Piper CHEROKEE WARRIOR II, Руководство по эксплуатации для пилотов

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Airplane Flight Manual Supplement or Supplemental Flight Manual for the NGT-9000
Revision 4 Issue: 9/19/17 Page 7 of 27 Document Number L3-76AK-AFMS1
FAA Approved
1.2 NGT-9000 ADS-B Traffic Advisory System (ATAS) [Optional]
The ADS-B Traffic Advisory System (ATAS) is a passive system that monitors ADS-B, ADS-R
and TIS-B ADS-B IN data and
alerts the flight crew via on-screen alerts aural traffic calls and an
optional Traffic Alert lamp to nearby aircraft and assists the pilot in the visual acquisition of
aircraft that may represent a danger. Refer to the Pilot's Guide, L3 p/n 0040-17000-01 Revision
H or later, for examples of on-screen symbology and aural alerts.
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The tracking of other aircraft is in a cylindrical volume centered on own aircraft with a
maximum radius of 20 nmi and extending 10,000 ft above and 10,000 ft below ownship.
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ATAS will track up to 60 intruders simultaneously.
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A Traffic Advisory (TA) is displayed when other aircraft are a potential threat.
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When ownship is in the airport environment, a Traffic Advisory (TA) is displayed 12.5 to
35 seconds prior to the CPA with another aircraft when the CPA is within 750 ft
horizontally and 300 ft vertically.
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A TA symbol remains on the screen for at least 8 seconds unless the respective track is
terminated.
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When the aircraft is outside the airport environment, aircraft that are within a range of 6
nmi of ownship with a vertical distance of +/- 1200 ft (if altitude is reporting) are classified
as a Proximate Advisory (PA). A PA is displayed only for aircraft that are in air.
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ATAS and TAS/TCAS may operate at the same time with traffic information being
correlated by the unit
When ATAS is installed, an Audio Acknowledge button will cancel the current aural
announcement.
1.3 NGT-9000 Terrain Awareness and Warning System (TAWS) [Optional]
The Terrain Awareness and Warning System (TAWS) is an optional function that is set up
during installation. The TAWS function continuously monitors the aircraft’s position, altitude,
speed, track, and phase of flight and compares the information to the terrain database loaded
during installation. Terrain and obstacle hazards are indicated by cautions and warnings using
screen annunciators, aural terrain alerts, and Terrain Caution and Warning alert lamps. Refer to
the Pilot's Guide, L3 p/n 0040-17000-01 Revision H, or later, for examples of on-screen
symbology and aural alerts.
The TAWS function uses Forward Looking Terrain Avoidance (FLTA) and Ground Proximity
Warning System (GPWS) functionality to determine when a terrain alert or altitude callout is
triggered due based on the following conditions:
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Reduced required terrain or obstacle clearance (FLTA)
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Imminent terrain impact (FLTA)
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Premature descent
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Excessive descent rate (GPWS)
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Negative climb rate or altitude loss after takeoff (GPWS)
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Passing an altitude of 500 ft (GPWS)