Daher TBM 850, Pilot'S Information Manual

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SUPPLEMENT 66
“GARMIN” G1000 NXI RETROFIT
T B M
850
Edition 0 -- October 30, 2017
Rev. 1 Page 9.66.13
SECTION 7
DESCRIPTION
Information hereafter supplement or replace those of the standard airplane
described in Section 7 ”Description” of the basic Pilot’s Operating Handbook
when the airplane is equipped with the “GARMIN” G1000 NXi RETROFIT.
7.3 -- ACCOMMODATIONS
DOORS, WINDOWS AND EMERGENCY EXIT
FWD compartment door
The FWD compartment door is located on the airplane left side between the
firewall and the front pressure bulkhead. It is hinged at the top. It is
maintained in the up position by a compensation rod. Two interlocking--type
latches ensure its closing and it is equipped with a lock [same key as for the
access door and the “pilot” door (if installed)]. When the door is closed,
latches are flush with the fuselage profile.
The “CARGO DOOR” CAS message lights on as long as FWD compartment
door is not locked.
7.15 -- MISCELLANEOUS EQUIPMENT
FLIGHT DECK INFORMATION SYSTEM (FS 510) (if installed)
The airplane is equipped with a flight deck information system allowing
portable electronics devices to stream data to and from the GARMIN
integrated flight deck system.
For the system description and its utilization, refer to GARMIN Cockpit
Reference Guide.
GARMIN INTEGRATED FLIGHT DECK (GIFD) APPROACHES
Advisory visual approaches (if installed)
The GIFD will provide advisory visual approaches to many runways in the
aviation database. Lateral guidance for the visual approach is aligned with
the runway bearing. The system also generates vertical guidance from the
runway threshold at a GIFD defined glide path (usually 3
°
, refer to the
GARMIN Pilot’s Guide for further information) allowing coupling of the
autopilot to the appropriate minimums.
PIM - DO NOT USE FOR FLIGHT OPERATIONS