BEECHCRAFT
35-C33,
35-C33A.
E33, E33A,
E33C,I
F33.
F33A,
F33C,
G33.
S3Ei,
V35,
V36A,
V36B,
36,
A36,
AND
A36TC
lANDPlANES
PllOT'S
OF>ERATING
HANDBOOK
AND
FAA APPROVED AIRPLANE FLIGHT MANUAL
SUPPLEMENT
for
the
LANDING GEAR
S.~FETY
SYSTEM
GENERAL
This document
is
to
be attached
to
the Pilot's Operating
Handbook and FAA Approved Airplane Flight Manual when
the airplane is equipped with the Landing Gear
Safety Sys-
tem
which
has
been
installed
in
accordance
with
BEECHCRAFT FAA approved data.
This document supersedes
or
adds to the Pilot's Operating
Handbook and
FAA
Approved Airplane Flight Manual only
where covered in the"items contained herein.
LIMITATIONS
The landing gear safety system is des1gned to help prevent
"gear-up" landings and premature
or
inadvertent operation
of the
landing gear mechanism. The system is
tobe
used
as
salety backup device only; normal usage
ot
the landing gear
position switch is mandatory.
EMERGENCVPROCEDURES
In
t.he
event of an emergency, automatic extension o! the
landing gear may be prevented by placing the landing gear
safety system switch in the
OFF position, thus inactivating
the safety system.
FAA Approved
Reviaod:
April
1981
P/N
35-590110-13
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