Tecnam P2006T, Aircraft Flight Manual

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GARMIN G950 IFDS – SMP
FOR DIGITAL CONFIGURATION
Page SMP3-4
Section 3 – Emergency procedures
INTRODUCTION
Ed.4, Rev.0
5. Failure lamp: when illuminated, indicates that the correspondent converter
is not working properly and needs to be replaced if the maximum available
power from converter box is needed. When all converters are working
properly, the system is capable to output 40A@28V. If one converter fails,
12A@28V are lost. For this reason, the end-user mission can continue if
the equipment demand is less than 25/28A. On the contrary, the converter
needs to be replaced.
Before operating the aircraft, the pilot/operator should become thoroughly famil-
iar with this manual and, in particular, with this Section. Further on a continued
and appropriate training and self study should be done.
Two types of emergency procedures are hereby given.
a.
“BOLD FACES” which must be known by heart by the pilot and executed, in
the correct and complete sequence, immediately after the failure is detected
and confirmed.
These procedures characters are boxed and highlighted:
1.1 ENGINE FAILURE DURING TAKEOFF RUN
BEFORE ROTATION: ABORT TAKE OFF
1. Throttle Lever BOTH IDLE
2. Rudder Keep heading control
3. - -
4. - -
b. “other procedures” which should be well theoretically known and mastered,
but that can be executed entering and following step by step the AFM current
section appropriate checklist.
Additionally operating the aircraft, the pilot should become thoroughly familiar
with the Garmin G950 Pilot’s Guide for Tecnam P2006T (P/N 190-01146-XX) –
last issue - and, in particular, with the present AFM Section.
CAUTION
Garmin G950 Pilot’s Guide for Tecnam P2006T (P/N 190-
01146-XX) – last issue - must be carried onboard the airplane
at all times.
WARNING
Garmin G950 has a very high degree of functional integrity. However,
the pilot must recognize that providing monitoring and/or self-test ca-
pability for all conceivable system failures is not practical. Although
unlikely, it may be possible for erroneous operation to occur without a
fault indication shown by the G950. It is thus the responsibility of the
pilot to detect such an occurrence by means of crosschecking with all
redundant or correlated information available in the cockpit.