Tecnam P2002-JF, Flight Manual, Page: 139 / 435

Page A01-5
Section 9 – Supplements
Supplement no. A01 – GARMIN GNS 430 GPS/VHF COMM/NAV
3
rd
Edition, Rev. 0
E
MERGENCY
P
ROCEDURES
1. If the information provided by the Garmin GNS430 is not available or
manifestly wrong, it is necessary to use other navigation instruments.
2.
If the message “WARN” appears in the lower left portion of the display,
the receiver cannot be considered useful as a navigation aid. The pilot
must use the VLOC receiver or an alternative navigation system.
3.
If the message “INTEG” appears in the lower left portion of the display,
the RAIM function is unavailable. The pilot must use the VLOC receiver
or an alternative navigation system;
4. In emergency flight conditions, pressing the COM flip-flop knob for 2 se-
conds will automatically tune-in the 121.500MHz emergency frequency.
N
ORMAL
O
PERATION
1. D
ETAIL FOR
N
ORMAL
O
PERATION
Normal operation is described in the “Pilot’s guide and Reference” P/N
190-00140-00 rev. F dated July 2000 or later versions.
2. GARMIN GNS 430 D
ISPLAY
Data for GNS 430 system appears on GARMIN GNS430 display.
Data source is either the GPS or the VLOC as indicated above the CDI
switch of the GARMIN 430 display.
P
ERFORMANCE
No variations.
W
EIGHT AND
B
ALANCE
See Section 6 of the present manual.
S
YSTEMS
See “GNS 430 Pilot’s Guide” p/n 190-00140-00 rev. F dated July 2000 or later
versions, for a complete description of the system.