Beech Beechcraft Bonanza V35 Pilot Operating Handbook page 283

BEECHCRAFT 35-C33, 35-C33A, E33, E33A, E33C,1
F33. F33A, F33C. G33, S35, V35,V35A. V35B, 36,
A36, AND A36TC LANDPLANES
PILOT'S OPERATING HANDBOOK AND
FAA APPROVED AIRPLANE FLIGHT MANUAL
SUPPLEMENT
for the
LANDING GEAR SAFETY 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 designed to help prevent
"gear-up" landings and premature or inadvertent operation
of the landing gear mechanism. The system is to be used as
safety backup device only; normal usage of the landing gear
position switch is mandatory.
EMERGENCY PROCEDURES
In the event of an emergency, automatic extension of 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
Revised: April 1981
P/N 35-590110-13
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