Garmin GNS 530W 파일럿 매뉴얼 부록 - 페이지 7

{카테고리_이름} Garmin GNS 530W에 대한 파일럿 매뉴얼 부록을 온라인으로 검색하거나 PDF를 다운로드하세요. Garmin GNS 530W 50 페이지. For continued airworthiness bell 206b
Garmin GNS 530W에 대해서도 마찬가지입니다: 파일럿 매뉴얼 부록 (24 페이지), 파일럿 매뉴얼 부록 (50 페이지), 파일럿 매뉴얼 부록 (24 페이지), 보충 설명서 (12 페이지), 빠른 참조 (23 페이지), 빠른 참조 (25 페이지), 사용 설명서 (23 페이지)

Garmin GNS 530W 파일럿 매뉴얼 부록
and avoid." Some of the more common examples of
these errors follow:
When client or intruder aircraft maneuvers exces-
sively or abruptly, the tracking algorithm may
report incorrect horizontal position until the
maneuvering aircraft stabilizes.
When a rapidly closing intruder is on a course that
crosses the client aircraft course at a shallow angle
(either overtaking or head on) and either aircraft
abruptly changes course within ¼ NM, TIS may
display the intruder on the opposite side of the
client than it actually is.
These are relatively rare occurrences and will
be corrected in a few radar scans once the course
has stabilized.

Improving TIS

Users of TIS can render valuable assistance in
the correction of malfunctions by reporting their
observations of undesirable performance. Reporters
should identify the time of observation, location, type
and identity of aircraft, and describe the condition
observed; the type of transponder processor and soft-
ware in use can also be useful information. Since TIS
performance is monitored by maintenance personnel
other than ATC, it is suggested that malfunctions be
reported in the following ways:
By telephone to the nearest Flight Service Station
(FSS) facility.
By FAA Form 8000-7, Safety Improvement Report,
a postage-paid card designed for this purpose.
These cards may be obtained at FAA FSSs, General
Aviation District Offices, Flight Standards District
Offices, and General Aviation Fixed Based Opera-
tions.
Part One: Section 1
TIS Operation and Symbology
3