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EDWARDS & ASSOCIATES, INC.
P.O. BOX 3689
BHT412EP
SIN 36106
N412SV
BRISTOL, TN. 37625
FAA APPROVED ROTORCRAFT FLIGHT MANUAL SUPPLEMENT
For
GARMIN GTX 330 MODE 8 TRANSPONDER
Ill .
EMERGENCY PROCEDURES
No Change.
IV • NORMAL PROCEDURES
1. DETAILED TRANSPONDER OPERATING PROCEDURES
Nonna! transponder operating procedures are described in the Gannin GTX 330 Pile
Guide, PIN 190-00207-00, Rev. C, dated
Mardi 2005 or later appropriate revision.
2. DISPLAY OF TRAFFIC INFORMATION SERVICE ms) DATA
TIS surveillance data unlinked
by Air Traffic Control (ATC) radar through the Gannin G.
330 Mode S Transponder will appear on the interfaced display devices. In this lnstallatic
the TIS information can
be displayed on the Garmin GNS 530). For detailed operati1
instructions and information regarding the TIS interface, refer to the Gannin 400/500
Seri
Display Interfaces (Pilot's Guide Addendum) PIN 190-00140-13 Rev. C, dated February 20l
or later appropriate revision.
V. PERFORMANCE
No Change.
VI • WEIGHT AND BALANCE
See current weight and balance data.
VII. SYSTEM DESCRIPTIONS
See the Garmin 400/500 Series Display Interfaces (Pilot's Guide Addendum}, PIN 190-0014(
13 and the Garmin GTX 330 Pilot's Guide, PIN 190-00207-00 for a complete description ofth
GTX 330 system.
JUN 2 8 2007
FAA Approval Date: -----------
(Original) Page 5 of
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