Cessna 206H - Page 8

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