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
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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
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NOTE: Revised text is indicated by a revision bar in the margin
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F.A.A. Approved November 17, 2015
LOG OF EFFECTIVE PAGES (Continued)
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NOTE: Revised text is indicated by a revision bar in the margin
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F.A.A. Approved November 17, 2015
LOG OF EFFECTIVE PAGES (Continued)
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NOTE: Revised text is indicated by a revision bar in the margin.
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F.A.A. Approved November 17, 2015
LOG OF EFFECTIVE PAGES (Continued)
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NOTE: Revised text is indicated by a revision bar in the margin.
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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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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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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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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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POHS CESSNA U/TU 206G
ix
F.A.A. Approved November 14, 2014
LOG OF REVISIONS (Continued)
Revision
Pages
Revised
Comments
F.A.A. Approved
No.
Date
15
10/4/05
All pages
Re-issuance of
complete POHS in
digital format.
Changed all
references to Soloy
Corporation to
Soloy, LLC.
Changed all
references to
Allison Gas
Turbines to Rolls-
Royce.
Corrected minor
errors that
occurred at last
revision.
T.E.A.
for Manager, Seattle
Aircraft Certification
Office, ANM-100S
Renton, WA 98055-
4056
Date: 10-4-05
16
11/14/14
Cover
Removed prev.
revision signature
and date.
for Manager, Seattle
Aircraft Certification
Office, ANM-100S
Renton, WA 98057-
3356
Date:
i - ix
Reformatted
revision log pages,
no content change.
Added Rev 16.
Section 1,
Section 2
Headers changed
from Section I and
II to Section 1 and
2.
2-11
Corrected cold
weather fuel spec.
number.
2-12
Updated Engine
Oil Specs.
6-9, 7-27
Added provisions
for optional battery.
8-1,8-6,8-7,
8-8,8-9
Updated Engine
Oil, Fuel specs.
(8-8 - 8-14)
Entire contents of
8-8 deleted. All
following pages
shifted up as a
result.
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POHS CESSNA U/TU 206G
x
F.A.A. Approved November 17, 2015
LOG OF REVISIONS (Continued)
Revision
Pages
Revised
Comments
F.A.A. Approved
No.
Date
17
11/17/15
Cover
i-iv, x-xii
2-1
2-7, 2-8
2-11
2-12
4-1,4-2,4-7
4-8,4-10
4-15
4-17
4-18,4-21
6-1
6-9
8-6
8-12
Removed prev.
revision signature
and date.
Added Rev 17.
Table of Contents
moved from pg. x to
pg. xi. Added page
xii.
Updated TOC.
Added propeller
RPM speed avoid
range.
Updated Fuel
Section formatting.
Updated Oil
Specification
Reference.
Updated engine
start procedures.
Updated Auto
feather procedure.
Updated amplified
start procedures.
Added start/gen
cooling cycles.
Updated amplified
prop avoid
procedures.
Updated Table of
Contents.
Corrected battery
rack installation
weights.
Updated formatting.
Updated nose gear
shock strut fill
procedure.
for Manager, Seattle
Aircraft Certification
Office, ANM-100S
Renton, WA 98057-
3356
Date:
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POHS CESSNA U/TU 206G
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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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SOLOY TURBINE PAC SECTION 1
POHS CESSNA U/TU 206G GENERAL
1-1
F.A.A. Approved November 14, 2014
SECTION 1
GENERAL
TABLE OF CONTENTS Page
Introduction ...........................................................................................1-4
Descriptive Data ...................................................................................1-4
Engine ...............................................................................................1-4
Propeller ............................................................................................1-4
Fuel ...................................................................................................1-4
Oil ......................................................................................................1-4
Maximum Certified Weights ............................................................... 1-5
Standard Airplane Weights ................................................................1-5
Cabin & Entry Dimensions .................................................................1-5
Baggage Space and Cargo Door Dimensions ....................................1-5
Specific Locations .............................................................................. 1-5
Symbols, Abbreviations and Terminology .............................................1-6
General Airspeed Terminology ..........................................................1-6
Meteorological Terminology ...............................................................1-7
Engine Power Terminology ................................................................1-7
Engine Controls and Instruments .......................................................1-8
Airplane Performance and Flight Planning Terminology .....................1-9
Weight and Balance Terminology ......................................................1-9
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POHS CESSNA U/TU 206G GENERAL
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F.A.A. Approved November 14, 2014
Figure 1-1. Three View
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SOLOY TURBINE PAC SECTION 1
POHS CESSNA U/TU 206G GENERAL
1-4
F.A.A. Approved November 14, 2014
INTRODUCTION
This handbook supplement contains nine sections and includes the material
required to be furnished to the pilot by CAR Part 3. It also contains supplemental
data.
Section I provides basic data and information of general interest. It also
contains definitions or explanations of symbols, abbreviations, and terminology
commonly used.
DESCRIPTIVE DATA
ENGINE
Number of Engines: 1
Engine Manufacturer: Soloy, LLC/Rolls-Royce
Engine Model Number: Soloy Turbine Pac, 780-1000-1
Horsepower Rating and Engine Speed:
Takeoff power (5 minute): 418 SHP @ 1810 RPM
Maximum continuous Power: 321 SHP @ 1810 RPM
PROPELLER
Propeller Manufacturer: Hartzell
Propeller Model Number: HC-C3YN-5A/FC9587D-2
Number of Blades: 3
Propeller Diameter: 95 Inches
Propeller Type: Constant speed, hydraulically
actuated, full feathering
FUEL
Approved Fuel Grades: See handling, service and
maintenance, Section 8
Fuel Capacity:
S/Ns: U20603522 thru U20604649
Total Capacity: 80 Gallons
Total Usable: 76 Gallons
S/Ns: U20602589, U20604650 thru U20606847 and on
Total Capacity: 92 Gallons
Total Usable: 88 Gallons
OIL
Oil Specifications: See handling, service and maintenance, Section 8
Oil Capacity: 9 U.S. Quarts, including oil filter.
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SOLOY TURBINE PAC SECTION 1
POHS CESSNA U/TU 206G GENERAL
1-5
F.A.A. Approved November 14, 2014
MAXIMUM CERTIFIED WEIGHTS
Takeoff: 3,600 lbs.
Landing: 3,600 lbs.
Weight in Baggage Compartment –Station 109 –145:
S/Ns U20602589 & U20603522 thru U20604649 –120 lbs. maximum
S/Ns U20604650 thru U20606847 and on –180 lbs. maximum
NOTE
Refer to Section 6 of this handbook for loading
arrangements with one or more seats removed
for cargo accommodations.
STANDARD AIRPLANE WEIGHTS
Standard Empty Weight, Stationair 6 (6 seats): 1927 lbs.
Stationair 6 II (6 seats): 1987 lbs.
Utility Option (1 seat): 1882 lbs.
II Utility Option (1 seat): 1941 lbs.
Maximum Useful Load, Stationair 6 (6 seats): 1685 lbs.
Stationair 6 II (6 seats): 1625 lbs.
Utility Option (1 seat): 1730 lbs.
II Utility Option (1 seat): 1671 lbs.
CABIN AND ENTRY DIMENSIONS
Detailed dimensions of the cabin interior and entry door opening are
illustrated in Section 6.
BAGGAGE SPACE AND CARGO DOOR ENTRY DIMENSIONS
Dimensions of the baggage/cargo area and cargo door opening are
illustrated in detail in Section 6.
SPECIFIC LOADINGS
Wing Loading: 20.7 lbs./sq. ft.
Power Loading: 8.61 lbs./hp.
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SOLOY TURBINE PAC SECTION 1
POHS CESSNA U/TU 206G GENERAL
1-6
F.A.A. Approved November 14, 2014
SYMBOLS, ABBREVIATIONS AND TERMINOLOGY
GENERAL AIRSPEED TERMINOLOGY & SYMBOLS
KCAS
Knots Calibrated Airspeed is indicated airspeed corrected for
position and instrument error and expressed in knots. Knots
calibrated airspeed is equal to KTAS in standard atmosphere at sea
level.
KIAS
Knots Indicated Airspeed is the speed shown on the airspeed
indicator and expressed in knots.
KTAS
Knots True Airspeed is the airspeed expressed in knots relative to
undisturbed air which is KCAS corrected for altitude and
temperature.
VA
Maneuvering Speed is the maximum speed at which you may use
abrupt control travel.
VFE
Maximum Flap Extended Speed is the highest speed permissible
with wing flaps in a prescribed extended position.
VMO
Maximum Operating Limit Speed is the speed limit that may not
be deliberately exceeded in normal flight operations.
VS
Stalling Speed or the minimum steady flight speed at which the
airplane is controllable.
VSO
Stalling Speed or the minimum steady flight speed at which the
airplane is controllable in the landing configuration at the most
forward center of gravity.
VX
Best Angle-of-Climb Speed is the speed which results in the
greatest gain of altitude in a given horizontal distance.
VY
Best Rate-of-Climb Speed is the speed which results in the
greatest gain in altitude in a given time.
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