Garmin GTN 7 series Manuel d'instructions - Page 6
Parcourez en ligne ou téléchargez le pdf Manuel d'instructions pour {nom_de_la_catégorie} Garmin GTN 7 series. Garmin GTN 7 series 22 pages. Instructions for continued airworthiness for md 369e; md 369f; md 369ff
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pair Bluetooth™ audio sources. This enables the distribution of audio to ICS positions when using a
compatible iOS or Android™ device. The GMA 35c supports up to ten stored devices and one active
Bluetooth device. The GMA 35 is mounted in a notch behind the GTN 7XX to free up mounting space in
the flight deck instrument panel.
If optional HTAWS function is enabled on the GTN, HTAWS terrain caution/warning indicator and HTAWS
status annunciation are required, unless the rotorcraft is equipped with a GDU 620. These annunciators
serve as the visual indication of a terrain/obstacle caution or warning alert, HTAWS failure and HTAWS
mode status.
The Flight Stream 510 is a wireless-enabled data card that is inserted into the GTN data card slot to allow
wireless database synchronization with personal electronic devices (PEDs). Synchronized information is
then disseminated to various LRUs through their existing GTN interface connections.
2.3 Control, Operation, and Testing Information
See Garmin 190-01004-03 Rev. D, "GTN 625/635/650 Pilot's Guide" and Garmin 190-01007-03 Rev. D,
"GTN 725/750 Pilot's Guide" for information on how to operate the system in normal mode.
See the Section 3 of the
on how to operate and access configuration mode and diagnostic pages, and Section 2.1 for document
part numbers. See Section 6 for general ground checks and system test procedures.
GTN 6XX/7XX PART 27 AML STC MAINTENANCE MANUAL
See
2.4 Servicing Information
None.
In the event of system failure, troubleshoot the GTN 6XX/7XX and GMA 35 in accordance with Section 4
GTN 6XX/7XX PART 27 AML STC MAINTENANCE MANUAL
of
2.5 Periodic Maintenance
The GTN and GMA 35 are designed to detect internal failures. A thorough self-test is executed
automatically upon application of power to the units, and built-in tests (BIT) are continuously executed.
Detected errors are indicated as failure annunciations, system messages, or a combination of the two.
Operation of the GTN 6XX/7XX and GMA 35 is not permitted unless the inspections described in this
section have been completed within time intervals prescribed in Table 1. All antennas connected to the
GTN should be maintained in accordance with maintenance and inspection data appropriate for the
antenna installation.
Table 1 Maintenance Intervals for GTNs GMA 35, and Flight Stream 510
I
TEM
I
NTERVAL
1. E
R
&
QUIPMENT
EMOVAL
R
EPLACEMENT
O
C
N
ONDITION
2. D
B
ISPLAY
ACKLIGHT
O
C
N
ONDITION
190-01007-KB Rev. 3
Instructions for Continued Airworthiness GTN 6XX/7XX - MD369E/F/FF
GTN 6XX/7XX PART 27 AML STC MAINTENANCE MANUAL
D
/P
ESCRIPTION
ROCEDURE
Removal and replacement of the following items.
GTN 6XX/7XX, GMA 35, or Flight Stream 510
(1)
NAV antenna cable splitter
(2)
NAV antenna cable diplexer
(3)
Cooling Fan
(4)
GTN 6XX/7XX PART 27 AML STC MAINTENANCE MANUAL
See Section 5 of
for instructions.
The display backlight LEDs are rated by the manufacturer as having a
usable life of at least 36,000 hours. This life may be more or less than the
rated time depending on the operating conditions of the GTN. Over time,
the backlight lamp may dim and the display may not perform as well in
direct sunlight conditions.
, Section 3 for details
for a system description.
.
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