
4-17
17
5-23
15
4-18
17
5-24
15
4-19
15
5-25
15
4-20
15
5-26
15
4-21
17
5-27
15
4-22
15
5-28
15
4-23
15
6-1
17
4-24
15
6-2
15
4-25
15
6-3
15
4-26
15
6-4
15
5-1
15
6-5
15
5-2
15
6-6
15
5-3
15
6-7
15
5-4
15
6-8
15
5-5
15
6-9
17
5-6
15
6-10
15
5-7
15
7-1
15
5-8
15
7-2
15
5-9
15
7-3
15
5-10
15
7-4
15
5-11
15
7-5
15
5-12
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7-6
15
5-13
15
7-7
15
5-14
15
7-8
15
5-15
15
7-9
15
5-16
15
7-10
15
5-17
15
7-11
15
5-18
15
7-12
15
5-19
15
7-13
15
5-20
15
7-14
15
5-21
15
7-15
15
5-22
15
7-16
15
NOTE: Revised text is indicated by a revision bar in the margin.
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SOLOY TURBINE PAC
POHS CESSNA U/TU 206G
iv
F.A.A. Approved November 17, 2015
LOG OF EFFECTIVE PAGES (Continued)
Page
Revision
Page
Revision
7-17
15
9-1
15
7-18
15
9-2
15
7-19
15
SS1
15
7-20
15
SS2
15
7-21
15
SS3
15
7-22
15
SS4
15
7-23
15
7-24
15
7-25
15
7-26
15
7-27
16
7-28
15
7-29
15
7-30
15
8-1
16
8-2
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8-3
15
8-4
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8-5
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8-6
17
8-7
16
8-8
16
8-9
16
8-10
16
8-11
16
8-12
17
8-13
16
8-14
16
NOTE: Revised text is indicated by a revision bar in the margin.
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COPY

SOLOY TURBINE PAC
POHS CESSNA U/TU 206G
v
F.A.A. Approved November 14, 2014
LOG OF REVISIONS
Revision
Pages
Revised
Comments
FAA Approval
No.
Date
0
1/4/85
Original
Original of
Manual.
Lester H. Berven
for Manager, Seattle
Aircraft Certification
Office, ANM-100S
Renton, WA 98055-
4056
Date: 1/4/85
1
1/11/85
i, ii, iii, iii(a),
6-8, 9-2
and SSI 1
thru 3
Added Log of
Revisions
Page. Added
Soloy Supp.
No. 1, Exhaust
Heat
Exchanger Kit.
Lester H. Berven
for Manager, Seattle
Aircraft Certification
Office, ANM-100S
Renton, WA 98055-
4056
Date: 1/11/85
2
1/18/85
i, ii, iii, iii(a),
6-8, 9-2
and SS2 1
thru 4
Added Soloy
Supp No. 2,
Engine Inlet
Anti-Ice Kit
Lester H. Berven
for Manager, Seattle
Aircraft Certification
Office, ANM-100S
Renton, WA 98055-
4056
Date: 1/18/85
3
4/15/85
i, ii, iii, iii(a),
1-7, 3-4, 3-
5, 4-3, 4-8,
4-9, 4-19,
4-20, 5-1,
5-6, 5-7, 5-
8, 5-11 thru
5-26
Added
abbreviation
terminology,
updated climb
speeds and
procedures.
Added bleed
air information
to checklist
procedures.
Added
performance
information to
performance
section.
Lester H. Berven
for Manager, Seattle
Aircraft Certification
Office, ANM-100S
Renton, WA 98055-
4056
Date: 4/15/85
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COPY

SOLOY TURBINE PAC
POHS CESSNA U/TU 206G
vi
F.A.A. Approved November 14, 2014
LOG OF REVISIONS (Continued)
Revision
Pages
Revised
Comments
F.A.A. Approval
No.
Date
4
1/27/86
i, ii, iii, iii(a),
2-10, 8-11
Added 5.00-5, 6-
Ply Nose Wheel
Size
Lester H. Berven
for Manager, Seattle
Aircraft Certification
Office, ANM-100S
Renton, WA 98055-
4056
Date: 1/27/86
5
4/11/86
i, ii, iii, iii(a),
2-1, 2-4, 2-5,
2-6, 2-6A, 7-
1, 7-2A, 7-2B,
7-2C, 7-3, 7-
3A, 7-8
Added
information on 2”
engine
instruments.
Lester H. Berven
for Manager, Seattle
Aircraft Certification
Office, ANM-100S
Renton, WA 98055-
4056
Date: 4/11/86
6
11/13/86
i, ii, iii, iii(a),
7-2C, 7-2D
Original of
Manual.
Lester H. Berven
for Manager, Seattle
Aircraft Certification
Office, ANM-100S
Renton, WA 98055-
4056
Date: 11/13/86
7
3/29/90
Title, I, iii(a)
Added 1986
Serial Number
block on title
page.
Donald B. Wilson
for Manager, Seattle
Aircraft Certification
Office, ANM-100S
Renton, WA 98055-
4056
Date: 11/13/86
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COPY

SOLOY TURBINE PAC
POHS CESSNA U/TU 206G
vii
F.A.A. Approved November 14, 2014
LOG OF REVISIONS (Continued)
Revision
Pages
Revised
Comments
F.A.A. Approved
No
Date
8
3/30/90
I, ii, iii(a), 9-
1
Added
Cessna
Skydiving Kit
to
Supplements,
Section 9
Donald B. Wilson
for Manager, Seattle
Aircraft Certification
Office, ANM-100S
Renton, WA 98055-
4056
Date: 3/30/90
9
5/11/90
I, ii, iii, iii(a),
iii(b), 4-5, 4-
6, 7-12A
Added
schematic
showing
revised fuel
vent and
balance
system.
Changed
preflight
inspection
procedures.
Added
second page
to Log of
Revisions.
Collet E. McElroy
for Manager, Seattle
Aircraft Certification
Office, ANM-100S
Renton, WA 98055-
4056
Date: 5/11/90
10
3/29/91
I, ii, iii, iii(b),
2-7, 6-4
Misc.
changes.
Richard A. Paul
for Manager, Seattle
Aircraft Certification
Office, ANM-100S
Renton, WA 98055-
4056
Date: 3/29/91
11
4/2/91
I, ii, iii(b), 7-
2E, 7-2F
Added new
Figure # 7-3
showing
instrument
panel with
Grimes
Warning
Lights
Richard A. Paul
for Manager, Seattle
Aircraft Certification
Office, ANM-100S
Renton, WA 98055-
4056
Date: 4/2/91
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SOLOY TURBINE PAC
POHS CESSNA U/TU 206G
viii
F.A.A. Approved November 14, 2014
LOG OF REVISIONS (Continued)
Revision
Pages
Revised
Comments
F.A.A. Approved
No.
Date
12
7/30/92
I, ii, iii, iii(a),
iii(b), 2-8, 2-
11, 3-4, 3-
18, 4-4, 4-6,
4-8, 4-9, 4-
13, 4-20, 7-
2E, 7-2F, 7-
12B, 7-13,
7-13A
Addition to
Fuel Low
Warning
Systems.
Addition of
fuel
management
system using
a four
position fuel
valve.
Revised Log
of Revisions
format.
Richard A. Paul
for Manager, Seattle
Aircraft Certification
Office, ANM-100S
Renton, WA 98055-
4056
Date: 7/30/92
13
12/23/99
I, ii, iii(b),
9-2, SS3 1
thru 3
Added Soloy
Supplement
No. 3,
Continuous
Ignition Kit
T.E.A.
for Manager, Seattle
Aircraft Certification
Office, ANM-100S
Renton, WA 98055-
4056
Date: 12/23/99
14
5/7/01
I, ii, iii, iii(a),
iii(b), iii(c),
iii(d), 2-6, 4-
8, 4-17
Changed
markings on
propeller
tachometer in
Limitations
Section.
Changed
auto feather
test
procedures in
Normal
Procedures.
Upgraded
Log of
Revisions to
current
format,
adding pages
iii(c) and
iii(d).
A.J. Pasion
for Manager, Seattle
Aircraft Certification
Office, ANM-100S
Renton, WA 98055-
4056
Date: 4/10/02
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