Garmin Cessna Caravan G1000 Suplement do instrukcji użytkowania samolotu - Strona 9

Przeglądaj online lub pobierz pdf Suplement do instrukcji użytkowania samolotu dla System nawigacji samochodowej Garmin Cessna Caravan G1000. Garmin Cessna Caravan G1000 33 stron. Integrated flight deck
Również dla Garmin Cessna Caravan G1000: Podręcznik pilota (16 strony), Podręcznik pilota (6 strony), Podręcznik pilota (32 strony), Podręcznik pilota (25 strony), Podręcznik pilota (34 strony), Podręcznik pilota (21 strony), Podręcznik pilota (22 strony)

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Garmin Cessna Caravan G1000 Suplement do instrukcji użytkowania samolotu
MOONEY
M20R
(c) MAP DATUM....WGS 84 (sets map datum to WGS--84, [see
note below])
(d) POSITION........deg--min (sets navigation grid units to deci-
mal minutes)
example: dd.mm.ss: 45_ 30' 30" in decimal minutes are: 45_
30.5'
In some areas outside the United States, datums other than
WGS- -84 or NAD- -83 may be used. If the G1000 is authorized
for use by the appropriate Airworthiness authority, the re-
quired geodetic datum must be set in the G1000 prior to its
use for navigation.
6. Operation is prohibited north of 70
addition, operation is prohibited in the following two regions: 1) north
of 65o N between 75
between 120
7. CAUTION: CDI automatic source switching to the ILS on Nav 1 or 2
must be set to manual for instrument approaches conducted with the
autopilot coupled. If the CDI navigation source is changed when au-
topilot is engaged in GPSS mode, the S--Tec 55x autopilot lateral
mode will revert to wings level mode and indicate GPSS FAIL. NAV
mode must be manually reselected by the pilot in order to track the
ILS or Localizer.
8. Display of autopilot operational mode on the PFD is supplemental to
the data which is presented on the display of the S--Tec 55X autopilot
control unit.
2.1 AIRSPEED MARKINGS – M20R
Marking
Red band
White band
Green band
Yellow band
Red band
The airspeed indicator is marked in IAS values.
ISSUED 11 - 2004
REVISION A 06--2005
REVISION B 03--2006
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
NOTE:
o
W and 120
o
o
E and 165
E longitude.
IAS
20 KIAS – 59 KIAS
59 KIAS – 110 KIAS
66 KIAS – 174 KIAS
174 KIAS -- 195 KIAS
195 KIAS and greater
o
N and south of 70
o
W longitude and 2) south of 55
Significance
Low speed awareness -- stall is
imminent
Operating range with flaps fully ex-
tended
Normal operating range
Caution range -- smooth air only
Lower limit of 195 KIAS is the maxi-
mum speed for all operations
AFM SUPPLEMENT
o
S latitudes. In
o
S
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FAA APPROVED