SUPPLEMENT 49
”GARMIN”
G1000 TAWS
SYSTEM
TBM
700
850
Page 9.49.3
Rev. 1
SECTION 1
GENERAL
This supplement is intended to inform the pilot about the equipment
limitations, description and operations necessary to the operation when the
airplane is equipped with the option ”GARMIN” G1000 TAWS SYSTEM.
The TAWS function enables to detect if the airplane path is in compliance with
the overflown terrain relief.
SECTION 2
LIMITATIONS
The limitations hereafter supplement those of the standard airplane
described in Section 2 ”Limitations” of the basic Pilot’s Operating Handbook,
when the airplane is equipped with the option ”GARMIN” G1000 TAWS
SYSTEM.
The G1000 TAWS function provides terrain proximity alerting and detection
to the pilot. It must not be used for airplane vertical and horizontal navigation.
AC 2318 recommendation : in order to avoid unwillingly warnings, TAWS
function must be inhibited for any landing on a terrain which is not mentioned
in the data base.
The use of the terrain awareness warning and terrain display functions is
prohibited during QFE (atmospheric pressure at airport elevation)
operations.
The following documents or any further edition applicable to the latter, shall
be readily available to the pilot, each time the TAWS system is used :
Airplanes equipped with MOD70--0176--00
-- ”GARMIN” G1000 Integrated Flight Deck Cockpit Reference Guide for the
Socata TBM 850 No. 190--00708--00.
Airplanes equipped with MOD70--0276--00
-- ”GARMIN” G1000 Integrated Flight Deck Cockpit Reference Guide for the
Daher--Socata TBM 700 No. 190--01247--00.
