Garmin GTN 650 Manuel de l'utilisateur - Page 8

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Également pour Garmin GTN 650 : Instructions d'activation (46 pages), Manuel de l'utilisateur (20 pages), Supplément au manuel (31 pages), Errata (4 pages), Manuel de vol (49 pages), Manuel de référence rapide (2 pages), Manuel du pilote (28 pages)

Garmin GTN 650 Manuel de l'utilisateur

Section 1. LIMITATIONS

1.1

Kinds of Operation

This model helicopter shall only be operated under VFR conditions in
accordance with 14 Code of Federal Regulations Part 91 and/or Part 135. This
RFM supplement does not grant approval for IFR operations to aircraft limited
to VFR operations.
1.2

Applicable System Software

Use of this RFMS is limited to the software versions shown in Table 2.
Software Item
Main SW Version
The Main software versions are displayed on the start-up page immediately after
power-on. All software versions displayed in Table 2 can be viewed on the
System – System Status page.
1.3

SD Card

The SD card shall be present in the unit at all times.
1.4

Ground Operations

SafeTaxi or Chartview functions shall not be used as the sole basis for ground
maneuvering.
SafeTaxi and Chartview functions do not comply with the requirements of AC
20-159 and are not qualified to be used as an airport moving map display
(AMMD). SafeTaxi and Chartview may be used by the flight crew to orient
themselves on the airport surface to improve flight crew situational awareness
during ground operations.
1.5

Terrain Proximity Function (All Units)

Aircraft maneuvers and navigation shall not be predicated upon the use of the
terrain display.
The terrain display is intended to assist the pilot with maintaining awareness of
the proximity of terrain and obstacles to the rotorcraft. By itself, the terrain
display may not provide either the accuracy or the fidelity on which to base
decisions and plan maneuvers to avoid terrain or obstacles.
190-01007-J4 Rev. 1
Page 8 of 22
Software Version
(or later FAA Approved versions for this STC)
Table 2 - Software Versions
RFMS, Bell 407 GTN GPS/SBAS System
4.00
FAA APPROVED