Daher TBM 850, Руководство пилота

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SUPPLEMENT 49
”GARMIN” TAWS SYSTEM
T B M
700
850
Page 9.49.3 Rev. 2
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” 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” TAWS SYSTEM.
The 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 document or any further edition applicable to the latter, shall be
readily available to the pilot, each time the TAWS system is used :
Airplane equipped with GARMIN G1000 flight deck (MOD70--0176--00)
-- ”GARMIN” G1000 Integrated Flight Deck Cockpit Reference Guide for the
TBM 850 P/N 190--00708--00.
Airplane retrofited with GARMIN G1000 flight deck (MOD70--0276--00)
-- ”GARMIN” G1000 Integrated Flight Deck Cockpit Reference Guide for the
TBM 700 P/N 190--01247--00.
Airplane retrofited with GARMIN G1000 NXi flight deck (MOD70--0539--00)
-- ”GARMIN” G1000 NXi Integrated Flight Deck Cockpit Reference Guide for
the TBM 850/900 P/N 190--02349--00.
PIM - DO NOT USE FOR FLIGHT OPERATIONS